• 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 device comprises: - a fixed frame (24); - A table (26) deployable relative to the frame (24) between a retracted position and an extended horizontal position; - A mechanism (90) for guiding the movement of the table (26) relative to the frame (24) between the retracted position and the extended horizontal position. The guiding mechanism (90) defines at least one support point (123) of the table (26) during its passage from the retracted position to the deployed horizontal position, the support point (123) presenting a position generally. invariant with respect to the frame (24), the table (26) being configured to pivot on the fulcrum (123) away laterally from the fulcrum (123), by sliding on the point of support (123), to the deployed position.
    公开号:FR3032177A1
    申请号:FR1500207
    申请日:2015-02-04
    公开日:2016-08-05
    发明作者:Nicolas Hance
    申请人:Dassault Aviation SA；
    IPC主号:
    专利说明:

    [0001] BACKGROUND OF THE INVENTION The present invention relates to a support device for an interior assembly assembly of an aircraft cabin, comprising: - a frame fixed; - A table deployable relative to the frame between a retracted position and a deployed horizontal position; a mechanism for guiding the movement of the table relative to the frame between the retracted position and the extended horizontal position.
    [0002] Such a set of arrangements is intended to be mounted in an aircraft cabin to participate in the comfort of the occupants of the cabin. During a cruise flight, the passengers of an aircraft wish to have a table to perform various activities, such as working, eating, or more generally to support various objects, such as books, portable electronic devices. .. For safety reasons, aircraft certification requires that each table in the aircraft be retracted during certain phases of flight, including take-off and landing. In some cases also, the passenger may wish for his own comfort that the table is retracted, for example to deploy a seat to lie down. Known interior arrangement sets therefore include a side console defining a receiving housing of the table and a retractable table in the side console. In these assemblies, a cover mounted on the console closes the housing upward when the table is retracted, which provides a pleasant interior appearance. To deploy the table, the lid is tilted to the open position, and remains in the open position once the table is deployed. The table then rests on the upper plate of the side console, projecting relative to the upper plate so as to provide some rigidity to the table thus deployed especially when a force is exerted on it. Such a set does not give full satisfaction on the aesthetic level, when the table is deployed. The lid remains open in this configuration and protrudes above the table top. This is unattractive and limits the accessibility to the rear of the support plate, including the object support compartments that may be present at the rear of the support plate.
    [0003] In addition, the table top is not flush with the top plate of the side console. In addition, the hinges of the table deployment mechanism are visible to the user. An object of the invention is therefore to provide a support device comprising a deployable table for a set of interior aircraft interior, which is compact and aesthetic, while having a robust and rigid deployment kinematics. To this end, the subject of the invention is a device of the aforementioned type, characterized in that the guiding mechanism defines at least one point of support of the table during its passage from the retracted position to the deployed horizontal position, the fulcrum having a generally invariant position relative to the frame, the table being configured to pivot on the fulcrum by deviating laterally from the fulcrum, by sliding on the support point, until in the deployed position. The device according to the invention may comprise one or more of the following characteristics, taken separately or in any technically possible combination: the or each point of support projects upwards with respect to the frame. - The guide mechanism comprises a support member rotatably mounted about a fixed axis relative to the frame, the fulcrum being defined on the support member. - The table has a sliding guide path of the table on the fulcrum. - The support point cooperates with the guide path. - The guide mechanism comprises a rail inserted into the table, the rail defining the guide path. the table is adapted to be applied on the fulcrum from the retracted position to the extended horizontal position, the guiding mechanism being configured so that the table follows a single and reproducible trajectory from the retracted position to the horizontal position deployed. - The frame comprises at least one substantially vertical leg, the guide mechanism comprising at least one guide path of the table along the leg. - The guide path is formed through the leg, the guide mechanism comprising a guide member movable together with the table, the guide member being mounted in the guide path. - The guide mechanism comprises a rack, the guide member comprising a toothed wheel. - The table comprises a carriage, the guide member being rotatably mounted in the carriage. - the upper end of the guideway is offset laterally with respect to a vertical axis passing through the fulcrum, the guideway being inclined relative to the vertical axis passing through the fulcrum or being parallel to the vertical axis passing through the fulcrum. - The guide mechanism comprises at least one elastic biasing member adapted to drive the table upwards relative to the frame. - The elastic biasing member is mounted in the carriage between the guide member and the carriage. The subject of the invention is also a set of interior fittings of an aircraft cabin, comprising: a device as defined above, a console delimiting a receiving compartment of the table opening through a deployment opening, the table being deployable through the deployment opening between the retracted position disposed in the receiving housing and an extended horizontal position; and a cover mounted on the console, the cover being movable between an open configuration of passage of the table and a closed configuration of closing the deployment opening. The assembly according to the invention may comprise one or more of the following characteristics, taken separately or in any technically possible combination: the lid in the closed configuration and the console delimit between them a passage slot, suitable for receiving the table in the extended horizontal position, the assembly comprising a closing shutter of the passage slot, movable by the table from an active configuration of closing the passage slot to an erased configuration of release of the passage slot during the passage of the table from its retracted position to its deployed position; - At least one elastic return mechanism of the shutter in its active configuration. - the shutter shutter in the active shutter configuration is located above the shutter shutter in the erased configuration. - The table is adapted to rest on the shutter when it moves from the retracted position to the extended horizontal position to push down the shutter in the erased configuration under the effect of the weight of the table. - The shutter and / or the table has at least one sliding member of the table on the shutter flap. - The shutter is movable in translation between the active closure configuration and the erased configuration. - The console has a fixed upper edge, defining downwardly the passage slot, the table resting on sliding members located on the shutter in the extended horizontal position, preferably without contact with the upper edge of the console. - The lid in the closed configuration is disposed above an upper surface of the table when the table occupies the extended horizontal position, the lid closing the receiving housing upwards. - The cover in the closed configuration is disposed above the shutter when the table occupies the retracted position, the cover closing the receiving housing upwards. - The console has a top object bearing surface, an upper wall of the lid in its closed configuration flush with the upper bearing surface. - The table has a base panel and an additional panel hinged to the base panel, the additional panel being folded over the base panel during the passage of the table from the retracted position to the extended horizontal position. The invention also relates to a method of interior layout of an aircraft cabin comprising the following steps: - providing a device as defined above, the table occupying its retracted position; - Passing the table from its retracted position to its deployed horizontal position, the table resting on the fulcrum and pivoting around the fulcrum away laterally of the support point by sliding on the point d support to the deployed position. The invention will be better understood on reading the description which will follow, given solely by way of example, and with reference to the appended drawings, in which: FIG. 1 is a perspective view, partly from above, a first set of interior arrangement according to the invention, the table occupying an extended horizontal position; - Figure 2 is a partial view, taken in section along a vertical plane II of the interior arrangement of Figure 1; - Figure 3 is a view similar to Figure 2, the table occupying a retracted position; - Figure 4 is a perspective view from above similar to Figure 3; - Figure 5 is a perspective view from above of the assembly of Figure 1, during the deployment of the table; - Figure 6 is a view of the support device comprising the table and the guide frame of the table during deployment of the table; - Figure 7 is a perspective view in partial section along a vertical plane VII of the support device of Figure 6, in the extended horizontal position of the table; - Figure 8 is a side view and partially in section along the vertical plane VII of the support device of Figure 6, in the extended horizontal position of the table. In what follows, the terms "backward" and "before" are generally relative to the deployment of the table. The term "back" preferably means closer to the table in its retracted position, while the term "front" is understood to be closer to the table in its deployed position.
    [0004] An interior fitting assembly 10 of a cabin 12 of an aircraft according to the invention is illustrated in FIGS. 1 to 8. The cabin 12 of the aircraft is delimited laterally by the fuselage 14 and downwards by a floor 16. It extends here along a longitudinal axis A-A '. The arrangement of arrangement 10 is mounted in the cabin 12 to be accessible to the occupants of the cabin 12. It comprises a console 20, and a support device 22, visible in FIG. 6, including in particular a frame 24 housed in the console 20 and a table 26 deployable between a retracted position in the console 20 and an extended horizontal position, visible in Figure 1. The arrangement of arrangement 10 further comprises a cover 28 for masking the support device 22 in the position retracted from the table 26, and a shutter 30 erasable additional shutter, mounted between the bracket 20 and the cover 28, the structure and function will be described in detail below. In the example shown in Figure 1, the bracket 20 extends along a horizontal main axis BB 'advantageously substantially parallel to the longitudinal axis of cabin A-A', along the fuselage 14. Other configurations of 20 console orientation are also possible. The bracket 20 includes a substantially vertically extending, curved flank 40 and an upper support plate 42 defining a substantially horizontal object support surface 43.
    [0005] The console 20 delimits a housing 44 for receiving the support device 22 which opens here upwardly through a deployment opening 46, visible in FIG. 5. With reference to FIG. 3, the sidewall 40 comprises an external lining of FIG. 48 and an inner support 50 for guiding the shutter 30, disposed in the vicinity of an upper edge 52 of the bracket 20, which here has a tapered shape upwards. The inner support 50 is disposed in the housing 44, at the rear of the seal 48. It defines a cavity 54 for sliding the shutter shutter 30. The upper plate 42 defines, at the rear of the housing 44, a plurality object receiving compartments 56, some of which are closed by a shutter. It has two lateral support tongues 58, extending on either side of the deployment aperture 46, around the cover 28. The receiving housing 44 is delimited laterally by the bracket 20. It is delimited towards the high by the support plate 42, at the rear of the deployment opening 46, on the side of the fuselage 14 in Figure 1. It extends substantially vertically from the floor 16 to the deployment opening 46. The lid 28 is intended to close up the housing 44 at the level of the deployment opening 46, in the retracted position of the table 26 and also in the extended horizontal position of the table 26.
    [0006] The cover 28 is movable between an open configuration of passage of the table 26 and a closed configuration of closing the deployment opening 46. In this example, the cover 28 is articulated on the console 20 around an axis of joint. Advantageously, the hinge axis is parallel to the main axis B-B '. It extends to the rear of the deployment opening 46.
    [0007] The cover 28 has a masking top wall 60, and in this example, two lateral feet 62, intended to be positioned around the table 26 in its extended position. In the closed configuration, the upper wall 60 is flush with the upper surface 43 of the support plate 42. It is disposed above the table 26. It has a lower local thickness than the table 26 in the region in which it rests . The feet 62 are placed in abutment on the upper edge 52 of the bracket 20. In this configuration, the cover 28 and the bracket 20 delimit between them a horizontal slot 64 for passage of the table 26, the outline of which is visible in FIG. 4.
    [0008] The slot 64 is delimited downwards by the upper edge 52, upwards by the upper wall 60 of the cover 28 and on the sides by the feet 62.
    [0009] The housing 44 is then closed upwards by the cover 28, in particular at the deployment opening 46, with the exception of the slot 64. As will be seen below, the table 26 is engaged through the slot 64 in the extended horizontal position. The shutter 30 closes the slot 64 in the retracted position of the table 26. In the open configuration, visible in FIG. 5, the cover 28 has been lifted and tilted backward to release the deployment opening 46 and allow access to housing. The shutter 30 is mounted vertically movable on the console 20 between an active configuration of closing the slot 64, constituting its rest configuration, visible in Figure 3, and an erased configuration of release of the slot 64, visible on Figure 2. The arrangement of arrangement 10 comprises at least one elastic biasing mechanism 70 of the shutter 30 to its active configuration of closing the slot 64, preferably at least two parallel mechanisms 70 resilient biasing of the shutter 30 to its configuration The flap 30 includes an appearance rod 74 adapted to protrude into the passage slot 64, and advantageously at least one sliding member 76 of the table 26 on the rod 74, visible on the FIG. 5. The rod 74 is guided in translation along a vertical axis in the cavity 54 of the inner support 50. The displacement of the shutter shutter 30 between the active configuration closing and the erased configuration is therefore carried out exclusively in translation along this axis. The flap 30 thus forms an erasable shutter guillotine of the slot 64. The appearance rod 74 has a tapered shape which extends the shape of the upper edge 52 of the bracket 20. It has a substantially horizontal upper edge 78. The shutter 30 comprises at least one sliding member 76. In this example, the shutter 30 comprises two sliding members 76 spaced along the appearance rod 74.
    [0010] Each slide member 76 is mounted in the appearance rod 74 projecting from the upper edge 78. In this example, each slide member 76 is formed by a rotatively mounted wheel in the appearance rod 74. in Figure 2 and Figure 3, each elastic biasing mechanism 70 comprises a movable rod 79 for moving the flap 30, a base 80 for guiding the rod 79, fixedly mounted on the bracket 20, and a spring 81 interposed between the console 20 and the flap 30, advantageously between the base 80 and the rod 79.
    [0011] The base 80 comprises a bushing carried by the inner support 50 and guide members of the rod 79 in vertical translation in the bushing. The rod 79 is mounted movably in vertical translation in the base 80. It comprises a high limit stop limiting its stroke upwards. It has a head 82 mounted in a housing 83 of the rod 74. The spring 81 is interposed between the rod 79 and the base 80. It permanently urges the rod 79 upwards. In the active closure configuration, visible in FIG. 3, the shutter shutter 30 protrudes vertically into the slot 64. The strip 74 is flush with the trim 48 of the bracket 20 at the upper edge 52. The upper edge 78 of the rod 74 is disposed under the upper wall 60 of the masking cover 28 in the vicinity of this wall 60, without contact between the sliding members 76 and the wall 60. As illustrated in FIG. 4, the slot 64 and the housing 44 are then completely closed upwards by the cover 28 and the shutter 30 in the slot 64, above the console 20. The external appearance of the arrangement of arrangement 10 is very satisfactory. In the erased configuration, when the table 26 is placed in the slot 64, the weight of the table 26 pushes down the rod 74 against the elastic biasing mechanism 70. The upper edge 78 of the rod is then lowered substantially at the same level as the upper edge 52 of the console 20. The table 22 is disposed between the upper horizontal wall 60 of the masking cover 28 in the closed configuration and the upper edge 78 of the shutter 30, providing a very external appearance. satisfactory.
    [0012] As indicated above, and with reference to FIG. 6, the support device 22 comprises the frame 24 and the table 26 mounted to move on the frame 24 between the retracted position and the deployed position. The support device 22 comprises a mechanism 90 for guiding the movement of the table 26 relative to the frame 24, adapted to guide the table 26 on a single path relative to the frame 24 between the retracted position and the deployed position. The frame 24 is completely received in the receiving housing 44 to be masked by the masking cover 28 in the retracted position and in the extended horizontal position.
    [0013] As illustrated in FIG. 6, the frame 24 comprises two parallel legs 92, placed on either side of the table 26, and at least one upper cross-member 94 for supporting the table 26, connecting the two legs 92. advantageously comprises at least one lower transverse stiffening cross member 96 connecting the two legs 92. Each leg 92 here has a lower region 95 thinned towards the rear to limit the bulk of the frame 90 and allow the passage of functional elements of the Aircraft such as cables at the rear of the frame 90. In this example, the frame 24 comprises two parallel bottom rails 96 mounted respectively at the front and rear of the legs 92. The upper cross member 94 extends horizontally, in the vicinity of the upper ends of the legs 92. The table 26 comprises at least one panel 100, 102 intended to extend horizontally in the extended horizontal position. It advantageously comprises a rear carriage 104 for connection with the frame 24. In this example, the table 26 comprises a base panel 100 and an additional panel 102 articulated on the base panel 100 about a horizontal axis between a folded position on the base panel 100, and an unfolded position from the base panel 100. The base panel 100 has a cross-section substantially complementary to that of the passage slot 64 to occupy the entire passage slot 64 in the horizontal position deployed. In the folded position, the additional panel 102 is applied above the base panel 100. In the unfolded position, the additional panel 102 horizontally extends the base panel 100 away from the frame 24. The rear carriage 104 is mounted sliding along the legs 92. It is connected to the base panel 100 via brackets 108. It is movable jointly in translation and in rotation with the base panel 100. The guiding mechanism 90 comprises an upper assembly 110 for guiding the base panel 100 relative to the frame 24, and a lateral assembly 112 for guiding the carriage 104 with respect to the frame 24.
    [0014] As illustrated in FIG. 6, the upper assembly 110 comprises at least one support member 114, integral with the frame 24, defining a support point 123 of the table 26 during its displacement between the retracted position and the deployed position. . It comprises, for each support member 114, a guide path 116 formed under the table 26, to receive the support member 114 and to maintain globally invariant the position of the support point 123.
    [0015] In this example, the upper assembly 110 comprises two separate support members 114 respectively received in two parallel guideways 116. Referring to Figure 7, each support member 114 comprises a bracket 120 attached to the crosspiece 94 and a rotary member 122, here a bronze ring rotatably mounted on the bracket 120. Each support member 114 defines a point 123 of support position of globally invariant position relative to the frame 24, on which the table 26 rests. The bearing point 123 is here located on the outer surface of the rotary element 122, away from the axis DD rotating the rotary element 122.
    [0016] By "globally invariant" is meant that the position of the fulcrum 123 of the table 26 on the support member 114 remains the same even when the rotary member 122 rotates about its axis DD 'and when the table 26 deviates from the support member 114. The rotary member 122 projects above the cross-member 94, so that the fulcrum 123 is situated above the cross-member 94.
    [0017] Each guide path 116 comprises a hollow rail 124 formed in the table 26, under the base panel 100, and at least one retaining blade 126 of the rotary member 122 of the support member 114, projecting against of hollow rail 124, to partially close down the hollow rail 124. Each guide path 116 extends along a deployment axis CC 'substantially perpendicular to the main axis B-B'. The rotary member 122 is slidable in the hollow rail 124 along the axis CC 'being retained between the blade 126 and the bottom of the rail 124. Thus, in each position of the table 26 from its retracted position towards its deployed position, at least one point of the table 26 remains disposed in abutment on the point of support 123 defined by the support member 114. The support members 114 define a pivot axis of the table 26 relative to the frame 24, which is here substantially parallel to the main axis B-B ', and the axis of rotation DD' so that the table 26 extends laterally with respect to the console 20. The table 26 follows a trajectory fixed and reproducible relative to the frame 24 from its retracted position to its deployed position and in the opposite direction, from its deployed position to its retracted position. The lateral guide assembly 112 comprises, for each leg 92, a guide member 130 carried by the carriage 104, a guide path 132 formed in the leg 92 along the latter, and a rack 133 adapted to cooperate with the guide member 130.
    [0018] The lateral guide assembly 112 further comprises an elastic biasing member 134, housed in the carriage 104, able to urge the table 26 away from its retracted position, and a mechanism 136 for retaining the table 26 in its seat. retracted position.
    [0019] In this example, each guide member 130 is rotatably mounted in the carriage 104 about an axis E-E 'parallel to the main axis B-B'. The guide members 130 are mounted at the opposite ends of a common shaft 135, received in the carriage 104. The shaft 125 is rotatably mounted about the axis EE 'relative to the carriage 104. The guideway 132 is arranged longitudinally in the leg 92 along an axis FF 'inclined rearwardly relative to a vertical axis passing through the fulcrum 123, an angle advantageously less than 10 °. The guideway 132 has an upper end offset laterally rearwardly relative to the vertical axis passing through the fulcrum 123. The inclination of the track 132 and the position of its upper end allow the table 26 to pivot about the fulcrum 123, while moving away from the fulcrum 123 along the deployment axis C-C '. The rack 133 extends along the track 132. The guide member 130 is formed by a toothed wheel adapted to cooperate with the rack 133 to allow the drive in translation of the table 26 along the axis F-F The elastic biasing member 134 is advantageously formed by a torsion spring interposed between each guide member 130 and the carriage 104, via the shaft 135. the carriage 104. The torsion of the spring increases when the table 26 occupies its retracted position and decreases during the displacement of the table 26 towards the extended position, under the effect of the rotation of each guide member 130 with respect to the carriage 104. Thus, the deployment of the elastic biasing member 134 is able to rotate the shaft 135 and jointly, the guide members 130. The guide members 130 then rise along the rack 133 in each v guide geometry 132 driving the carriage 104 and the panels 100, 102 of the table 26 upwards. The retaining mechanism 136 is adapted to selectively retain the table 26 in its retracted position against the bias of the member 134. It is adapted to be released by an occupant of the cabin 12 for example by actuating a command button.
    [0020] The operation of the arrangement 10 according to the invention will now be described. Initially, the table 26 occupies its retracted position in the receiving housing 44. The panels 100, 102 are folded over each other. The holding mechanism 136 is active. The rotary members 130 are located in a lower part of each guideway 132. The elastic biasing of the member 136 is maximum. In the retracted position, the table 26 is inserted into the frame, between the legs 92. It occupies a vertical or inclined position of an angle less than 10 ° relative to a vertical axis.
    [0021] As visible in Figure 3 or Figure 4, the cover 28 closes the receiving housing 44 upwards. The table 26 being disposed away from the shutter 30, it does not apply thereon. The shutter 30 is pushed up by each elastic biasing mechanism 70 and is maintained in its active configuration of masking the slot 64 in the vicinity of the wall 60 of the cover 28, without contact therewith. The external aesthetic appearance of the assembly 10 is therefore very satisfactory, since the receiving housing 44 is completely closed, on the one hand, by the cover 28 and on the other hand, by the shutter 30. When the user wishes deploy the table 26, it opens the lid 28 to switch to its open configuration. Then, it releases the holding mechanism 136. Under the effect of the elastic biasing member 134, the guide members 130 are rotated relative to the carriage 104 and up along the guideway 132, in cooperation with the rack 133. The table 26 then moves by a combined translational movement along the axis FF 'defined by the legs 92 and rotated about an axis defined by the points of support 123 on the organs of 114 support, to an intermediate position of input of the table 26, advantageously appearing a handle. During this movement, the rotary elements 122 of the support members 114 are rotated and slide in each rail 124 of a guide path 116.
    [0022] The table 26 therefore deviates laterally from the frame 24 by simultaneous sliding and pivoting. Each retaining blade 126 holds the support member 114 in the guide path 116, slaving the movement of the table 26 to a fixed and reproducible trajectory.
    [0023] In the inclined intermediate position of the table 26, the user advantageously grasps the base panel 100 and moves it progressively away from the frame 24 until it reaches the extended horizontal position. When the table 26 comes into contact with the shutter 30 at the sliding members 76 of the flap 30, it pushes down the shutter 30 under the effect of its weight (see Figure 5). The shutter 30 is guided in vertical translation relative to the console 20 through the mechanisms 70, in particular by sliding each rod 79 in the base 80 against the bias of the spring 81. The flap 30 s' progressively erases against the biasing mechanism 70, a simple translational movement, until reaching its erased configuration. This greatly simplifies the structure of the arrangement 10, since no complex mechanism is necessary to clear the shutter 30 when the slot 64 is to be released for the passage of the table 26.
    [0024] In the extended horizontal position, visible in Figure 8, the table 26 projects horizontally along the axis C-C 'perpendicular to the main axis B-B'. The carriage 104 is then disposed in the vicinity of the upper cross member 94. Referring to Figures 2 and 8, the table 26 rests in stable support on each support member 114, and on the sliding members 76 of the shutter 30 , through the base panel 100. The table 26 remains away from the upper edge 52 of the console 20. The user then closes the masking cover 28. The thinned upper wall region 60 is disposed of above the top surface of the base panel 100, producing an aesthetic effect similar to an outcrop.
    [0025] The base panel 100 is additionally received in the passage slot 64. Thus, the receiving housing 44 containing the frame 24 and the guiding mechanism 90 is completely hidden, which gives a very pleasant aesthetic appearance to the user. .
    [0026] The additional panel 102 can then be deployed to lengthen the length of the deployed table 26. The overall aesthetic appearance of the layout assembly 10 is therefore greatly improved, both in the retracted position of the table 26, and in the extended horizontal position of the table 26, which are the two main use positions. .
    [0027] This effect is obtained in a particularly simple manner, without having to provide complex mechanisms with complicated movements, including rotation.
    [0028] Furthermore, the deployment kinematics of the table 26 on the frame 24 is appropriately guided by the guiding mechanism 90, to ensure a reproducible trajectory and substantial rigidity during the deployment of the table 26. The rigidity is obtained in particular by the provision of support points 123 of globally invariant position of the table 26 on support members 114 mounted on the frame 24, and by the maintenance of these support members 114 in guideways 116 provided under the table 26. In addition, the presence of the resilient biasing member 134 assists the user in the manual deployment of the table 26, particularly compact and simple. When the table 26 is to be folded again, the movements described above are made in reverse. Alternatively, the support members 114 are devoid of rotating elements 122. They are for example made of a material limiting friction, such as PTFE.
    [0029] In another variant (not shown), the support members 114 are integral with the frame 24. In yet another variant (not shown), the guideways 116 project downwards relative to the table 26 , and each fulcrum is defined in a notch provided on the frame 24 to receive the guide path 116.
    [0030] In a variant, at least one jack (not shown) actuates the movement of the table 26 on the frame 24. In another variant, the displacement of the table 26 on the frame 24 is caused by a motor activated by the user. In another variant, the guideway 130 is vertical, while having an upper end offset laterally rearwardly with respect to a vertical axis passing through the fulcrum 123. In yet another variant, the flap 30 is Deployable downward from the cover 28. It is adapted to be moved by the table 26 to fade up under the effect of the weight of the cover 28.30
    权利要求:
    Claims (16)
    [0001]
    CLAIMS1.- Device (22) support for an assembly (10) for interior layout of an aircraft cabin (12) comprising: - a fixed frame (24); - A table (26) deployable relative to the frame (24) between a retracted position and an extended horizontal position; a guide mechanism (90) for moving the table (26) relative to the frame (24) between the retracted position and the extended horizontal position; characterized in that the guiding mechanism (90) defines at least one fulcrum (123) of the table (26) as it passes from the retracted position to the extended horizontal position, the fulcrum (123) having a generally invariant position relative to the frame (24), the table (26) being configured to pivot on the fulcrum (123) laterally away from the fulcrum (123) by sliding on the fulcrum (123) to the deployed position.
    [0002]
    2. - Device (22) according to claim 1, wherein the or each support point (123) protrudes upwardly relative to the frame (24).
    [0003]
    3. - Device (22) according to one of claims 1 or 2, wherein the guide mechanism (90) comprises a support member (114) rotatably mounted about a fixed axis relative to the frame (24). , the fulcrum (123) being defined on the support member (114).
    [0004]
    4. - Device (22) according to any one of the preceding claims, wherein the table (26) comprises a guide path (116) of sliding of the table (26) on the fulcrum (123).
    [0005]
    5. - Device (22) according to claim 4, wherein the fulcrum (123) cooperates with the guide path (116).
    [0006]
    6. - Device (22) according to any one of claims 4 or 5, wherein the guiding mechanism (90) comprises a rail (124) inserted into the table (26), the rail (124) defining the path of guiding (116).
    [0007]
    7. - Device (22) according to any one of the preceding claims, wherein the table (26) is adapted to be applied on the fulcrum (123) from the retracted position to the extended horizontal position, the guiding mechanism (90) being configured so that the table (26) follows a single and reproducible trajectory from the retracted position to the extended horizontal position.
    [0008]
    8. - Device (22) according to any one of the preceding claims, wherein the frame (24) comprises at least one leg (92) substantially vertical, the guide mechanism (90) comprising at least one guideway (132) of the table (26) along the leg (92).
    [0009]
    9. - Device (22) according to claim 8, wherein the guide path (132) is formed through the leg (92), the guide mechanism (90) having a guide member (130) movable together with the table (26), the guide member (130) being mounted in the guideway (132).
    [0010]
    10. - Device (22) according to claim 9, wherein the guiding mechanism (90) comprises a rack (133), the guide member (130) comprising a toothed wheel.
    [0011]
    11. - Device (22) according to any one of claims 9 or 10, wherein the table (26) comprises a carriage (104), the guide member (130) being rotatably mounted in the carriage (104).
    [0012]
    12. - Device (22) according to any one of the preceding claims, wherein the upper end of the guideway (132) is offset laterally with respect to a vertical axis passing through the fulcrum (123), the guide path (132) being inclined with respect to the vertical axis passing through the fulcrum (123) or being parallel to the vertical axis passing through the fulcrum (123).
    [0013]
    13. - Device (22) according to any one of the preceding claims, wherein the guiding mechanism (90) comprises at least one elastic biasing member (134) adapted to drive the table (26) upwards relative to the frame (24).
    [0014]
    14. - Device (22) according to claim 13, taken in combination with claim 11, wherein the resilient biasing member (134) is mounted in the carriage between the guide member (130) and the carriage (104). ).
    [0015]
    15. - Assembly (10) for interior layout of an aircraft cabin (12), comprising: - a device (22) according to any one of the preceding claims, - a console (20) delimiting a receiving housing. (44) of the table (26) opening through a deployment opening (46), the table (26) being deployable through the deployment opening (46) between the retracted position disposed in the receiving housing (44) and an extended horizontal position; and a cover mounted on the console (20), the cover being movable between an open configuration for the passage of the table (26) and a closed configuration for closing the deployment opening (46).
    [0016]
    16. - Method of interior layout of an aircraft cabin (12) comprising the following steps: - Provision of a device (22) according to any one of claims 1 to 14, the table (26) occupying its position. retracted position; - Passing the table (26) from its retracted position to its extended horizontal position, the table (26) resting on the fulcrum (123) and pivoting about the support point (123) away laterally of the fulcrum (123) by sliding on the fulcrum (123) to the extended position.
    类似技术:
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    EP1405758B1|2006-09-20|Improved folding table arrangement in an automotive vehicle passenger compartment
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    FR3092056A1|2020-07-31|Vehicle interior component, comprising a retractable shelf
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    EP1207079B1|2005-10-05|Vehicle seat delimiting a loading space
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    WO2016038260A1|2016-03-17|Arrangement for holding difference types of mobile multimedia devices in a vehicle, and corresponding instrument panel
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    FR2880851A1|2006-07-21|Retractable step plate for motor vehicle, has horizontal support plate comprising groove cooperating with slug that is integrated to carriage which slides on lower rail while opening and closing sliding door
    EP1564053B1|2008-12-10|Foldable hardtop for vehicle
    EP1711359B1|2012-02-29|Vehicle provided with a vertically retractable open roof
    FR2859957A1|2005-03-25|Rear parcel shelf system for convertible vehicle, has pin, sensing device and cam allowing rear of shelf to be pressed against front side of cover, when shelf reaches deployed position
    FR2856347A1|2004-12-24|Motor vehicle, has displacement unit that moves roof unit between closed position above cab interior and opened position in storage space, and rear glass raising towards hoods front and placing itself behind roof unit to close cab interior
    EP2172367A2|2010-04-07|Moveable tray for the trunk of a motor vehicle
    EP2790960B1|2020-11-18|Retractable seat for a motor vehicle
    FR2828838A1|2003-02-28|Sedan convertible into pick up comprises compartment delimited by floor, partly retractable roof, rear door with window and panel, roof formed by transverse slats able to move rearwards
    FR2913373A1|2008-09-12|Convertible motor vehicle, has roller cooperated with guiding rail guiding cassette carrying panel between retracted, intermediate and storage positions, and reducing unit for reducing trajectory of driving unit driving cassette
    FR2953169A1|2011-06-03|Multifunctional vehicle e.g. automobile such as car, has connection unit connecting movable partition with structure to fix partition at intermediate position in which partition is spaced from roof to define storage compartment with roof
    FR3098461A1|2021-01-15|Vehicle with a seat convertible into an office
    FR3080070A1|2019-10-18|VEHICLE BENCH WITH ARMREST WITH TABLETS
    同族专利:
    公开号 | 公开日
    FR3032177B1|2017-03-03|
    CA2919237A1|2016-08-04|
    US20160221677A1|2016-08-04|
    BR102016002397A2|2016-10-11|
    US9938016B2|2018-04-10|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
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    FR3032177B1|2015-02-04|2017-03-03|Dassault Aviat|SUPPORT DEVICE FOR AN INTERIOR ARRANGEMENT OF AN AIRCRAFT CAR, ASSOCIATED ASSEMBLY AND METHOD|
    FR3032178B1|2015-02-04|2017-03-03|Dassault Aviat|AIRCRAFT CABIN INTERIOR DEVELOPMENT ASSEMBLY AND METHOD THEREOF|US9919802B2|2014-04-07|2018-03-20|B/E Aerospace, Inc.|Laterally-expanding tray table|
    CN106455825A|2014-04-07|2017-02-22|Be航天公司|Laterally-expanding tray table|
    FR3032177B1|2015-02-04|2017-03-03|Dassault Aviat|SUPPORT DEVICE FOR AN INTERIOR ARRANGEMENT OF AN AIRCRAFT CAR, ASSOCIATED ASSEMBLY AND METHOD|
    FR3032178B1|2015-02-04|2017-03-03|Dassault Aviat|AIRCRAFT CABIN INTERIOR DEVELOPMENT ASSEMBLY AND METHOD THEREOF|
    WO2017003521A1|2015-06-29|2017-01-05|Zodiac Seats Us Llc|Core of tray table assembly|
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    US10875652B2|2017-04-03|2020-12-29|Rockwell Collins, Inc.|Passenger tray table|
    KR102114066B1|2018-10-31|2020-05-25|주식회사 서연이화|Cupholder with integral Table|
    法律状态:
    2016-02-18| PLFP| Fee payment|Year of fee payment: 2 |
    2016-08-05| PLSC| Publication of the preliminary search report|Effective date: 20160805 |
    2017-02-08| PLFP| Fee payment|Year of fee payment: 3 |
    2018-01-29| PLFP| Fee payment|Year of fee payment: 4 |
    2020-01-13| PLFP| Fee payment|Year of fee payment: 6 |
    2021-01-22| PLFP| Fee payment|Year of fee payment: 7 |
    2022-01-12| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1500207A|FR3032177B1|2015-02-04|2015-02-04|SUPPORT DEVICE FOR AN INTERIOR ARRANGEMENT OF AN AIRCRAFT CAR, ASSOCIATED ASSEMBLY AND METHOD|FR1500207A| FR3032177B1|2015-02-04|2015-02-04|SUPPORT DEVICE FOR AN INTERIOR ARRANGEMENT OF AN AIRCRAFT CAR, ASSOCIATED ASSEMBLY AND METHOD|
    CA2919237A| CA2919237A1|2015-02-04|2016-01-27|Supporting device for an interior layout assembly of an aircraft cabin, related assembly and method|
    US15/010,696| US9938016B2|2015-02-04|2016-01-29|Supporting device for an interior layout assembly of an aircraft cabin, related assembly and method|
    BR102016002397A| BR102016002397A2|2015-02-04|2016-02-03|support device for an aircraft cabin interior physical fittings set, related assembly and method|
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