• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to an acoustic treatment gas ejection duct (8) provided with at least one wall called "acoustic wall (30)" intended to be in contact with said gas. The acoustic wall (30) comprises an inner skin (40) and an outer skin (35) which are separated at least partially by a space, said acoustic wall (30) comprising at least one mesh (60) internal to said space, said mesh (60) defining a plurality of cavities (61). Each cavity (61) has a parallelepipedal shape, each mesh (60) extending longitudinally in a direction called "manufacturing direction" having an acute angle greater than or equal to a predetermined angle with a horizontal plane (300), the inner skin (40) and the outer skin (35) each having an acute inclination greater than or equal to a predetermined angle with said horizontal plane (300).
    公开号:FR3042541A1
    申请号:FR1502204
    申请日:2015-10-20
    公开日:2017-04-21
    发明作者:Philippe Loewenstein；Remi Herfort
    申请人:Airbus Helicopters SAS；
    IPC主号:
    专利说明:

    Noise-treated gas removal duct, aircraft and method for manufacturing such duct
    The present invention relates to an acoustic treatment gas ejection duct, and an aircraft provided with such a duct. In addition, the invention relates to a method of manufacturing such a conduit. The invention is therefore in the technical field of aircraft gas ejection ducts.
    An aircraft usually comprises a motor involved in the propulsion or lift of this aircraft. For example, a rotorcraft may comprise a heat engine rotating a rotor participating at least in the lift of the aircraft.
    The heat engine generates exhaust gases expelled from the aircraft by an ejection system. On an aircraft, a gas ejection system may comprise a conduit usually referred to as a "nozzle" discharging exhaust gases outside the aircraft. A heat engine may also include a gas sampling duct directing gases to other equipment of the aircraft.
    Engines used in the aeronautical field can produce a painful sound to hear for a man. Gas ejection systems are then sometimes treated acoustically to try to reduce the noise emitted, especially in a range of frequencies making hearing painful to the human ear.
    Aircraft gas ejection systems must furthermore meet mechanical strength requirements for the ambient environment and the requirements of the official aeronautical regulatory bodies.
    To reduce the noise emitted, a mechanical system may comprise walls provided with small locally open cells on the outside forming so-called Helmholtz resonators. Such cells are referred to as "cavities" for convenience.
    Helmholtz resonance is a physical phenomenon that occurs when an acoustic wave moves near a cavity in communication with the outside through an opening. The original acoustic wave enters the cavity through the opening, then bounces back into the cavity forming a phase-shifted wave, an image of the original acoustic wave. The superimposition of the original acoustic wave and the phase-shifted wave leads to an attenuated resulting wave. The level of noise emissions is therefore reduced.
    The cavities therefore function in the presence of acoustic waves as a vibrating system with a degree of freedom whose mass is related to the dimensions of the cavities, make the stiffness is related to the volume of air in each cavity, and the damping is related the resistance offered by the external environment to the generation of acoustic waves.
    On an aircraft, a wall provided with resonators using this principle comprises a core defining small hexagonal-section cavities applying the principle of the Helmholtz resonator. Such a cavity then has the shape of a hexagonal section cylinder extending in elevation from an open base to an open top. Because of this geometry, the soul is called a "honeycomb layer".
    This soul is then brazed to a rear plate which closes each base of the cylinders. In addition, a perforated skin rests on the tops of the cylinders so that each cavity can communicate through a plurality of perforations with the ejected gases.
    Thus, a helicopter gas ejection prototype with acoustic treatment comprises titanium sheets. These sheets are shaped and welded together to form a wall comprising cavities with hexagonal section or large cavities. The wall further comprises a perforated skin contiguous to the cavities.
    This gas ejection prototype can make it possible to produce cavities with different dimensions. Therefore, the use of cavities with different volumes can attenuate a noise over a wider range of frequencies. Nevertheless, the realization of different cavities proves difficult to achieve using sheets brazed to each other.
    In addition, the assembly of the sheets requires many manufacturing operations. In particular, this assembly may require the delicate soldering of thin metal sheets.
    As a result, the realization of a gas ejection duct and in particular a nozzle provided with such acoustic treatment means may be difficult and / or expensive.
    FR 2,712,640, FR 2,929,336 and EP 2,865,947 are far from the problem of the invention and are cited for information purposes only.
    FR 2,712,640 describes a structure having a low aerodynamic drag surface. This structure comprises cells opening on an external medium through an opening and on a channel through another opening.
    The document FR 2,929,336 relates to a planar jets device used to reduce the noise generated by an aircraft reactor. The device comprises a wall surrounding a flow of gas ejected by a reactor. Ducts are distributed at a periphery of a downstream end of the wall to eject a jet of fluid in the form of a web.
    The document EP 2,865,947 aims a damper for reducing acoustic pulsations in a chamber of a gas turbine. This damper has a cavity opening on a bent tube in communication with this chamber.
    The present invention therefore aims to provide an acoustic treatment gas ejection duct having a structure that can allow its realization in an optimized manner.
    According to the invention, an acoustic treatment gas ejection duct is provided with at least one mechanical member, this mechanical member having at least one so-called "acoustic wall" intended to be in contact with said gas, this acoustic wall. comprising an inner skin and an outer skin which are at least partially separated by a space, said acoustic wall comprising at least one internal mesh arranged in space, the mesh defining a plurality of cavities, each cavity extending in thickness of the skin inside the outer skin, the inner skin being intended to be in contact with the gas, the inner skin having perforations, each cavity communicating with at least one perforation.
    The acoustic treatment gas ejection duct may be a nozzle directing the gases towards the outside of the aircraft, or a sampling duct directing gases towards at least one other equipment of an aircraft.
    Each cavity has a parallelepipedal shape, the inner skin and the outer skin and each mesh extending in elevation from a horizontal plane, each mesh extending in elevation in a direction known as "manufacturing direction" having an angle acute upper or equal to a predetermined angle with said horizontal plane, the inner skin and the outer skin each having an acute inclination greater than or equal to a predetermined angle with said horizontal plane. The expression "each having an inclination" means that each surface of each wall concerned has the inclination described. The expression "in elevation" refers to a direction having an acute angle or zero with gravity during the manufacture of the wall concerned.
    As a result, the term "longitudinal" refers to a direction of extension of a cavity in a direction from the inner skin to the outer skin. The term "transverse" refers to a direction substantially orthogonal to a direction in elevation and a longitudinal direction.
    As a result, this acoustic treatment gas ejection duct can be produced according to the invention by implementing a laser sintering method, said acoustic treatment gas ejection duct being made in layer-by-layer elevation of a base to a vertex by repetition of the following steps: - removal of a layer of material by a roller, such as a metal powder, - local consolidation of said layer, by implementing a laser, - descent of a supporting plate the sound treatment gas ejection duct during manufacture to deposit the next layer.
    When the acoustic treatment gas ejection duct is terminated, the acoustic treatment gas ejection duct is removed from the manufacturing device to remove the surrounding powder.
    The technology of three-dimensional printing, and in particular the sintering of a powder by laser, is interesting because of its relative simplicity. This technology can enable relatively complex parts to be produced with reasonable manufacturing costs. Nevertheless, this technology is not always easy to implement. Therefore, an acoustic wall of an acoustic treatment gas ejection duct has according to the invention Helmholtz resonators in the form of parallelepipeds and not honeycombs. This innovative parallelepipedic shape allows an elevation of the mesh and avoids the establishment of substantially horizontal surfaces that are impossible to manufacture with a laser sintering method. This parallelepipedal shape further optimizes the acoustically treated surface by allowing the transversal alignment and elevation of an unlimited number of cavities without loss of treated surface.
    In addition, the parallelepiped shape can help attenuate the sound waves, very painful to bear by a human ear, a frequency close to 5000 Hz.
    In addition, the cavities of a mesh are in a plane extending transversely and in elevation which has an acute angle greater than or equal to a predetermined angle with a horizontal plane.
    Indeed, the applicant notes that a wall having an angle too small relative to a horizontal plane can not be manufactured by laser sintering. Indeed, such an angle does not maintain the powder of a layer bearing on the previous layer.
    As a result, the other elements of the acoustic treatment gas ejection duct and in particular the inner skin and the outer skin of an acoustic wall also have an acute inclination greater than or equal to this predetermined angle.
    In addition, the acoustic treatment gas ejection duct can be made by laser sintering with a strong metal material.
    In addition, the manufacture of an object by laser sintering requires the evacuation of powder residues which is problematic in the presence of cavities. The perforations of the inner skin can nevertheless participate in the evacuation of powder residues used in the manufacture, but also in the drainage of the acoustic treatment gas ejection duct.
    As a result, the acoustic treatment gas ejection duct can meet acoustic requirements due to the presence of innovative cavities, the requirements of regulating organisms (drainage, mechanical resistance, etc.), to the necessary requirements. for the mechanical strength of the acoustic treatment gas ejection duct at environmental conditions (temperature, pressure, etc.) and finally design requirements for the laser sintering of metal powder (skin thicknesses, angles with respect to the vertical...).
    The acoustic treatment gas ejection duct may also include one or more of the following features.
    Thus, the predetermined angle is optionally equal to 45 degrees.
    In addition, each tangent to one of said skins which is arranged in a plane perpendicular to said horizontal plane has a said inclination.
    As a result, each wall surface has the required inclination.
    Furthermore, said cavities of a mesh are for example arranged in elevation one above the other, and transversely next to each other.
    The mesh takes the form of a plane having for thickness the thickness of the cavities in a longitudinal direction. This arrangement makes it easy to produce the mesh by laser sintering.
    In addition, each cavity may be bounded in elevation by a partition called "upper partition" and a partition called "lower partition", each cavity being delimited transversely by a partition called "left sidewall" and a partition called "right sidewall" each extending in elevation from the lower partition to the upper partition, each cavity being defined in transverse thickness by a non-perforated portion of the outer skin and a perforated portion of the inner skin.
    Each cavity is then delimited by six faces, namely an upper partition substantially parallel to a lower partition, a left lateral partition substantially parallel to a right lateral partition, and a non-perforated portion of the outer skin substantially parallel to a rear perforated portion of the inner skin.
    Each of said partitions is optionally rectangular.
    Furthermore, each cavity has a non-rectangular parallelepiped shape, the lower partition and the upper partition each having a different angulation of 90 degrees with the left side wall or the right side wall.
    On the other hand, like the meshes as well as the inner and outer skins, each partition has an angulation of between 45 degrees included and 90 degrees included with a horizontal plane.
    In addition, at least one said partition of a cavity has a drainage opening opening out of this cavity.
    The acoustic treatment gas ejection duct thus contains openings allowing the drainage of this acoustic treatment gas ejection duct.
    In particular, each cavity can communicate with each adjacent cavity transversely through an opening to allow the escape of the powder after manufacture. Two transversely adjacent cavities thus share a common lateral partition, the left lateral partition of one cavity representing the right lateral partition of the other cavity. This side wall can then have a drainage opening.
    This characteristic is not obvious in the context of the application of the Helmholtz principle. However, the Applicant notes that a side wall with a limited opening nevertheless provides an acoustically efficient cavity.
    Similarly, the acoustic treatment gas ejection duct may comprise at least one skin provided with at least one drainage orifice opening on the outside of the acoustic treatment gas ejection duct.
    The acoustically treated gas ejection duct contains internal holes of the drainage port type for drainage. For example, the space between an inner skin and an outer skin opens on at least one drainage hole in the inner skin or the outer skin.
    In addition, the acoustic wall can be made from various materials, and in particular from materials compatible with the laser sintering method known by the acronym ALM and the English expression "Additive Layer manufacturing".
    Titanium 6242 seems to be conceivable.
    Similarly, the acoustic wall can be made from NiCr19Fe19Nb5Mo3 material.
    This material corresponds to the material known under the brand inconel 718. The material used to manufacture the acoustic treatment gas ejection duct can thus be inconel 718 powder which makes it possible to meet the requirements of mechanical resistance in the environment. external to the acoustic treatment gas ejection duct with low thicknesses.
    Thus, at least one of said inner and outer skins has a thickness of less than one millimeter.
    Thickness is the smallest dimension of a skin.
    Moreover, each perforation may have a diameter less than or equal to four millimeters and of the order of one millimeter.
    Similarly, the openings and orifices described above have a diameter less than or equal to four millimeters.
    The applicant notes that the making of a hole in a plane extending in elevation with diameters greater than four millimeters is difficult or impossible.
    As a result, each cavity optionally communicates with at least four perforations with a maximum diameter of 1.5 millimeters.
    The cavities are covered with a perforated inner skin with perforations 1.5 millimeters in diameter to allow a Helmholtz resonance phenomenon at a calculated frequency of 5000 Hz. This frequency is determined from the volume of cavities, the speed of sound , the number and the diameter and the depth of the perforations.
    In addition, the acoustic treatment gas ejection duct may be a nozzle, each mechanical member is to be selected from a list comprising a skirt, a central cone, and an arm connecting said skirt to the central cone.
    For example, the acoustic treatment gas ejection duct is made on the basis of the nozzle of the Tigre® helicopter by incorporating acoustic walls according to the invention into the skirt, the central cone and the arms of the nozzle.
    Furthermore, the invention is directed to an aircraft equipped with an acoustic treatment gas ejection duct of the type described above. The invention and its advantages will appear in more detail in the context of the following description with examples given by way of illustration with reference to the appended figures which represent: FIG. 1, a view showing an aircraft according to the invention; FIG. 2 is a three-dimensional view of an acoustical processing gas-jet type acoustic treatment gas ejection duct; FIG. 3 is a view of a portion of an acoustic wall; FIG. 4, a view explaining the inclination and the angle allowed for the inner and outer skins as well as for the mesh, FIG. 5, an exploded view of a portion of an acoustic wall making it possible to visualize cavities FIG. 6 is a view of a skirt of an acoustic treatment gas-jet type ejection duct with acoustic treatment according to the invention; FIG. of a conduit acoustic treatment gas ejection of acoustic treatment gas ejection nozzle type; FIGS. 8 and 9, a view of a central cone of a nozzle type acoustic treatment gas ejection duct; Figure 10 is a view of a sound treatment gas-extraction gas ejection duct, and Figure 11 is a view of a manufacturing device illustrating the process according to the invention.
    The elements present in several separate figures are assigned a single reference.
    Note that three directions X, Y and Z orthogonal to each other are shown in some figures.
    The X direction is called longitudinal. Another direction Y is said transverse. Finally, a third direction Z is elevation and corresponds to the height dimensions of the structures described.
    Figure 1 shows an aircraft 1 according to the invention.
    This aircraft 1 is provided with a power plant 3 comprising at least one engine 4. For example, the engine 4 sets in motion a rotor 2 at least participating in the lift of the aircraft via a power transmission box 5. The Engine 4 may be a heat engine ejecting gases 200, such as a piston engine or a turbine engine.
    To evacuate gases from the engine, the aircraft 1 is provided with an acoustic treatment gas ejection duct 8.
    Such an acoustic treatment gas ejection duct 8 may be an acoustic treatment gas ejection nozzle 10 directing the gases towards the outside of the aircraft, for example downstream of an expansion turbine of a turbine engine.
    In addition, an acoustic treatment gas ejection duct 8 may take the form of a duct drawing a gas from the engine 4 to direct these gases to at least one other equipment 6 of the aircraft, such as a air conditioning system for example. For example, the gases are taken from a gas generator of a turbine engine.
    The acoustic treatment gas ejection duct 8 comprises at least one mechanical member 11. This mechanical member 11 is acoustically treated to reduce the emission of noise during the exhaust of gas 200.
    For example, the sampling duct 9 comprises a bend 500 followed by a diffuser 502.
    In addition, the acoustic treatment gas ejection nozzle 10 is for example provided with a skirt 20. The skirt 20 is provided with a diverging member 21 secured to a flange 22. The flange is screwed to the engine 4 by example. Such a diverging member 21 may then represent a mechanical member 11 treated acoustically.
    The acoustic treatment gas ejection nozzle 10 is also provided with a central cone 15 which can represent a mechanical member 11 treated acoustically. This central cone comprises, for example, an outer convergent member 16 which surrounds an inner convergent member 17. The inner convergent member is then connected to the base of the outer convergent member 16.
    In addition, the acoustic treatment gas ejection nozzle 10 is also provided with a plurality of arms 25 each connecting the outer convergent member 16 of the central cone 15 to the diverging member 21 of the skirt 20. At least one arm 25 extends for example radially and may represent a mechanical member 11 treated acoustically.
    FIG. 2 shows a three-dimensional view of an acoustic treatment gas ejection duct 8 of acoustic treatment gas ejection nozzle type 10 according to the invention.
    Regardless of the nature of the acoustical treatment gas ejection duct 8, each acoustically treated mechanical member has an innovative acoustic wall. Such an acoustic wall 30 has an outer skin 35 and an inner skin 40, the inner skin 40 being necessarily opposite a passage 201 which is traversed by the gases 200. This inner skin 40 then has perforations 41 intended to be traversed. by an acoustic wave generated by the circulation of gases 200.
    The acoustic treatment gas ejection duct 8 and in particular the acoustic wall 30 may be made from NiCr19Fe19Nb5Mo3 material. Other materials are possible
    FIG. 3 presents a three-dimensional view of an acoustic wall 30.
    As indicated above, the acoustic wall 30 has an outer skin 35 and an inner skin 40.
    The outer skin 35 and the inner skin 40 may locally form a single skin. Nevertheless, the outer skin 35 and the inner skin 40 are also separated at least locally by an internal space 50. Therefore, a mesh 60 is arranged in this space 50.
    This mesh 60 defines cavities that are not visible in FIG. 3, each of which represents a Helmholtz resonator. Therefore, each cavity communicates with a passage 201 through which the gas passes through perforations 41.
    In order to allow the manufacture of the acoustic treatment gas ejection duct 8 from bottom to top by laser sintering, the mesh 60 of an acoustic wall extends in elevation in a direction known as the "production direction 301". This manufacturing direction 301 has an acute angle 302 greater than or equal to a predetermined angle with a horizontal plane 300. This horizontal plane represents the plane on which the first layer of powder is deposited during manufacture.
    Likewise, the inner skin 40 as well as the outer skin 35 each have an acute inclination 303 greater than or equal to this predetermined angle with the horizontal plane 300.
    In general and with reference to FIG. 4, any surface of the acoustic treatment gas ejection duct 8 extends from bottom to top in a direction having at least said predetermined angle with the horizontal plane 300.
    Indeed, when a layer of powder called "upper layer 411" is deposited on a layer called "lower layer 412", the upper layer 411 may collapse under its own weight according to arrow 413. However, the plaintiff notes that from a predetermined angle, the upper layer 411 can remain on the lower layer 412.
    Such a predetermined angle is for example equal to 45 degrees. Consequently, each of the outer and inner skins 40 comprises a tangent 401 arranged in a plane perpendicular to the horizontal plane 300. This tangent 401 then has an inclination 303 with respect to the horizontal plane 300 greater than or equal to the predetermined angle.
    Figure 5 shows an exploded view of an acoustic wall 30 for viewing the internal mesh 60.
    This mesh 60 thus has a plurality of cavities 61 which extend transversely of the outer skin 35 towards the inner skin 40.
    Each cavity 61 is delimited by six substantially plane faces.
    Thus, a cavity is delimited in elevation in a direction in elevation Z on the one hand by a partition 62 called "upper partition 63" and on the other hand by a partition 62 called "lower partition 64". The upper partition 63 is parallel to the lower partition 64.
    In addition, the cavity 61 is delimited transversely in a transverse direction Y on the one hand by a partition 62 called "left lateral partition 65" and, on the other hand, by a partition 62 called "right lateral partition 66". The left lateral partition 65 is parallel to the right lateral partition 66. In addition, the left lateral partition 65 and the right lateral partition 66 each extend in elevation from bottom to top, according to the direction of manufacture of the wall, the lower partition 64 to the upper partition 63.
    Finally, each cavity 61 is delimited longitudinally in a longitudinal direction X on the one hand by a flat face represented by a non-perforated portion 67 of the outer skin 35 and, on the other hand, by a flat face represented by a perforated portion. 68 of the inner skin 40.
    Each cavity then has by construction an innovative parallelepiped shape.
    In particular, each partition can be rectangular.
    However, each cavity 61 may have a non-rectangular parallelepiped shape. The lower partition 64 and the upper partition 63 each have an acute angulation 304 different from 90 degrees with the left lateral partition 65 or the right lateral partition 66.
    In addition, the cavities 61 of a mesh 60 are arranged in elevation one above the other, and transversely next to each other.
    As a result, two transversely adjacent cavities 601, 602 have a common side wall 603.
    Similarly, two adjacent cavities in elevation are arranged one above the other. A so-called cavity "top cavity 604" then overhangs a cavity called "bottom cavity 605". Therefore, two adjacent cavities have a common partition 606 which represents an upper partition for the lower cavity 605 and a lower partition for the upper cavity 604.
    In addition, the left side partition of the top cavity is located in alignment with the left side partition of the bottom cavity, and the right side partition of the top cavity is located in alignment with the right side partition. of the cavity below. Lateral partitions of a row of cavities arranged one above the other thus form a flat plate extending in elevation.
    Moreover, each cavity has by construction an innovative parallelepiped shape.
    To allow the evacuation of residues of a powder during the manufacture of the acoustic wall, at least one partition 62 of a cavity 61 has a drainage opening 70 opening out of this cavity 61.
    For example, each side wall 65, 66 has a drainage opening 70. This drainage opening 70 then opens onto either another cavity or a part of the space 50 which is not filled by a mesh.
    Similarly, at least one skin may be provided with at least one drainage orifice 71. Preferably, the outer skin of an acoustic wall is provided with at least one drainage orifice, this outer skin being not contact with the acoustic wave.
    Furthermore, all the lights made in the sound treatment gas ejection duct 8 can be accurately sized. These lights include the perforations, openings, and orifices previously described.
    Thus, each perforation 41, or even each drainage opening and each drainage orifice has a diameter 42 less than or equal to four millimeters.
    Indeed, the Applicant notes that a larger diameter can induce the undue collapse of a powder layer during a laser sintering process. Therefore, each cavity can communicate fluidly with a passage 201 which is traversed by the gas through four perforations with a diameter less than or equal to 1.5 millimeters.
    On the other hand, the inner and outer skins 35 may have small thicknesses that can nevertheless be obtained by laser sintering. Therefore, at least one of the inner skin 40 and 35 outer skin optionally has a thickness ep less than one millimeter.
    Figures 6 to 9 illustrate an acoustic treatment gas ejection nozzle according to the invention provided with a skirt, a central cone and arms.
    Referring to Figure 6, the skirt 20 may comprise a plurality of meshes 60 extending in a manufacturing direction and from bottom to top of a base 23 to an apex 24. The diverging member 21 of the skirt s' extends in a manufacturing direction and from bottom to top of a base 23 to a top 24. This diverging member 21 may have between the base 23 and its top 24 a periodic form forming folds. This periodic shape comprises a repeated section multiple times, this section successively comprising an inner arch 211, a first side 212, an outer arch 213 and a second side 214. The inner arch 211 has a convex face with respect to an axis of symmetry AX of the divergent member 21, while the outer arch 213 has a concave face with respect to this axis of symmetry AX. Therefore, the first side 212 away from the axis of symmetry AX extending from the inner arch 211 to the outer arch 213, while the second side 214 is close to the axis of symmetry AX in extending from the second arch 213. Therefore, at least mesh 60 may be disposed at the inner arch 211, the first side 212, the outer arch 213 and the second side 214.
    In addition, FIG. 6 illustrates the possibility of locally fusing the outer skin and the inner skin, in particular at the base 23 and / or at the top 24 of the diverging member 21.
    FIG. 7 illustrates an arm 25 of the acoustic treatment gas ejection nozzle 10. This arm extends from bottom to top in a manufacturing direction of a foot 26 towards an end 27, the foot 26 and the end 27 that can be secured to the central cone 15 and to the skirt 20 of the acoustic treatment gas ejection nozzle 10.
    The arm may then comprise an acoustic wall 30 of the type described above.
    Figures 8 and 9 illustrate a central cone 15.
    With reference to FIG. 9, the external convergent member 16 may comprise an annular acoustic wall 30 according to the invention. The inner convergent member 17 may optionally only have a skin forming an open cone at its top. This skin has the required inclination relative to the horizontal plane 300, or even at least one drainage orifice 71.
    FIG. 10 illustrates a sampling duct 9 according to the invention. This sampling duct 9 comprises a bend 500 followed by a diffuser 502. The bend 500 and / or the diffuser 502 may comprise acoustic walls 3 of the type described above.
    Optionally, the elbow 500 and / or the diffuser 502 are attached to a fastening flange 501.
    FIG. 11 illustrates a manufacturing device 100 by laser sintering making it possible to implement the method according to the invention.
    This manufacturing device 100 comprises a table 101 or equivalent. This table 101 delimits a tray 102. The tray 102 is open at its top but has a movable bottom. This moving bottom is obtained by means of a plate 110 moving in elevation along the double arrow 103.
    In addition, the manufacturing device 100 comprises a roller 104 rolling on the table 101 along the double arrow 105. This roller 104 makes it possible to deposit successive layers of powder in the tray 102.
    Furthermore, the manufacturing device 100 comprises a laser system 106 capable of solidifying the powder deposited in the tray in predetermined areas. This laser system 106 then has a laser emitter 107 emitting a laser beam. In addition, the laser system 106 has an optical system 108 capable of directing the laser beam into the required areas.
    The manufacturing device 100 also has a not shown electronic system for controlling the plate 110, the roller 104 and the laser system 106.
    According to the method of the invention, the sound treatment gas ejection duct 8 is produced layer by layer by repetition of the following steps: - removal of a layer of material by the roller 104 in the tank 102, - local consolidation of the layer by the laser system, - descent of the plate 110 supporting the acoustical treatment gas duct 10 during manufacture to deposit the next layer.
    Naturally, the present invention is subject to many variations as to its implementation. Although several embodiments have been described, it is well understood that it is not conceivable to exhaustively identify all the possible modes. It is of course conceivable to replace a means described by equivalent means without departing from the scope of the present invention.
    权利要求:
    Claims (16)
    [1" id="c-fr-0001]
    1. Acoustic treatment gas ejection duct (8) provided with at least one mechanical member (11), said mechanical member (11) having at least one so-called "acoustic wall (30)" wall intended to be in contact with said gas (200), said acoustic wall (30) comprising an inner skin (40) and an outer skin (35) which are at least partially separated by a gap (50), said acoustic wall (30) comprising at least one mesh (60) internally arranged in said space (50), said mesh (60) defining a plurality of cavities (61), each cavity (61) extending in thickness from the inner skin (40) to the outer skin (35); ), said inner skin (40) being intended to be in contact with said gas (20), said inner skin (40) having perforations (41), each cavity (61) communicating with at least one perforation (41), characterized in that each cavity (61) has a parallelepipedal shape, the inner skin ( 40) as well as the outer skin (35) and each mesh (60) extending in elevation from a horizontal plane (300), each mesh (60) extending in elevation in a direction called "direction of manufacture (301) "having an acute angle (302) greater than or equal to a predetermined angle with said horizontal plane (300), the inner skin (40) and the outer skin (35) each having a higher acute inclination (303) or equal to said predetermined angle with said horizontal plane (300).
    [2" id="c-fr-0002]
    An acoustic treatment gas ejection duct according to claim 1, characterized in that said predetermined angle is equal to 45 degrees.
    [3" id="c-fr-0003]
    3. An acoustic treatment gas ejection duct according to any one of claims 1 to 2, characterized in that each tangent (401) to one of said skins (35, 40) which is arranged in a perpendicular plane (400) said horizontal plane (300) has a said inclination (303).
    [4" id="c-fr-0004]
    4. An acoustic treatment gas ejection duct according to any one of claims 1 to 3, characterized in that said cavities (61) of a mesh (60) are arranged in elevation (Z) above each other. others, and transversely (Y) next to each other.
    [5" id="c-fr-0005]
    5. An acoustic treatment gas ejection duct according to any one of claims 1 to 4, characterized in that each cavity (61) is delimited in elevation by a partition (62) called "upper partition (63)" and a partition (62) called "lower partition (64)", each cavity (61) being delimited transversely by a partition (62) called "left side partition (65)" and a partition (62) called "right side partition (66)" ) Which each extend in elevation from the lower partition (64) to the upper partition (63), each cavity (61) being delimited transversely by a non-perforated portion (67) of the outer skin (35) and a perforated portion (68) of the inner skin (40).
    [6" id="c-fr-0006]
    6. Acoustic treatment gas ejection duct according to claim 5, characterized in that each of said partitions (62) is rectangular.
    [7" id="c-fr-0007]
    7. An acoustic treatment gas ejection duct according to any one of claims 5 to 6, characterized in that each cavity (61) has a non-rectangular parallelepiped shape, the lower partition (64) and the upper partition ( 63) each having an acute angulation (304) different from 90 degrees with the left lateral partition (65) or the right lateral partition (66).
    [8" id="c-fr-0008]
    8. An acoustic treatment gas ejection duct according to any one of claims 5 to 7, characterized in that at least one said partition (62) of a cavity (61) has a drainage opening (70) opening out of this cavity (61).
    [9" id="c-fr-0009]
    9. An acoustic treatment gas ejection duct according to any one of claims 1 to 8, characterized in that said acoustic wall (30) is made from NiCr19Fe19Nb5Mo3 material.
    [10" id="c-fr-0010]
    10. An acoustic treatment gas ejection duct according to any one of claims 1 to 9, characterized in that at least one of said inner skins (40) and outer (35) has a thickness (ep) less than one millimeter.
    [11" id="c-fr-0011]
    11. An acoustic treatment gas ejection duct according to any one of claims 1 to 10, characterized in that each perforation (41) has a diameter (42) less than or equal to four millimeters.
    [12" id="c-fr-0012]
    12. An acoustic treatment gas ejection duct according to any one of claims 1 to 11, characterized in that each cavity (61) communicates with at least four perforations (41) with a maximum diameter (42) of 1.5 millimeters.
    [13" id="c-fr-0013]
    13. An acoustic treatment gas ejection duct according to any one of claims 1 to 12, characterized in that, said acoustic treatment gas ejection duct (8) being a nozzle (10), each mechanical member (11) is to be selected from a list comprising a skirt (20), a central cone (15), and an arm (25) connecting said skirt (20) to the central cone (15).
    [14" id="c-fr-0014]
    14. Acoustic treatment gas ejection duct according to any one of claims 1 to 13, characterized in that said acoustic treatment gas ejection duct (10) comprises at least one skin provided with at least one drainage port (71).
    [15" id="c-fr-0015]
    15. Aircraft (1) provided with an acoustic treatment gas ejection duct (8), characterized in that said acoustic treatment gas ejection duct (8) is according to any one of claims 1 to 14.
    [16" id="c-fr-0016]
    16. A method of manufacturing an acoustic treatment gas ejection duct (8) according to any one of claims 1 to 14, wherein said acoustic treatment gas ejection duct (8) is realized. by implementing a laser sintering method, said acoustic treatment gas ejection duct (8) being carried out layer by layer by repetition of the following steps: - depositing a layer of material by a roller (104), - local consolidation of said layer, - descent of a plate (110) supporting the acoustic treatment gas ejection duct (8) during manufacture.
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3159522B1|2018-12-12|A gas ejection duct with acoustic treatment, an aircraft, and a method of fabricating such a duct
    EP2953130B1|2017-05-17|Acoustically attenuating sandwich panel constructions
    EP1533787B1|2007-05-09|Sound insulation panel containing balls and method for producing it
    EP2071561B1|2021-02-03|Absorbent structure for reducing the noise generated in particular by a rotor and fairing comprising such a structure
    FR3019775A1|2015-10-16|
    EP3489487B1|2021-02-17|Acoustic attenuation panel for aircraft
    FR2750453A1|1998-01-02|NOISE REDUCING PANEL, METHOD FOR MANUFACTURING SAME, AND MOTOR COMPRISING SAME
    EP1902948B1|2016-08-24|Gas turbine helicopter engine with reduced sound emissions due to acoustic treatment of a jet pump
    EP3660295B1|2021-01-13|Process for producing an acoustic element of an acoustic absorption structure from at least one sheet of material
    WO2014114893A1|2014-07-31|Acoustic attenuation panel with a honeycomb core
    EP3696090B1|2021-05-19|Method for manufacturing an acoustic absorption structure including a skin forming a plurality of enclosures, acoustic absorption structure obtained according to said method and aircraft comprising said acoustic absorption structure
    WO2009133009A1|2009-11-05|Improved acoustic panel
    FR3099963A1|2021-02-19|Acoustic element with double enclosure and reduced bulk, in particular for aircraft acoustic panels
    EP3720711A1|2020-10-14|Method for in situ additive manufacturing of a coating on a turbomachine casing
    EP3552951A1|2019-10-16|Acoustic attenuation panel for aircraft having combined acoustic absorption properties
    FR3105553A1|2021-06-25|Acoustic treatment system with at least two degrees of freedom comprising a quarter-wave coating allowing the passage of acoustic waves in a cavity-mode resonator
    EP3628461A1|2020-04-01|Method for manufacturing two soundproofing panels in a single mould and mould for producing two soundproofing panels
    EP3916717A1|2021-12-01|Honeycomb soundproofing structure including a diaphragm provided with a tube configured to process different acoustic frequencies, method for manufacturing such a honeycomb soundproofing structure, and associated tool
    EP3491227B1|2020-09-02|Acoustic panel for a turbomachine and method for the production thereof
    CA2988229A1|2019-06-06|In situ additive fabrication process for a coating on a turbine engine casing
    CA3126511A1|2020-08-13|Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
    CA3126629A1|2020-08-13|Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
    CA3126505A1|2020-08-13|Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
    EP3850616A1|2021-07-21|Acoustic treatment panel for a turbojet engine
    FR3111002A1|2021-12-03|Manufacturing process of a soundproofing honeycomb structure including a diaphragm, and soundproofing honeycomb structure obtained
    同族专利:
    公开号 | 公开日
    US20170107909A1|2017-04-20|
    US10125688B2|2018-11-13|
    EP3159522B1|2018-12-12|
    EP3159522A1|2017-04-26|
    FR3042541B1|2019-08-09|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4240252A|1978-01-19|1980-12-23|General Electric Company|Acoustically-treated mixer for a mixed flow gas turbine engine|
    US4452335A|1982-05-03|1984-06-05|United Technologies Corporation|Sound absorbing structure for a gas turbine engine|
    EP1391597A2|2002-08-14|2004-02-25|Sener, Ingenieria Y Sistemas, S.A.|Noise reduction conduit for static components in aircraft engines|
    EP1998003A2|2007-05-29|2008-12-03|United Technologies Corporation|Noise control cassette for a gas turbine engine|
    WO2015098148A1|2013-12-26|2015-07-02|三菱重工業株式会社|Muffler and muffling apparatus with same|
    US3542152A|1968-04-08|1970-11-24|Gen Electric|Sound suppression panel|
    GB2188397B|1984-09-13|1988-12-29|Rolls Royce|A low drag surface construction|
    US7784283B2|2006-05-03|2010-08-31|Rohr, Inc.|Sound-absorbing exhaust nozzle center plug|
    FR2929336B1|2008-03-31|2012-06-01|Airbus France|JET DEVICE NOISE REDUCTION PLATES GENERATED BY AN AIRCRAFT REACTOR|
    DE102008051241B4|2008-10-10|2011-06-16|Airbus Operations Gmbh|Muffler for an auxiliary engine of an aircraft|
    GB0820597D0|2008-11-11|2008-12-17|Rolls Royce Plc|A noise reduction device|
    EP2700068A4|2011-04-20|2016-01-13|Dresser Rand Co|Multi-degree of freedom resonator array|
    FR2982844B1|2011-11-18|2014-03-14|Eurocopter France|CABLE DISCONNECT DEVICE, AND AIRCRAFT|
    CA2810956A1|2012-03-28|2013-09-28|Magellan Aerospace, Winnipeg A Division Of Magell|Cable cutting device for aircraft|
    GB201301702D0|2013-01-31|2013-03-20|Rolls Royce Plc|Exhaust cone|
    EP2865947B1|2013-10-28|2017-08-23|Ansaldo Energia Switzerland AG|Damper for gas turbine|
    GB201319256D0|2013-10-31|2013-12-18|Rolls Royce Plc|Gas turbine engine|
    US9592918B2|2014-06-23|2017-03-14|Rohr, Inc.|Acoustic liner|
    FR3031142B1|2014-12-24|2017-03-24|Aircelle Sa|ACOUSTICAL ATTENUATION PANEL FOR TURBOREACTOR NACELLE|US10436118B2|2017-06-19|2019-10-08|Rohr, Inc.|Acoustic panel with folding chamber|
    FR3074227B1|2017-11-28|2020-02-28|Airbus Operations|INTERNAL STRUCTURE OF A PRIMARY EJECTION DUCT|
    US11034460B2|2017-12-08|2021-06-15|The Boeing Company|Additively manufactured septa for acoustic panels|
    FR3095671A1|2019-04-30|2020-11-06|Safran Aircraft Engines|Integration of a fan floating damper in a crankcase|
    法律状态:
    2016-10-20| PLFP| Fee payment|Year of fee payment: 2 |
    2017-04-21| PLSC| Publication of the preliminary search report|Effective date: 20170421 |
    2017-10-24| PLFP| Fee payment|Year of fee payment: 3 |
    2018-10-22| PLFP| Fee payment|Year of fee payment: 4 |
    2019-10-28| PLFP| Fee payment|Year of fee payment: 5 |
    2020-10-21| PLFP| Fee payment|Year of fee payment: 6 |
    2021-10-21| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1502204A|FR3042541B1|2015-10-20|2015-10-20|ACOUSTICALLY PROCESSED GAS EJECTION DUCT, AIRCRAFT AND METHOD OF MANUFACTURING SUCH A CONDUIT|
    FR1502204|2015-10-20|FR1502204A| FR3042541B1|2015-10-20|2015-10-20|ACOUSTICALLY PROCESSED GAS EJECTION DUCT, AIRCRAFT AND METHOD OF MANUFACTURING SUCH A CONDUIT|
    EP16191420.5A| EP3159522B1|2015-10-20|2016-09-29|A gas ejection duct with acoustic treatment, an aircraft, and a method of fabricating such a duct|
    US15/298,550| US10125688B2|2015-10-20|2016-10-20|Gas ejection duct with acoustic treatment, an aircraft, and a method of fabricating such a duct|
    [返回顶部]