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    • 专利摘要:
    The present invention relates to a heat exchanger (50) comprising a plurality of plates (10, 20) provided with a plane peripheral zone (19, 29), an internal zone provided with sinusoidal corrugations (13, 23, 14, 24) and two chimneys (11, 21, 12, 22) positioned at two opposite corners of said plates (10, 20). Modules (30) are formed by the assembly of two plates (10,20) which bear on said recessed corrugations (14,24) and said peripheral zones (19,29). The modules (30) are stacked while being supported on the inlet (11,21) and outlet (12,22) chimneys. Each module (30) can thus be deformed independently, especially at the level of said indentations (14,24) and peaks (13,23) without transmitting stresses to the other modules (30) of said exchanger (50). In addition, said exchanger (50) may comprise a tie rod (40) in each inlet (53) and outlet (54) pipe in order to withstand the static pressure of the fluids flowing in said pipes (53,54).
    公开号:FR3024224A1
    申请号:FR1401715
    申请日:2014-07-25
    公开日:2016-01-29
    发明作者:Olivier Honnorat；Christophe Dubourg
    申请人:Airbus Helicopters SAS；
    IPC主号:
    专利说明:

    [0001] 1 Plate heat exchanger with structural reinforcement for turboshaft engines. The present invention is in the field of heat exchangers. The invention relates to a plate heat exchanger with structural reinforcements in which two fluids preferably flow countercurrently. This heat exchanger is particularly intended for heating the intake air of a gas turbine fitted to an aircraft. The invention also relates to a gas turbine equipped with this exchanger and a rotary wing aircraft, such as a helicopter, powered by one or more of these gas turbines. Indeed, it is known that the efficiency of gas turbines is relatively low. In particular for turbine engines, a particular type of engine with gas turbines traditionally used for rotary wing aircraft, this efficiency is of the order of 25%. A known solution for improving this efficiency is to heat the air, after compression and before admission into the combustion chamber of the turbine engine. This then reduces the thermal need in the combustion chamber, and consequently reduce the fuel consumption of the turbine engine. This heating of the intake air can in particular be obtained by using the heat of the exhaust gas leaving the turbine, this heat is generally not used. For this purpose, suitable heat exchangers are particularly used in industrial thermal power plants. On the other hand, the application of such exchangers to the specific field of aircraft turbine engines encounters several major problems, the mass and the volume of these exchangers, as well as a loss of engine power using such an exchanger. Indeed, the exhaust gases leave the turbine at high speed and their circulation in a heat exchanger recovering part of their heat generates significant pressure losses on the circulation of these exhaust gases, resulting in a loss of power of the engine. turbine engine. In addition, the volume available in an aircraft being limited, the implementation of an exchanger on a turbine engine poses congestion problems. Finally, the mass is also an important criterion affecting the performance of the aircraft. We know the document FR2280870 which describes an exchanger whose two fluids flow against the current. This exchanger is formed by metal plates, for example aluminum, having regular corrugations. These corrugations are parallel to each other and perpendicular to the flows of the two fluids. The two cavities formed by these plates have the same volume, the spacing between the plates being constant and provided by spacers and bosses on each plate.
    [0002] The sealing between the plates is obtained by the use of synthetic plastic material, the fixing of the plates together being obtained by crimping. US6016865 discloses a plate heat exchanger for heat exchange between a first high-pressure and low-flow fluid and a second low-pressure, high-flow fluid. Each plate has protruding and hollow herringbone shapes that are inclined relative to the fluid flow. These shapes are also inclined to one another on two adjacent plates.
    [0003] The plates are assembled in pairs, by welding or brazing for example, on their peripheral areas and at the points of support between the recessed shapes to form modules. These modules are then stacked one on the other 5, being supported on bosses. Thus, the fluids can circulate in two independent volumes, allowing a heat exchange between them. Furthermore, EP1122505 discloses a plate heat exchanger whose plates grouped two by two are positioned in a housing. In addition, each plate has several chimneys which, once grouped, form inlet ducts and outlet pipes of the exchanger. Finally, we know the document FR2988822 which describes a heat exchanger comprising a plurality of plates. Each plate has a multitude of parallel sinusoidal corrugations of different heights and two chimneys. The plates are associated in pairs by relying on the lowest undulations and the modules formed by these pairs of plates bear on the highest undulations. The various corrugations participate in the agitation of the fluids thus improving their heat exchange. The plates of this exchanger are of low thickness and made of Inconel®. These different plate heat exchangers are usable in an engine, their volumes and masses being in reasonable proportions. However, they do not meet all the constraints generated by a turbine engine fitted to a rotary wing aircraft. Apart from the previously mentioned volume and mass constraints, the exhaust gases of a turbine engine 30 are extremely hot, of the order of 700 ° C. (degrees Celsius).
    [0004] In fact, the elements constituting the exchanger must be able to withstand such temperatures. In addition, when starting the engine, a very large and rapid temperature variation, with a passage of a temperature of the order of 15 ° C. to 700 ° C. in a ten second period, occurs within the exchanger , and in particular on each module constituted by the association of two plates. Each module then deforms following a very large thermal expansion and, the modules of the exchanger being linked together, can generate mechanical stresses on the other modules of the exchanger. A significant increase in the mechanical stresses at the level of each module occurs, accompanied by a general deformation of the exchanger and in particular a significant deformation at the two extreme modules of the exchanger. In addition, the temperature difference between these exhaust gases and the intake air is large, of the order of 300 ° C, or nearly 600 ° C at the start of the turbine engine. Likewise, the pressure difference between the two fluids is large, the exhaust gases leaving the turbine at atmospheric pressure, whereas the intake air enters the exchanger at a pressure of between 6 and 11 bars. These differences in pressure and temperature between the two fluids generate additional thermal and mechanical stresses on the exchanger. These stresses are likely to cause particular deformations and / or cracks on the components of this exchanger as well as cracks or breaks in the welds. Subsequently, the sealing of the exchanger modules may degrade, leaks appear at these modules.
    [0005] More particularly, the intake air flowing in the exchanger with a high pressure creates a very large thrust on the two end modules of the exchanger. In fact, the intake air generates localized zones of thrust on the two walls obstructing the inlet and outlet ducts, these two walls being opposite respectively to the inlet and the outlet of these ducts. Large deformations appear then on each extreme module which can go up to its degradation. The term "extreme modules" means the first and last modules 10 of the stack of modules of the heat exchanger. Solutions exist to strengthen these extreme modules, such as the addition of stiffeners (stamped) or reinforcing flanges (inserts). These solutions do not reduce the thrust of the extreme modules, but they only limit the consequences of this thrust. As a result, each end module continues to undergo deformations, which can certainly be reduced, but which ultimately will generate the appearance of cracks and leaks, or even breaks of this extreme module and / or its welds. As a result, the life of the exchanger 20 is reduced. Finally, in order to have a correct thermal efficiency of the exchanger, that is to say a large capacity to transmit the heat of the exhaust gases to the intake air, the fluids must flow over an exchange surface important and with a good heat exchange. As a result, the thermal convection between the two fluids is important. A mixing of the fluids causes an increase in convection between these fluids and, consequently, also makes it possible to improve this heat exchange. On the other hand, this mixing creates a turbulent flow of these fluids, generating pressure drops that can be significant. The pressure drops of the fluids circulating in the exchanger and the heat exchange coefficient between these fluids are therefore directly dependent. Moreover, the pressure losses of a fluid are proportional to the first order squared of the velocity of this fluid. In fact, the intake air flowing at low speed, the pressure losses suffered are very low. On the other hand, the pressure drops of the exhaust gases are all the more important as they leave the turbine at high speed. These pressure losses then lead to a loss of power of the turbine engine, which is detrimental for certain particular flight phases, such as the take-off, landing and hovering phases. The present invention therefore aims to provide a plate heat exchanger to overcome the limitations mentioned above and more particularly to improve the life of this heat exchanger by reducing the mechanical and thermal stresses experienced by the modules of the heat exchanger. According to the invention, a heat exchanger comprises a plurality of modules formed of two metal plates. Each plate has a peripheral zone, at least one inlet chimney, at least one outlet chimney and an internal crenellated zone including ridges and valleys. The peripheral zone is preferably flat and then forms a lower plane P1 in which the bottom of the hollows is located. Each inlet chimney and outlet chimney rise from the peripheral zone to an upper parallel plane P2 at the lower plane P1. The plates are assembled in pairs to form a module. These two plates are supported on the one hand at their peripheral zones and on the other hand at the contact points of the hollows. These two plates are fixed firstly at the points of support of their peripheral zones and secondly at the level of at least one point of support of their recesses.
    [0006] These two plates are fixed for example by welding and preferably by brazing. The heat exchanger according to the invention is formed by the stack of several modules. In such an exchanger, the directions of the recesses and ridges of each plate form a first angle β with the flow direction of the fluids in the exchanger and the directions of the recesses and crests of two adjacent plates form a second angle θ. not zero between them. An inlet pipe of the exchanger is formed by the assembly of an inlet chimney of each plate 15 constituting the modules. Likewise, an outlet pipe is formed by assembling an outlet chimney of each of these plates. In fact, this heat exchanger comprises one or more inlet ducts and one or more outlet ducts. This heat exchanger comprises as many inlet ducts as the plates constituting the modules comprise inlet chimneys and as many outlet ducts as these plates have outlet chimneys. The heat exchanger according to the invention also comprises a casing in which the modules are housed, this housing being provided with a plurality of walls. Two additional openings are arranged in the housing to form an inlet and an outlet of the exchanger.
    [0007] A first cavity is constituted by the interior space of a module, that is to say by the space between the two plates of this module. A first fluid then flows through all the first cavities of the heat exchanger modules between each inlet pipe and each outlet pipe. A second cavity is mainly constituted by the space between two adjacent modules and also by the space between each extreme module and a housing wall. A second fluid then flows in all the second cavities of the modules of the heat exchanger between the inlet and the outlet of the heat exchanger. This second fluid can thus flow parallel to the first fluid and preferably in the opposite direction to this first fluid: there is then a countercurrent exchanger.
    [0008] However, the second fluid can also flow in parallel and in the same direction as the first fluid: there is then a co-current exchanger. A third cavity is constituted by the space between the peripheral zones of the modules and the walls of the housing. The second fluid can also flow in this third cavity. This device is remarkable in that the modules are stacked so that two adjacent modules are supported at their inlet chimneys and their outlet chimneys, a first non-zero distance separating the peaks of the two adjacent plates of two adjacent modules. For this purpose, the peaks of each plate are located in an intermediate plane P3, which is parallel to the lower and upper planes and positioned between these two planes.
    [0009] Two adjacent modules are fixed at the inlet chimneys and outlet chimneys, for example by welding and preferably by brazing. Likewise, each end module of the stack of modules is attached to a wall at each inlet chimney and each outlet chimney by welding and preferably brazing. A plurality of modules is stacked to form the heat exchanger object of the invention. The exchanger thus comprises several first cavities and several second cavities.
    [0010] The first cavities are interconnected via each inlet conduit formed by the inlet chimneys of each plate and through each outlet conduit formed by the outlet chimneys of each plate. One end of the inlet and outlet ducts 15 opens out of the exchanger at the level of the walls of the casing and allows respectively the entry and the exit of the first fluid circulating in the first cavities. The second cavities are interconnected in particular at the inlet and the outlet of the exchanger and the space at the periphery of each plate constituting the third cavity. The circulation of the second fluid is limited by the walls of this housing. In this way, heat exchanges between the two fluids circulating in the first and second cavities are made through the plates, the two fluids flowing in parallel on either side of the plates and preferably in the opposite direction. On the other hand, no heat exchange between the two fluids occurs when the second fluid circulates in the third cavity. At least a portion of this third cavity may include a plurality of combs for orienting the second fluid to the second cavities. Indeed, a fluid is naturally directed to the space facilitating its circulation, that is to say where the pressure losses are the lowest. The second fluid would therefore naturally and essentially travel to the third cavity if it did not include these combs. These combs thus occupy the entire height of the third cavity, between the walls of the housing and the modules, in order to obstruct the second fluid and to direct it towards the second cavities. These combs also allow their particular shape to be positioned between the modules at the periphery of the plates, thus ensuring the spacing between these modules. So that the modulus of the exchanger is homogeneous, in terms of material and thermal expansion in particular, the combs are in a material close to that of the plates constituting this exchanger. Preferably, the combs are made of the same material as these plates. Advantageously, the modules forming the heat exchanger 20 of the invention are supported at the level of the inlet and outlet chimneys as well as possibly at the level of the combs present between the walls and the modules. As a result, the mechanical and thermal behaviors of each module are independent of the other modules.
    [0011] Each module can thus undergo significant deformations due firstly to a thermal expansion following significant temperature differences between the first and second fluids and secondly to a high pressure of the first fluid and / or to a significant pressure difference between the first and second fluids. These deformations of a module occur mainly at the level of the hollows and ridges. As a result, since the recesses and ridges 5 of a module are not in contact with the adjacent modules or the casing of the heat exchanger, these deformations do not propagate to the other modules or to the casing and therefore do not generate no constraint on adjacent modules or crankcase.
    [0012] Thus, the heat exchanger according to the invention allows each module to deform freely in order to absorb the thermal and mechanical stresses it undergoes. In this way, this heat exchanger makes it possible to improve the service life of each module during thermal and pressure cycles and, consequently, the lifetime of the heat exchanger in its entirety. Consequently, the heat exchanger according to the invention is particularly suitable for a first fluid whose pressure is high and / or whose pressure is significantly greater than that of the second fluid. In addition, this heat exchanger is also adapted to withstand large temperature differences as a result of large temperature differences between the first and second fluids as they enter the heat exchanger. Advantageously, this improvement in the life of the heat exchanger is obtained without the addition of stiffening or reinforcing components, that is to say without increasing the mass of this heat exchanger. In addition, the recesses and ridges of the plates can take many forms traditionally used in a heat exchanger. These various forms may in particular be imposed by the material constituting these plates and possible constraints of shaping of these plates and in order to optimize the heat exchange between the first and second fluids. The hollows and ridges of the plates have, for example, crenellated shapes of rectangular section or trapezoidal shapes. The ridges and troughs may also be sinusoidal undulations.
    [0013] In addition, the hollows and ridges of a plate may be in a single direction such as a straight line across the entire plate. For example, the hollows and ridges are directed in parallel directions. On the other hand, the hollows and ridges of a plate can be in several intersecting directions on the whole of this plate. For example, the recesses and ridges are in two intersecting directions thus forming chevrons, that is to say that each recess and each peak of a plate consist of two straight lines forming a "V", these two straight lines forming a generally acute angle between them. Of course, other shapes are possible for the hollows and ridges of these plates. These forms must, however, be compatible with the construction and stacking of the modules as well as the circulation of the first and second fluids.
    [0014] Furthermore, to have a good compromise between heat exchange and pressure drops, the peaks and troughs of the plates form a first angle / 3 with the direction of flow of the two fluids. Indeed, if the directions of the hollows and ridges were parallel to the flow direction of the fluids, their effects on the pressure losses would be minimal, but they would generate on the other hand few movements of these fluids. They would not then favor the turbulence, and consequently the thermal exchanges between the fluids.
    [0015] On the other hand, if the directions of the hollows and ridges were perpendicular to the flow direction of the fluids, they would generate a lot of movements and therefore turbulence on these fluids, thus favoring heat exchanges. On the other hand, their effects on the pressure losses would then be important.
    [0016] Consequently, in order to have a good compromise making it possible to generate acceptable turbulence on the two fluids and, consequently, a good heat exchange while limiting the pressure drops on these two fluids, the directions of the hollows and ridges are inclined by relative to the direction of flow of the two fluids of a first acute angle f3. For example, this first angle entre between the directions of the hollows as well as those of the peaks and the direction of flow of the two fluids is between 30 ° and 60 °. In addition, it may be advantageous to optimize the heat exchange between the two fluids as this first angle fi varies in the exchanger. For example, this first angle fi increases in the direction of flow of the first fluid. For example, the variation of this first angle est is between 5 ° and 20 ° from the inlet pipe to the outlet pipe of the exchanger. Preferably, the variation of this first angle est is equal to 10 ° of the inlet line to the outlet line of the exchanger. Likewise, a second angle θ between the directions of the hollows and ridges of two adjacent plates has effects on the turbulence of the flows of the two fluids and on the charge losses of these fluids. In the same manner as before, and 3024224 14 to obtain a good compromise between pressure drop and turbulence, and therefore heat exchange, this second angle e between the directions of the hollows and crests of two adjacent plates must be a non-zero angle . This second angle e between the directions of the recesses and crests of two adjacent plates is preferably between 60 ° and 120 ° depending on the flow direction of the fluids. Moreover, the exchanger is obtained by stacking these modules. Fixing these modules together can be obtained by clamping or welding, for example. Preferably, these modules are soldered at the points of support of the inlet and outlet chimneys. In addition, their spacing can be maintained by the combs located in the third cavity. Likewise, the housing walls can be fixed by clamping. Preferably, these walls are fixed together by brazing and a wall is respectively fixed to each extreme module by brazing as well. This method of fixing ensures the sealing of the exchanger and its resistance to thermal and mechanical stresses it undergoes.
    [0017] When using the heat exchanger according to the invention in a rotary-wing aircraft turbine engine, the components of the exchanger are subjected to high thermal and mechanical stresses, the first and second fluids being able to high and very different temperatures, and at equally high and different pressures. In addition, these solicitations are accentuated when the aircraft makes many starts and stops in close time, for example two to four starts in one hour. Indeed, in this case, the heat exchanger is repeatedly subjected to rapid rise in temperature and pressure, then to drops in temperature and pressure without stabilization period. Therefore, significant thermal and mechanical stresses and a phenomenon of fatigue are likely to cause cracks in particular on the plates of this exchanger or cracks or breaks in the welds. In order to best withstand these stresses, the plates can be made from a material known as "inconel®" and the solders are made with inconel® or a metal heavily loaded with nickel, whose composition is very close to that of the inconel®. This allows to have a set deforming uniformly thermally. Likewise, the walls of the casing are in inconel® and their assembly is carried out by brazing with a metal which is identical or very close to that used for brazing the plates. In addition, so that the entire exchanger remains homogeneous, in terms of material and thermal expansion in particular, the combs are optionally also Inconel®. However, other materials can also be used to make these plates according to the stresses experienced by the exchanger and the plates in particular. On the other hand, the thermal conductivity of inconel® is low, much lower than that of mild steel or aluminum. In fact, its use is not usual in a heat exchanger. In addition, the shaping of inconel® can be complex depending on the desired shapes.
    [0018] In order to compensate for this low thermal conductivity and to provide the exchanger according to the invention with a good thermal efficiency, the thickness of the plates constituting the exchanger is small. Indeed, using plates having a thickness of between 0.1 and 0.25 mm, for example, the heat exchanges between the two fluids are almost directly, that is to say as if there were no plates between them. In fact, the heat efficiency of the exchanger is excellent despite the use of a low thermal conductivity material.
    [0019] The corrosion resistance of the inconel® is also very important, which is favorable for use in an exchanger intended for an aircraft turbine engine. Indeed, the exhaust gases are corrosive and can generate the oxidation of a non-resistant material.
    [0020] The inconel® is also of great ductility. This characteristic then allows the plates to withstand the differences in temperature and pressure of the fluids flowing on either side of these plates, without degradation of these plates. These differences in temperature and pressure between the cavities are also likely to cause cracks and breaks in the welds. The use of a solder as previously described during the brazing of the plates also prevents these degradations. Indeed, the use of a filler metal very close to the metal constituting the plates 25 makes it possible to limit the differential effects of deformation in these brazing zones between the plates and the solder, thus to avoid the appearance of cracks. or breaks. In addition, the plates can be assembled together by a so-called "hard" soldering, carried out between 900 ° C and 1100 ° C. In order to withstand the temperatures of the fluids during the operation of the exchanger, the filler metal is a alloy of inconel® modified according to the soldering point, to lower its creep temperature, as and when required. assembly of the exchanger.
    [0021] Finally, the differences in pressure and temperature between the two fluids also solicit the seal between the two cavities of the exchanger. The sealing in the exchanger according to the invention is ensured by brazing between the plates. As mentioned above, the solder used during these brazing operations 10 makes it possible to guarantee a good resistance of the weld zones to these stresses, and consequently to good sealing performance. On the other hand, the small thickness of inconel® plates could pose a problem with regard to mechanical stresses, in particular the pressure difference between the two fluids flowing in the first and second cavities, and thermal stresses. The shape and the assembly of the plates however make it possible to resist these constraints. Preferably, the recesses and ridges of plates made of inconel® are, for this purpose, sinusoidal corrugations.
    [0022] The realization of these sinusoidal undulations is however a delicate operation. Indeed, whatever the material used, its elongation limit may be exceeded and cracks or cracks, due to the constraints of forming the plate, may appear in certain areas of this plate. The use of inconel® does not facilitate this forming, these mechanical characteristics not being favorable to such shaping. To mitigate these risks, the technique of electrohydroforming can be used. This technique consists of plastically deforming, possibly in several passes, a thin part, a plate for example, under the action of a fluid under pressure placed in an intense electric field. Other techniques can also be used to shape the plates, such as hot forming or cold forming using multiple passes with possible intermediate anneals. The heat exchanger according to the invention may further comprise one or more additional characteristics. In particular, the first fluid can generate, when it enters the exchanger under a large pressure, a significant thrust within the exchanger. This large thrust generated by the static pressure of the first fluid is applied to the obstructed end of each inlet pipe and each outlet pipe. This obstructed end of each inlet pipe and the end of each outlet pipe is generally obstructed by a wall of the housing respectively. As a result, this significant thrust can be transmitted to the extreme module which is attached to each of these walls and, consequently, cause large deformations on these extreme modules and possibly their degradations.
    [0023] The exchanger according to the invention may comprise a tie rod located in each inlet duct and in each outlet duct in order to avoid transmitting this significant thrust to the two end modules of the exchanger. A first opening and a second opening are respectively arranged in two of the housing walls, at the ends of each inlet line. Likewise, a third opening and a fourth opening are respectively arranged in two of these walls at the ends of each outlet duct.
    [0024] Each tie has a tubular portion, a fifth opening at a first end of the tie rod and a domed bottom at a second end of this tie rod. The first end of each tie rod is attached to one of the housing walls at the first or third openings and the second end of each tie rod is attached to another of the housing walls at the second opening or good of the fourth opening. Each tie is fixed for example by welding and preferably soldered to a wall of the housing at one side 10 of the fifth opening and secondly the curved bottom. This fastening of each tie by welding or solder thus ensures on the one hand the sealing of the heat exchanger and on the other hand the mechanical strength of this tie rod. In fact, the first fluid enters the inlet pipe through this tie rod and more precisely through the fifth opening. In addition, the tie has several cells on its tubular portion, these cavities being opposite the first cavities at the input chimneys of each plate. Thus, these cells allow the circulation of the first fluid between the first 20 cavities and on the one hand the inlet pipe, on the other hand the outlet pipe. The tubular portion of the tie rod has a section equivalent to the section of each inlet and outlet pipe to be housed inside this pipe. Since the pipe is generally cylindrical, the tubular portion of the tie rod is cylindrical as well. On the other hand, the tubular portion of the tie is not attached to any plate forming the modules of the heat exchanger. When it enters the heat exchanger, the first fluid is distributed in each inlet pipe, then in the first cavities and finally in each outlet pipe. Its static pressure then acts mainly on the curved bottom of each 302 42 2 4 20 pulling. Each curved bottom allows, by its shape, to distribute substantially uniformly the pressure of the first fluid and then undergoes little deformation. In addition, an axial thrust generated by the pressure of the first fluid is exerted mainly, or even only on the convex bottom of each tie rod and is thus taken directly by each pulling pull. This axial thrust is thus transmitted to the walls on which the tie rods are fixed, without being transmitted to the modules of the heat exchanger. The curved bottom of the tie rod has ideally a hemispherical shape in order to perfectly distribute the pressure of the first fluid on the curved bottom. However, a hemispherical bulge bottom can be penalizing in terms of size. In order to limit this bulk, the curved bottom preferably has a flattened hemispherical shape that can be referred to as "quasi-spherical". Such a substantially spherical convex bottom thus makes it possible to have a good compromise between the distribution of the pressure of the first fluid on this convex bottom and its bulk. Of course, other forms for the curved bottom may be used, these forms may in particular be imposed by the material chosen to produce the curved bottom and possible shaping constraints. In addition, each tie rod does not generate significant additional pressure drops on the first fluid, the cells 25 being placed facing the first cavities as well as sufficiently large and numerous. The use of a tie rod in each inlet pipe and in each outlet pipe does not therefore deteriorate the performance of the heat exchanger while improving its mechanical strength.
    [0025] 3024224 21 Each tie rod can also be broken down into several components to facilitate its manufacture and / or assembly on the housing walls. Such a tie has for example a tubular portion, a curved bottom and a flange having the fifth opening. The flange is attached to a housing wall at the first or third opening while the curved bottom is attached to another wall at the second or fourth opening. This flange is of a section equivalent to the tubular part, this tubular part being fixed on the one hand to this flange and on the other hand to a wall at the level of the second opening or the fourth opening. On the other hand, when the second fluid enters the heat exchanger at a very high temperature, the internal temperature of the exchanger significantly increases very rapidly. More particularly, a portion of each inlet pipe and outlet pipe is directly exposed to the flow of this second fluid, this "exposed portion" of each pipe then heats up very quickly. On the other hand, another part of each pipe is not exposed directly to this flow of the second fluid, this "unexposed part" of each pipe then heating up much less rapidly. As a result, a significant differential expansion between the exposed portion and the unexposed portion of each conduit 25 appears very rapidly as soon as the second fluid enters the exchanger. This differential expansion can reach several millimeters and generate significant stresses at the plates or modules and accelerated fatigue, this plate fixing area at the input chimneys and outlet chimneys of these plates being particularly rigid. In particular, cracks may appear on the fasteners between two plates forming a module at the inlet and / or outlet stacks of these plates. Similarly, cracks may also appear on the plates near these inlet and / or outlet chimneys. These cracks and / or these cracks then lead to degradation of the plates and / or modules, such as leaks or even breaks in plates or a module. In order to limit the effects of this differential expansion, a flexible zone may be integrated near each inlet chimney and outlet chimney of these plates in order to absorb at least a portion of the deformations consecutive to this differential expansion. This flexible zone notably allows two adjacent modules to deform independently of one another. This flexible zone also allows each inlet pipe and outlet pipe to deform radially with the exposed portion of each pipe expanding more than the unexposed portion without introducing additional plate stresses. and modules. This flexible zone preferably starts on the upper plane P2 and is situated between the upper plane P2 and the lower plane P 1. This flexible zone may be formed by one or more waves integrated in each plate around the inlet chimneys and chimneys. Release. This flexible zone is radial and located closest to the inlet chimney and the outlet chimney. This flexible zone thus plays the role of a ball joint allowing each pipe to deform or even to twist more easily by limiting the stresses transmitted beyond this flexible zone. Each wave of this flexible zone has for example the shape of a half-period of a sine wave. This flexible zone 3024224 23 preferably comprises a single wave in order to limit its bulk. In addition, a shield may also be positioned between two modules to protect each inlet stack and outlet stack from direct contact with the flow of the second fluid. This protection screen also protects the connection between two modules at the input and output stacks of a direct contact with this flow of the second fluid. In order to better protect the chimneys and the connection between the modules, this protection screen is located between each intermediate plane P3 of the two adjacent plates of two adjacent modules, that is to say between the peaks of these two adjacent plates. . The effect of the flow of the second fluid is thus reduced on the exposed portion of each inlet and outlet conduit, thereby radially uniformizing the heating of each inlet and outlet conduit. In fact, this protection screen makes it possible to reduce the differential expansion between the exposed part and the unexposed part. This protective screen is for example a circular section tube 20, each inlet chimney and each outlet chimney being cylindrical and of circular section. A shield is thus positioned around each inlet chimney and each outlet chimney and concentric with each inlet or outlet chimney.
    [0026] The function of the shields is to protect the exposed portion of each inlet stack and outlet stack from the flow of the second fluid. In fact, each shield may also be constituted by a portion of tube, for example by a half-tube. The half-tubes are then positioned around the inlet chimneys and outlet chimneys, at the exposed portion of each inlet and outlet chimney, and concentrically with each inlet or outlet chimney. exit. The material of this protective screen is identical to that of the plates, as is its thickness. The height of this protection screen 5 makes it possible to position it between two modules, a clearance taking into account, on the one hand, the expansion of this protection screen which is subjected to the flow of the second fluid and, on the other hand, the deformation and the expansion. plates of each module. In order to minimize the thermal effects of the flow of the second fluid on each inlet or outlet chimney, the use of a protective screen can be combined with the use of a flexible zone. In this case, the protective screen is preferably positioned outside the flexible zone, with respect to the center of the inlet or outlet chimneys. The joint use of a flexible zone and a protective screen makes it possible to drastically reduce the significant thermal stresses generally experienced by the inlet or outlet pipes of an exchanger equipping, in particular, a turbine engine, and thus greatly elongates. its life time.
    [0027] In addition, each module, whatever its position within the exchanger, is traversed by the first fluid and must therefore withstand the pressure of this first fluid. This pressure of the first fluid, when it is important, tends to inflate the module, or even to burst. In the central part 25 of the module, the attachment points between the two plates constituting this module are sufficiently numerous to allow the modules to resist this pressure. On the other hand, near the inlet and outlet ducts, the number of fixing points is generally lower, the directions of the recesses of the plates constituting this module being secant. As a result, these attachment points can break under the effect of the pressure of the first fluid, resulting in degradation of the module and, consequently, leakage. In fact, in order to increase the number of fixing points 5 between the two plates constituting this module and, consequently, to reinforce this zone, a stiffening washer can be positioned between these two plates on the periphery of each inlet chimney and of each exit chimney. This stiffening washer can be fixed to each of the plates for example by welding and preferably solder at the hollows of these plates and possibly the peripheral zone. This stiffening washer can be complete, that is to cover 360 °, to be fixed on the hollows located around an inlet chimney or an outlet chimney and on the peripheral zone 15 around of this entry or exit chimney. This stiffening washer may also have the shape of an arc to be fixed only at the hollows around an inlet chimney or an outlet chimney. This stiffening washer considerably increases the contact and bonding surface between the two plates constituting a module. This stiffening washer thus makes it possible to reinforce the resistance of each module to the pressure of the first fluid. Advantageously, this stiffening washer also makes each module tolerant to a potential rupture of one or more attachment points near the inlet inlet chimney and the outlet chimney, thus increasing the service life of the heat exchanger according to the invention. This stiffening washer has a small thickness. For example, this stiffening washer has a thickness equivalent to the plates, i.e. between 0.1 and 0.25mm. This stiffening washer is metallic. Preferably, this stiffening washer is made of the same material as the plates.
    [0028] Furthermore, in order to position this washer between two plates constituting a module without calling into question the other attachment points of these two plates, the recesses locally have a reduced depth for positioning the stiffening washer between the two plates. Each depression of a plate of this module thus has a reduced depth of a value at least equal to half the thickness of the stiffening washer. In addition, movable flaps may be positioned in the third cavity, between the modules and at least one of the walls. These movable flaps allow in a first open position 15 the circulation of the second fluid mainly in the third cavity and do not allow in a second closed position the circulation of the second fluid in the third cavity. In this second closed position, the second fluid then flows in the second cavities.
    [0029] In the second closed position, the flaps occupy for example the entire height of this third cavity. In fact, the second fluid encounters, in this third cavity, obstacles constituted by these flaps and is oriented mainly towards an area in which it can circulate, that is to say the second 25 cavities of the exchanger. In addition, the invention also relates to a gas turbine equipped with such an exchanger. The first fluid is then constituted by the intake air of the combustion chamber of the turbine, leaving a compressor, and the second fluid is constituted by the exhaust gas leaving the turbine.
    [0030] The gas turbine has at least one cold volute and at least one hot volute. The cold volute allows the intake air to flow from the turbine compressor to the inlet pipe of the exchanger, while the hot volute allows the intake air to flow from the outlet pipe. from the exchanger to the combustion chamber of the turbine. The gas turbine also comprises at least one intermediate nozzle and an outlet nozzle. The exhaust gases exit the turbine through the intermediate nozzle and are directed to the inlet of the exchanger, and the outlet nozzle directs the exhaust gases after they exit through the outlet of the exchanger to the exchanger. the outside of the turbine. The exchanger can be installed in the continuity of the turbine or next to the turbine. In the first case, the exhaust gases are directed directly to the exchanger after their exit from the turbine, but the volume of such a gas turbine-exchanger assembly is very important. In the second case, the exhaust gases must be directed towards the exchanger positioned next to the gas turbine.
    [0031] For this purpose, the intermediate nozzle comprises a bend which, by its adapted geometry, makes it possible to ensure this orientation of the exhaust gases while minimizing pressure losses. The gas turbine-exchanger assembly then has a more compact volume than in the first case, and can, for example, be integrated into an aircraft.
    [0032] In order to withstand the thermal and mechanical stresses while ensuring the necessary sealing for the proper functioning of the exchanger, metal bellows are arranged at the junction between the exchanger and the various elements of the gas turbine.
    [0033] Indeed, the exchanger being in a high temperature environment, all the components of the exchanger and the engine can expand. These bellows allow to overcome these dilations. The environment of the exchanger is also subjected to numerous vibrations. Again, the bellows can absorb these vibrations. These bellows are found in particular at the outlet nozzles of the turbine and outlet of the exchanger for the exhaust gases, as well as at the level of the hot and cold volutes 10 respectively connected to the inlet and outlet pipes of the intake air. Preferably, these bellows are in inconel ®. Finally, the invention also relates to a rotary wing aircraft comprising at least one gas turbine provided with an exchanger according to the invention.
    [0034] The invention and its advantages will become more apparent in the following description with exemplary embodiments given by way of illustration with reference to the appended figures which show: FIG. 1, a plate of the exchanger, FIG. 2, a module of the exchanger, FIG. 3, the stack of plates in a module, FIGS. 4 to 9, exchangers according to the invention, FIG. 10, a detailed view of FIG. 11, a plate provided with stiffening washers, and FIGS. 12 and 13, a turbine engine equipped with the exchanger.
    [0035] 3024224 29 The elements present in several separate figures are assigned a single reference. FIG. 1 shows a plate 10 comprising a flat peripheral zone 19 and a crenellated inner zone provided with sinusoidal corrugations 13 in peaks 14 and recesses 14 parallel to each other. An inlet chimney 11 and an outlet chimney 12, placed at two opposite corners of the plate 10, rise from the peripheral zone 19 to an upper plane P2 as indicated in FIG.
    [0036] The peripheral zone 19 forms a lower plane P1, in which the recesses 14 are located. The ridge corrugations 13 lie in an intermediate plane P3, this intermediate plane P3 being positioned between the lower planes P1 and upper P2 and parallel to these planes. plans P1, P2.
    [0037] A module 30 is formed, according to Figure 2, by the assembly of the plate 10 with a plate 20. The peaks 13 and the recesses 14 of the first plate 10 form with the crests 23 and the recesses 24 of the second plate A second angle e between 60 ° and 120 °.
    [0038] FIG. 3 shows the points of support between the plates 10, 20 as well as the stacking of the modules 30. The plates 10, 20 bear against the recesses 14, 24 as well as on their peripheral zones. 19, 29. They are fixed by brazing at these points of support to form the modules 30.
    [0039] These modules 30 are stacked one on the other to form the exchanger 50 according to the invention. They are supported on the inlet chimneys 11, 21 and on the outlet chimneys 12, 22. The modules 30 are joined by soldering at these points of support.
    [0040] The inlet chimneys 11, 21 of each plate 10, 20 are thus connected and form an inlet pipe 53 of the heat exchanger 50. Similarly, the outlet chimneys 12, 22 form an outlet pipe 54.
    [0041] The peaks 13 of the plates 10, 20 of two adjacent modules 30 are separated by a first distance d1 which is not zero. A second distance d2 corresponds to the distance between the apex of the ridges 13 and the bottom 14 of recesses 14 of each plate, that is to say the distance between the lower plane P1 and the intermediate plane P3 of a plate 10,20. The total height d3 of a plate 10,20 is the distance between the lower plane P1 and the upper plane P2, the input chimneys 11,21 and the outlet chimneys 12,22 rising up to this upper plane P2. These sinusoidal undulations have the same period P.
    [0042] The first distance d1 is for example between 2 and 3 mm while the second distance d2 is between 3 and 4 mm. The period P is for example equal to 9mm. The thickness of the plates 10, 20 is between 0.1 and 0.25 mm, these plates 10, 20 being in inconvenient.
    [0043] FIGS. 4 to 9 show heat exchangers 50 constituted by the stacking of the modules 30. This stack is placed inside a housing 60, provided with walls 65, in which an inlet 55 and an outlet 56 are arranged. of the heat exchanger 50.
    [0044] The space between two plates 10, 20 of a module 30 forms a first cavity. The first cavities 51 are connected by the inlet 53 and outlet 54 conduits. The space between two adjacent modules 30 forms a second cavity 52, as well as the space between an extreme module and a wall 65. cavity 58 is formed by the space between the peripheral zones 3024224 31 19 of the modules 30 and the walls 65 of the casing 60. The second cavities 52 are interconnected in particular at the inlet 55 and the outlet 56 of the exchanger 50 as well as the third cavity 58.
    [0045] A first fluid enters the exchanger 50 via the inlet pipe 53 and leaves the exchanger 50 via the outlet pipe 54 and then flows into the first cavities 51. A second fluid enters the exchanger 50 via the 55 and exits the exchanger 50 through the outlet 56 and flows in the second cavities 52, 10 parallel and preferably in the opposite direction of the first fluid. The circulation of the second fluid is limited by the walls 65 of this casing 60. The second fluid can also circulate in the third cavity 58. Thus, the first and second fluids pass through the heat exchanger 50, ensuring a thermal exchange between them. . In addition, the plates 10, 20 have a sufficiently small thickness to allow heat exchange between the first and second fluid, regardless of the thermal conductivity capabilities of these plates 10, 20.
    [0046] In the exchanger 50, the directions of the recesses 14,24 and the ridges 13,23 of each plate 10,20 form a first angle β with the direction of flow of the fluids as shown in FIG. 3 is generally constant on the same plate 10, 20 and identical for each plate 10, 20 of the exchanger 50. As a result, the second angle e between the recesses 14, 24 and the peaks 13, 23 of two plates 10, Adjacent is also generally constant and not zero. Indeed, the plates 10,20 are assembled in such a way that the directions of their recesses 14,24 and their ridges 13,23 are intersecting in order to have a good compromise between heat exchange and pressure drops between the two fluids . FIG. 4 shows combs 59 present in the third cavity 58, between the modules 30 and the walls 65 5 of the casing 60. These combs 59 make it possible to create pressure drops on the second fluid and to direct it towards the second cavities 52. These combs 59 occupy the entire height between the walls 65 of the housing 60 and the modules 30 to prevent the second fluid. The particular shape of these combs 59 also makes it possible to guarantee the spacing between the modules 30 at the periphery of these modules 30. In addition, the first fluid and the second fluid can have significant differences in temperature and pressure.
    [0047] In particular, this exchanger 50 can equip a gas turbine 100 motorizing for example a rotary wing aircraft, such a gas turbine 100 being shown in Figures 12 and 13. The first fluid can then be constituted by the air of admission of a combustion chamber 90 of the gas turbine 100 and the second fluid 20 by the exhaust gas exiting the combustion chamber 90 through an intermediate nozzle 70. This intake air flows in the modules 30 with a high pressure while the exhaust gases enter the exchanger 50 at very high temperatures.
    [0048] Each module 30 can then undergo significant deformations due firstly to the high pressure of the intake air and secondly to a thermal expansion following the significant temperature differences between the intake air and the gases. exhaust.
    [0049] 302 42 2 4 33 However, the modules 30 being supported at the inlet chimneys 11,21 and outlet 12,22 as well as possibly at the level of the combs 59 present between the walls 65 and the modules 30, the behaviors The mechanical and thermal components of each module 30 are independent of the other modules 30 of the heat exchanger 50. In fact, the deformations of a module 30, which occur essentially at the recesses 14, 24 and the ridges 13, 23, do not propagate to the other modules 30 of the heat exchanger 10 50. Similarly, these deformations of each module 30 do not propagate to the walls 65 of the housing 60. Thus, each module 30 can deform freely without generating stress on the adjacent modules 30 or on the housing 60 thus making it possible to improve the service life of each module 30 to the thermal and pressure cycles and, consequently, the service life of the heat exchanger 50. exchanger 50 may include a shot 40 in each inlet pipe 53 and in each outlet pipe 54, such a heat exchanger 50 being shown in Figures 5 to 7.
    [0050] Each tie 40 has a tubular portion 44 provided with a plurality of cells 46, a fifth opening 43 at a first end 41 of the tie rod 40 and a curved bottom 45 at a second end 42 of the tie rod 40. Each tie rod 40 may be in one piece, and that is to say composed of one and the same piece as shown in FIG. 6. Each tie rod 40 is then fixed to two walls 65 of the casing 60. The first end 41 of a first tie 40 is fixed at the level of the first opening 61 of a first wall 65 and the second end 42 of this tie rod 40 is fixed at the second opening 62 of a second wall 65 opposite this first wall 65. Similarly, the first end 41 a second tie 40 is attached at the third opening 66 of the second wall 65 and the second end of the second tie 40 is attached at the fourth opening 62 of the opposite first wall 65. Indeed, in the heat exchanger 50 shown in all the figures, the inlet of the first fluid through the inlet pipe 53 is on one side of the exchanger 50 which is opposite the outlet of the first by the outlet pipe 54.
    [0051] Each tie rod 40 may also be composed of several pieces as shown in FIG. 7, in particular to facilitate its manufacture and / or its assembly on the walls 65 of the casing 60. Each tie rod then comprises three components, a tubular portion 44 provided with several cells 46, a curved bottom 45 and a flange 47 having the fifth opening 43. The flange 47 is attached to a wall 65 at the first opening 61 or the third opening 66 depending on whether the tie 40 is located in the conduit 53 or outlet 54. The curved bottom 45 is attached to another wall 65 at the second opening 62 or the fourth opening 67. The flange 47 is of a cylindrical section equivalent to the tubular portion 44 , this tubular portion 44 being fixed on the one hand to the flange 47 and on the other hand to a wall 65 at the second opening 62 or the fourth opening 66, near the curved bottom 45.
    [0052] Each tie rod 40 or each component 44, 45, 47 of this tie rod 40, if appropriate, can be fastened by welding and preferably by brazing to the walls 65, thus ensuring, on the one hand, a seal between the inside and the outside. of the heat exchanger 50 and on the other hand the mechanical strength of this heat exchanger 50.
    [0053] The walls 65 may have dropped edges at the first and second openings 61, 62 to facilitate this assembly. On the other hand, the tubular portion 44 of the tie rod 40 is not attached to any plate 10,20 forming the modules 30 of the heat exchanger 50. In fact, the mechanical stresses undergone by this tie 40, 5 under the effect essentially of the static pressure of the first fluid flowing in the inlet pipes 53 and outlet 54 and, consequently, in the tie rod 40, are not transmitted to the modules 30, but directly to the walls 65 of the casing 60. In addition, the cells 46 facing the first cavities 51 allow the circulation of the first fluid between the inlet pipes 53 and outlet 54 and the first cavities 51. The curved bottom 45 of the tie rod has the shape of a flattened half-sphere in order to limit its size. In addition, the heat exchanger 50 shown in Figures 6 and 7 also includes a stiffening washer 70 to allow each module 30 of the heat exchanger 50 to withstand the pressure of the first fluid. This stiffening washer 70 is fixed inside each module 30, between two plates 10, 20 for example by welding and preferably solder. This stiffening washer 70 is fixed at the recesses of these plates 10, 20 around an inlet chimney 11, 21 and an outlet chimney 12, 22 and near these chimneys 11, 12, 21 , 22 and at the peripheral zone 19,29 of these plates 10,20, as shown in FIG. 11. This stiffening washer 70 can also have the shape of a circular arc and be fixed only at the level of hollow 14,24 located around an inlet chimney 11,21 or an outlet chimney 12,22 in order to follow the circular shape of these chimneys 11,12,21,22.
    [0054] 3024224 36 This stiffening washer 70 increases the contact and connecting surface between the two plates 10,20 constituting a module and thus strengthens the resistance of each module 30 to the pressure of the first fluid.
    [0055] This stiffening washer has a small thickness, equivalent to that of the plates 10,20. This stiffening washer 70 is made of the same material as the plates 10,20. Furthermore, as shown in FIG. 10, the recesses 14, 14 have locally a reduced depth making it possible to position the stiffening washer 70 between the two plates 10, 20 while allowing the other attachment points to be made between these two plates. 10.20. The heat exchanger 50 shown in FIGS. 6 and 7 also includes flexible zones 80 integrated near and around each inlet chimney 11, 21 and each outlet chimney 12, 22 of the plates 10, 20 on each of the plates 10,20. This flexible zone 80 starts on the upper plane P2 and is located between the upper plane P2 and the lower plane P1 of each plate 10,20. This flexible zone 80 comprises a single circular wave as shown in FIG. 10 positioned around the outlet chimneys 12, 22. This wave of the flexible zone 80 is in the form of a half-period of a sinusoidal wave. This wave has a height of between 1 and 2 mm and a width of between 2 and 3 mm. These flexible zones 80 allow two adjacent modules 30 to deform independently of one another, for example by expansion. These flexible zones 80 also allow each inlet pipe 53 and each outlet pipe 54 to deform radially without introducing significant mechanical stresses at the plates 10, 20 and the modules 30. The heat exchanger 50 shown in FIG. FIGS. 6 and 7 also include protection screens 85. A protection screen 85 is positioned between each pair of modules 30, around the inlet chimneys 11, 21 and outlet chimneys 12, 22, between the ridges 14. , 24 of the two adjacent plates 10,20 of two adjacent modules 30. A protective screen 85 is also positioned between an end module 30 and a wall 65 of the casing 60, around the inlet chimneys 11, 21 and the outlet chimneys 12, 22, between this wall 65 and the ridges 14, 24. of the plate 10.20 of this module 30. These protective screens 85 are circular section tubes positioned concentrically and respectively around each outlet chimney 12,22. This protection screen 85 is of the same material as the plates 10, 20 and of the same thickness. The height of this protection screen 85 is for example between 5 and 10mm. The shields 85 thus protect the inlet funnels 11, 21 and the outlet chimneys 12, 22 and the connection between two adjacent modules 30 of direct contact with the flow of the second fluid entering the exchanger 50. by the inlet 55. In fact, this protective shield 85 may also be constituted by a half-tube to protect the exposed portion of each inlet chimney 11,21 and each outlet chimney 12,22 thereof. flow of the second fluid flowing in the exchanger 50. In FIGS. 8 and 9, the heat exchanger 50 comprises movable flaps 57 positioned in the third cavity 58 between the modules 30 and a wall 65 of the casing 60, at the periphery of these 30. Combs 59 are present between another wall 65 of the casing 60, opposite these flaps 57, in order to orient the second fluid between the modules 30. In FIG. 8, the second fluid can not not pass through the third cavity 58, which is closed by the flaps 57 and the combs 59, these flaps 57 and these combs 59 orienting the second fluid between the modules 30, that is to say the second cavities 52. In Figure 9, the flaps 57 are open and the third cavity 58 is accessible by the second fluid. Indeed, this third cavity 58 is free, that is to say without obstacle. In fact, this third cavity 58 creates very little loss of load on the second fluid. The circulation in the third cavity 58 is then simpler for the second fluid than the circulation between the modules 30, which generates pressure drops. As a result, the second fluid will naturally and essentially pass through the third cavity 58 instead of passing between the modules 30. Accordingly, when the flaps 57 are open, the second fluid passes through the exchanger 50 essentially through the third cavity 58 where he suffers very little load loss. This function is useful when applying such a heat exchanger 50 to a gas turbine 100 as shown in FIGS. 12 and 13. In this case, the first fluid consists of the air 25. admission of a combustion chamber 90 of the gas turbine 100 and the second fluid by the exhaust gas exiting the combustion chamber 90 through an intermediate nozzle 70. When the exhaust gas passes through the second cavities 52 of the exchanger 50, they heat the intake air which 3024224 39 also passes through the exchanger 50 through the first cavities 51. This reduces the fuel consumption of the gas turbine 100, the intake air having It has been heated before injection into the combustion chamber 90. On the other hand, the exhaust gases can undergo head losses by passing through the second cavities 52 before leaving the exchanger via an outlet nozzle 72. charge affect say the performance of the gas turbine 100 whose power is reduced.
    [0056] To avoid this reduction in power, it is necessary to reduce or eliminate, if possible, the pressure drops of the exhaust gases. For this, the exhaust gas passes through the third cavity 58 of the exchanger 50. In this case, the intake air is not heated, the fuel consumption is not reduced.
    [0057] On the other hand, the exhaust gases undergo very little pressure drop, the gas turbine 100 then operates at maximum power. The switching between the two operating modes, that is to say reduced consumption and reduced power at normal consumption and full power, is obtained by controlling the flaps 57 from the closed position to the open position by means of means of travel. These displacement means are integrated in the exchanger or the gas turbine. In Fig. 13, a top view of the gas turbine 100 is shown. A cold volute 73 allows the intake air to flow from a compressor of the gas turbine 100 to the inlet pipe 53. A hot scroll 74 allows the intake air to flow from the fuel line. outlet 54 to the combustion chamber 90 of the gas turbine 100.
    [0058] 3024224 It can also be seen in Figure 10 that the exchanger 50 is positioned between the nozzles 70,72. In order to withstand the thermal and mechanical stresses, in particular by absorbing the expansions and the vibrations, while ensuring the necessary sealing for the proper operation of the heat exchanger 50, the metal bellows 75 are arranged at the junction between the heat exchanger 50 and the various elements of the gas turbine 100. These bellows 75 are found in particular at the intermediate nozzle 70 and the outlet nozzle 72. Such bellows 75 can also be used at the inlet ducts 53 and intake air outlet 54 in conjunction with the cold scrolls 73 and hot 74. Naturally, the present invention is subject to many variations in its implementation. Although several embodiments have been described, it is well understood that it is not conceivable to exhaustively identify all possible modes. It is of course conceivable to replace a means described by equivalent means without departing from the scope of the present invention. In particular, the shape of the hollows and ridges of the plates can be of different shapes.
    [0059] In particular, the recesses 14,24 and the ridges 13,23 of the plates 10,20 which have the shape of sinusoidal waves in all the figures can have other shapes such as rectangular slots or trapezoidal shapes. Similarly, these recesses 14,24 and the ridges 13,23 of the plates 10,20 which are in a single straight direction on all the figures can be in several intersecting directions on the whole of this plate. For example, these hollows 14,24 and the ridges 13,23 may have the form of chevrons or crenellations.
    权利要求:
    Claims (15)
    [0001]
    REVENDICATIONS1. Plate heat exchanger (50) comprising: - a plurality of modules (30) formed of two metal plates (10, 20), each plate (10, 20) having a peripheral zone (19, 29), at least one chimney inlet (11,21), at least one outlet chimney (12,22) and an inner crenellated zone having ridges (13,23) and depressions (14,24), said depressions (14,24) and said peripheral zone lying in a lower plane (P1), said input chimneys (11,21) and said output chimneys (12,22) rising from said peripheral zone (19,29) to a plane upper (P2) parallel to said lower plane (P1), said peaks (13,23) lying in an intermediate plane (P3) parallel to said planes (P1, P2) and positioned between said planes (P1, P2), two plates ( 10,20) constituting a module (30) bearing on the one hand at the level of said peripheral zones (19,29) and on the other hand at the points of support of said recesses (14,24), at least one inlet duct (53) being formed by said inlet ducts (11,21) of each plate (10,20) and at least one outlet duct (54) being formed by said outlet ducts (12,22) of each plate (10, 20), the directions of said recesses (14,24) and said peaks (13,23) of each plate (10,20) forming a first angle / 3 with the direction of circulation of the fluids circulating in said exchanger (50), the directions of said recesses (14,24) and said peaks (13,23) of two adjacent plates (10,20) forming a second angle e not zero between them, 3024224 42 - a housing (60) provided with of walls (65) inside which said modules (30) are housed, an inlet (55) and an outlet (56) of said exchanger (50) being arranged in said housing (60), - a first cavity (51) constituted by the interior space of each module (30), a first fluid able to flow in said first cavities (51) between each inlet duct (53) and each duct an outlet (54); a second cavity (52) constituted by the space between two adjacent modules (30) and the space between each extreme module (30) and a wall (65) of said housing (60); ), a second fluid able to flow in said second cavities (52) between an inlet (55) and an outlet (56) of said exchanger (50), and - a third cavity (58) constituted by the space between said zones peripherals (19,29) of said modules (30) and said walls (65), characterized in that said modules (30) are stacked such that two adjacent modules (30) are supported at said input chimneys ( 11,21) and said output chimneys (12,22), a first non-zero distance separating said peaks (13,23) from said two adjacent plates (10,20) of two adjacent modules (30).
    [0002]
    Heat exchanger (50) according to claim 1, characterized in that a first opening (61) and a second opening (62) are respectively arranged in two of said walls (65) for each inlet line (53). , a third opening (66) and a fourth opening (67) being respectively arranged in two of said walls (65) for each outlet line (54), a tie rod (40) is located in each inlet duct (53). ) and in each outlet duct (54), said tie rod (40) having a tubular portion (44), a fifth opening (43) at a first end (41) of said tie rod (40) and a curved bottom (45) at a second end (42) of said tie rod (40), said first end (41) of each tie rod (41) being attached to one of said walls (65) at said first opening (61) or said third opening (66); ) and said second end (42) of each tie rod (40) being attached to another desdi said walls (65) at said second opening (62) or said fourth opening (67), said tie rod (40) having a plurality of cavities (46) on said tubular portion (44) for allowing said first fluid to flow between on the one hand said inlet pipe (53) or said outlet pipe (54) and on the other hand said first cavities (51). 15
    [0003]
    3. heat exchanger (50) according to claim 2, characterized in that said tie rod (40) comprises at least three components, a tubular portion (44), a flange (47) having a fifth opening (43) and a domed bottom (45), said flange (47) being attached to one of said walls (65) at said first opening (61) or said third opening (66) and said domed bottom (45) attached to another of said walls (65) at said second opening (62) or said fourth opening (67), said tubular portion (44) being attached to said wall at said second opening (62) or said fourth opening (67). ) and said flange (47), said tubular portion (44) having a plurality of cells (46) for allowing said first fluid to flow between said inlet pipe (53) or said outlet pipe (54). and on the other hand said first cavities (51).
    [0004]
    4. heat exchanger (50) according to any one of claims 2 to 3, 3024224 44 characterized in that said curved bottom (45) of each tie rod (40) is of quasi-spherical shape.
    [0005]
    5. Heat exchanger (50) according to any one of claims 1 to 4, characterized in that a stiffening washer (70) is positioned in each module (30) at the periphery of each inlet pipe (53) and outlet (54), said stiffening washer (70) being fixed to said recesses (14,24) of said two plates (10,20) constituting said module (30). 10
    [0006]
    6. heat exchanger (50) according to claim 5, characterized in that said recesses (14,24) locally have a reduced height for positioning said stiffening washer (70) between said two plates (10,20) constituting said module (30). 15
    [0007]
    7. Heat exchanger (50) according to any one of claims 1 to 6, characterized in that a flexible zone (80) is integrated around each inlet chimney (11,21) or each outlet chimney (12,22). 20
    [0008]
    8. Heat exchanger (50) according to claim 7, characterized in that said flexible zone (80) comprises at least one radial wave starting on said upper plane (P2) and being between said upper plane (P2) and lower plane ( P1).
    [0009]
    9. Heat exchanger (50) according to any one of claims 1 to 8, 3024224 45 characterized in that a protective screen (85) is positioned between two modules (30) around each inlet chimney (11). 21) and / or each outlet chimney (12,22).
    [0010]
    10. Heat exchanger (50) according to claim 9, characterized in that said shielding screen (85) is located between each lower plane (P1) of said two adjacent plates (10,20) of two adjacent modules (30).
    [0011]
    11. Heat exchanger (50) according to any one of claims 9 to 10, characterized in that said protective screen (85) is a circular section tube.
    [0012]
    12. Heat exchanger (50) according to any one of claims 9 to 10, characterized in that said protective screen (85) is a half-tube of circular section.
    [0013]
    13. Gas turbine (100), characterized in that it comprises a plate heat exchanger (50) according to any one of claims 1 to 12.
    [0014]
    14.Turbine gas (100) according to claim 13, characterized in that said first fluid is compressed air supplying a combustion chamber (90) of said turbine (100) and said second fluid is constituted by the gases of exhaust from said combustion chamber (90), said gas turbine having at least one cold volute (73) allowing said intake air to flow from a compressor of said turbine (100) to said inlet line (53), at least one hot volute (74) 3024224 46 allowing said intake air to flow from said outlet pipe (54) to said combustion chamber (90), at least one intermediate nozzle (70) for directing said exhaust gases from said combustion chamber (90) to said inlet (55) of said exchanger (50) and at least one outlet nozzle (72) for directing said exhaust gases after their exit through said outlet ( 56) of said exchanger (50).
    [0015]
    15. A rotary wing aircraft, characterized in that said aircraft comprises at least one gas turbine (100) according to any one of claims 13 to 14.
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    同族专利:
    公开号 | 公开日
    WO2016012161A2|2016-01-28|
    EP3172517A2|2017-05-31|
    US20170131035A1|2017-05-11|
    FR3024224B1|2018-12-07|
    WO2016012161A4|2016-06-02|
    US10619934B2|2020-04-14|
    WO2016012161A3|2016-03-24|
    EP3172517B1|2019-08-07|
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    法律状态:
    2015-06-25| PLFP| Fee payment|Year of fee payment: 2 |
    2016-01-29| PLSC| Search report ready|Effective date: 20160129 |
    2016-07-21| PLFP| Fee payment|Year of fee payment: 3 |
    2017-07-24| PLFP| Fee payment|Year of fee payment: 4 |
    2018-07-25| PLFP| Fee payment|Year of fee payment: 5 |
    2020-07-21| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1401715|2014-07-25|
    FR1401715A|FR3024224B1|2014-07-25|2014-07-25|PLATE HEAT EXCHANGER WITH STRUCTURAL REINFORCEMENTS FOR TURBOMOTEUR|FR1401715A| FR3024224B1|2014-07-25|2014-07-25|PLATE HEAT EXCHANGER WITH STRUCTURAL REINFORCEMENTS FOR TURBOMOTEUR|
    US15/318,596| US10619934B2|2014-07-25|2015-06-16|Plate heat exchanger comprising structural reinforcements for a turbine engine|
    PCT/EP2015/063401| WO2016012161A2|2014-07-25|2015-06-16|Plate heat exchanger comprising structural reinforcements for a turbine engine|
    EP15729169.1A| EP3172517B1|2014-07-25|2015-06-16|Plate heat exchanger comprising structural reinforcements for a turbine engine|
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