Electric aero seat clutch

Abstract

The utility model provides an electric aero seat clutch, and belongs to the technical field of aero seats. Comprising a planetary gear set which is arranged in a case, and a planetary gear shaft is connected to the end, away from a driving motor, of the planetary gear set through a planetary gear mounting disc; the driven gear is rotationally connected to the interior of the case through a rotating shaft, the rotating shaft and the planetary gear shaft are arranged in parallel, the two ends of the rotating shaft are provided with a hand-driven gear and an adjusting assembly mounting block respectively, and the hand-driven gear and the adjusting assembly mounting block both protrude out of the case body; the clutch assembly is movably connected to the shaft body of the planetary gear shaft and used for connecting or disconnecting transmission of the planetary gear set; and the control assembly is used for controlling the sliding position of the clutch assembly. The device is simple and compact in structure and easy to manufacture and install, and the production cost and the maintenance difficulty are reduced; smooth switching between electric adjustment and manual adjustment is achieved, and the adjustment flexibility and convenience of the seat are improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation seats, and particularly relates to an electric aviation seat clutch. Background Art

[0002] In the seats used in the fields of bullet trains or aviation, relatively high requirements are placed on the seats. However, according to the requirements of safety technical performance, in such places, the seats are often relatively fixed and cannot move, to avoid the seats moving by themselves during operation and threatening personal safety or affecting the normal operation of equipment. In this specific environment, the seats are fixed, but the staff sitting on them is not the only one, which will result in that the seats that cannot move freely are not suitable for passengers with different body shapes.

[0003] With the continuous development of transportation technology, passengers have higher and higher requirements for the comfort and convenience of aviation seats. The existing aviation seat adjustment mechanisms mostly rely on electric or pneumatic drive. However, in some special cases (such as power failure), manual adjustment becomes necessary. However, the traditional clutch designs often have problems such as complex structures and inconvenient operations, and it is difficult to meet the adjustment requirements of modern aviation seats.

[0004] Therefore, this application provides an electric aviation seat clutch to meet the requirements. Summary of the Utility Model

[0005] The technical problem to be solved by the utility model is to provide an electric aviation seat clutch to solve the problems that the existing clutch designs often have complex structures and inconvenient operations, and it is difficult to meet the adjustment requirements of modern aviation seats.

[0006] To solve the above technical problems, the utility model provides the following technical solutions:

[0007] An electric aviation seat clutch, comprising: a chassis and a chassis cover, which are fixedly connected by bolts and are used to provide a support box body for installing and building each component of the clutch; a planetary gear set, which is arranged inside the chassis and is used to connect a driving motor. One end of the planetary gear set far from the driving motor is connected with a planetary gear shaft through a planetary gear mounting disc; a driven gear, which is rotatably connected inside the chassis through a rotating shaft, and the rotating shaft is arranged parallel to the planetary gear shaft. A manual driving gear and an adjusting component mounting block are respectively arranged at both ends of the rotating shaft, and both the manual driving gear and the adjusting component mounting block protrude outside the box body; a clutch component, which is movably connected to the shaft body of the planetary gear shaft and is used to connect or disconnect the transmission of the planetary gear set; a control component, which is used to control the sliding position of the clutch component.

[0008] Preferably, an installation groove is opened on the chassis for installing the driving motor.

[0009] Preferably, the clutch assembly includes: a flanged bearing, which is movably connected to the planetary gear mounting disc through a positioning shaft, and an internal gear sleeve is provided inside the flanged bearing; a transmission gear set, which includes a large gear and a small gear arranged coaxially, the large gear is meshed and connected with the driven gear, and the small gear is clamped and connected with the internal gear sleeve; a spring, which is sleeved on the shaft body of the transmission gear set, and both ends of the spring abut between the large gear and the clutch assembly respectively.

[0010] Preferably, it further includes positioning holes, there are two of them, and they are symmetrically arranged on the opposite side walls of the chassis.

[0011] Preferably, the control assembly includes: a pin, which is rotatably connected inside the chassis through two positioning holes, and one end of the pin protrudes outside the chassis; a shoulder nut, which is fixedly connected to the end of the pin protruding outside the chassis; a U-shaped top plate, which is fixedly connected to the pin, and one end of the U-shaped top plate is clamped on the outer side wall of the flanged bearing.

[0012] Preferably, an assembly part is provided at the middle position of the pin, and an assembly groove is provided on the side of the U-shaped top plate away from the flanged bearing, and the assembly part and the assembly groove are fixedly connected by bolts.

[0013] Preferably, the shoulder nut has an L-shaped structure, and an installation slot is provided at the end of the shoulder nut away from the pin for installing a rotating handle.

[0014] Compared with the prior art, the present invention has at least the following beneficial effects:

[0015] 1. The structure is simple and compact, easy to manufacture and install, reducing the production cost and maintenance difficulty.

[0016] 2. It realizes the smooth switching between electric and manual adjustment, improving the adjustment flexibility and convenience of the seat. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] The drawings incorporated herein and constituting a part of the specification illustrate embodiments of the present disclosure and, together with the specification, are further used to explain the principles of the present disclosure and enable those skilled in the relevant art to implement and use the present disclosure.

[0018] Figure 1 It is a schematic diagram of the overall structure of the present invention;

[0019] Figure 2 It is an exploded view of the overall structure of the present invention;

[0020] Figure 3 It is a schematic diagram of the structure of the clutch assembly of the present invention;

[0021] Figure 4 It is an exploded view of the control assembly structure of the present invention.

[0022] In the figure: 11, chassis; 12, box cover; 13, positioning hole; 14, installation groove; 2, clutch assembly; 21, spring; 22, flanged bearing; 23, internal gear sleeve; 24, transmission gear set; 3, planetary gear set; 31, planetary gear shaft; 32, planetary gear mounting disc; 4, hand drive gear; 5, driven gear; 6, adjustment component mounting block; 7, pin; 71, assembly part; 8, shoulder nut; 81, installation card slot; 9, U-shaped top disc; 91, assembly groove.

[0023] As shown in the figure, in order to clearly implement the structure of the embodiments of the present invention, specific structures and devices are marked in the figure, but this is only for schematic needs and is not intended to limit the present invention to this specific structure, device and environment. According to specific needs, those of ordinary skill in the art can adjust or modify these devices and environments, and the adjustments or modifications still fall within the scope of the appended claims. Specific embodiments

[0024] The following will describe in detail an electric aviation seat clutch provided by the present invention in conjunction with the accompanying drawings and specific embodiments. At the same time, it should be noted here that in order to make the embodiments more detailed, the following embodiments are the best and preferred embodiments. For some well-known technologies, those skilled in the art can also adopt other alternative methods for implementation; moreover, the accompanying drawings are only for more specifically describing the embodiments and are not intended to specifically limit the present invention.

[0025] As Figure 1 - Figure 4 shown, an embodiment of the present invention provides an electric aviation seat clutch, including: a chassis 11 and a box cover 12, fixedly connected by bolts, and used as a support box for installing and building each component of the clutch; a planetary gear set 3, arranged inside the chassis 11, and used to connect a driving motor. One end of the planetary gear set 3 far from the driving motor is connected with a planetary gear shaft 31 through a planetary gear mounting disc 32; a driven gear 5, rotatably connected inside the chassis 11 through a rotating shaft, and the rotating shaft is arranged parallel to the planetary gear shaft 31. A hand drive gear 4 and an adjustment component mounting block 6 are respectively arranged at both ends of the rotating shaft, and both the hand drive gear 4 and the adjustment component mounting block 6 protrude outside the box body; a clutch assembly 2, movably connected to the shaft body of the planetary gear shaft 31, and used to connect or disconnect the transmission of the planetary gear set 3, including: a flanged bearing 22, movably connected to the planetary gear mounting disc 32 through a positioning shaft, and an internal gear sleeve 23 is arranged inside the flanged bearing 22; a transmission gear set 24, including a large gear and a small gear arranged coaxially, the large gear is meshed and connected with the driven gear 5, and the small gear is clamped and connected with the internal gear sleeve 23; a spring 21, sleeved on the shaft body of the transmission gear set 24, and both ends of the spring 21 respectively abut between the large gear and the clutch assembly 2; a control component, used to control the sliding position of the clutch assembly 2.

[0026] Among them, the chassis 11 serves as the main structure of the entire clutch and is made of high-strength materials to ensure its stability and durability. The cover 12 is tightly connected to the chassis 11 through precisely machined bolts to form a closed space, protecting the internal components from the external environment. This not only facilitates assembly and maintenance but also provides good sealing to prevent dust and impurities from entering. In addition, the shapes, sizes, and materials of the chassis 11 and the cover 12 can be adjusted according to specific requirements to adapt to different models of electric aviation seats.

[0027] The planetary gear set 3 is the core component for the clutch to achieve power transmission. Through complex gear meshing relationships, it efficiently transmits the power of the drive motor to subsequent components. The planetary gear mounting disk 32, as a connecting part, firmly connects the planetary gear set 3 to the planetary gear shaft 31 to ensure the continuity and stability of power transmission. The design of the planetary gear set allows for a large reduction ratio to be achieved within a relatively small volume, which is suitable for the aviation seat environment with strict space requirements. The drive motor operates at a high speed, and the planetary gear set 3 reduces the speed to a range suitable for seat adjustment through multi-stage reduction, while increasing the torque output to meet the needs of seat adjustment.

[0028] The driven gear 5 is the output component of the clutch. It rotates freely within the chassis 11 through a rotating shaft. A sliding groove for installing the planetary gear shaft 31 is provided at the central position inside the rotating shaft, and the two are slidably connected. Power reception and transmission are achieved by the engagement of a small gear with an internal gear sleeve 23 inside a flanged bearing 22 that is axially movably connected to the planetary gear mounting disk 32. The design of the manual drive gear 4 allows for driving seat adjustment through corresponding gear sleeve fittings and manual rotation in case of failure of the electric system, improving the reliability and emergency response ability of the system. Among them, the manual drive gear 4 can be replaced with other forms of manual operating mechanisms, such as a crank or a knob, to adapt to the usage habits of different users. The adjustment component mounting block 6 is used to connect the aviation seat adjustment components (such as: backrest adjustment lever, leg rest adjustment lever, etc.).

[0029] By controlling the sliding clutch component 2, the switching between connecting and disconnecting the transmission of the planetary gear set 3 is controlled, thereby achieving the control of the seat adjustment function.

[0030] As Figure 1 shown, an installation groove 14 is provided on the chassis 11 for installing the drive motor, facilitating the fixation and transmission connection of the motor.

[0031] As Figure 2 and Figure 4As shown, it further includes positioning holes 13, with two of them, symmetrically arranged on the opposite side walls of the chassis 11; and the control component includes: a pin 7, rotatably connected inside the chassis 11 through the two positioning holes 13, with one end of the pin 7 protruding outside the chassis 11; a shoulder nut 8, fixedly connected to the end of the pin 7 protruding outside the chassis 11; a U-shaped top plate 9, fixedly connected to the pin 7, with one end of the U-shaped top plate 9 clamped on the outer side wall of the flanged bearing 22; an assembly part 71 is provided at the middle position of the pin 7, and an assembly groove 91 is provided on the side of the U-shaped top plate 9 away from the flanged bearing 22, and the assembly part 71 and the assembly groove 91 are fixedly connected by bolts.

[0032] By providing a rotating pin 7 to drive the U-shaped top plate 9 to flip, and then cooperating with the abutment against the protruding edge of the flanged bearing 22 to drive the flanged bearing 22 to slide against the elastic force of the spring 21, so that the inner gear sleeve 23 is disengaged from the pinion on the transmission gear set 24, realizing the disconnection of the transmission connection between the two systems and enabling manual drive adjustment.

[0033] As Figure 1 As shown, the shoulder nut 8 has an L-shaped structure, and an installation slot 81 is provided at the end of the shoulder nut 8 away from the pin 7 for installing a rotating handle to facilitate manually twisting the pin 7.

[0034] In the technical solution provided by the present utility model, during normal operation, under the elastic force of the spring 21, the flanged bearing 22 is pushed away from the end far from the large gear, so that the pinion is engaged with the inner gear sleeve 23 to ensure that the planetary gear set 3 can normally transmit power to the driven gear 5, and the adjustment of the aviation seat is realized by driving the drive motor. When a power failure occurs, by manually turning the shoulder nut 8, the pin 7 is driven to rotate, driving the U-shaped top plate 9 to flip. Through the abutment between the U-shaped top plate 9 and the protruding part of the flanged bearing 22, the whole flanged bearing 22 is driven to slide against the elastic force of the spring 21, so that the pinion in the transmission gear set 24 is disengaged from the inner gear sleeve 23, disconnecting the transmission of the planetary gear set 3. At this time, the flanged bearing 22 is connected by sliding of the positioning shaft and also rotates synchronously with the output end of the planetary gear set 3 when the transmission is disconnected, facilitating the subsequent reset and docking of the clutch assembly 2; on the other hand, due to the loss of the transmission and support of the electric drive system, by directly driving the rotation of the installation block 6 of the adjustment component by rotating the manual drive gear 4, the manual adjustment of the aviation seat is realized.

[0035] The present utility model covers any alternatives, modifications, equivalent methods and solutions made within the essence and scope of the present utility model. In order to enable the public to have a thorough understanding of the present utility model, specific details are described in detail in the above preferred embodiments of the present utility model, and those skilled in the art can fully understand the present utility model without these detailed descriptions. In addition, in order to avoid unnecessary confusion to the essence of the present utility model, well-known methods, processes, procedures, components and circuits are not described in detail.

[0036] The above are only the preferred embodiments of the present utility model. It should be noted that for those of ordinary skill in the art, several improvements and modifications can be made without departing from the principle of the present utility model, and these improvements and modifications should also be regarded as the protection scope of the present utility model.

Claims

1. An electric aviation seat clutch, characterized in that Including: A chassis (11) and a box cover (12), fixedly connected by bolts, for providing a support box for installing and building each component of the clutch; A planetary gear set (3), arranged inside the chassis (11), for connecting a driving motor. One end of the planetary gear set (3) far from the driving motor is connected with a planetary gear shaft (31) through a planetary gear mounting disc (32); A driven gear (5), rotatably connected inside the chassis (11) through a rotating shaft, and the rotating shaft is arranged parallel to the planetary gear shaft (31). A manual driving gear (4) and an adjusting component mounting block (6) are respectively arranged at both ends of the rotating shaft, and both the manual driving gear (4) and the adjusting component mounting block (6) protrude outside the box body; A clutch component (2), movably connected to the shaft body of the planetary gear shaft (31), for connecting or disconnecting the transmission of the planetary gear set (3); A control component, for controlling the sliding position of the clutch component (2).

2. The electric aviation seat clutch according to claim 1, wherein An installation groove (14) is opened on the chassis (11) for installing a driving motor.

3. The electric aviation seat clutch according to claim 1, characterized in that The clutch component (2) includes: A flanged bearing (22), movably connected to the planetary gear mounting disc (32) through a positioning shaft, and an internal gear sleeve (23) is opened inside the flanged bearing (22); A transmission gear set (24), including a large gear and a small gear arranged coaxially. The large gear is meshed and connected with the driven gear (5), and the small gear is clamped and connected with the internal gear sleeve (23); A spring (21), sleeved on the shaft body of the transmission gear set (24), and both ends of the spring (21) are respectively abutted between the large gear and the clutch component (2).

4. The electric aviation seat clutch according to claim 3, characterized in that, There are also two positioning holes (13), symmetrically arranged on the opposite side walls of the chassis (11).

5. The electric aviation seat clutch according to claim 4, wherein The control component includes: A pin (7), rotatably connected inside the chassis (11) through the two positioning holes (13), and one end of the pin (7) protrudes outside the chassis (11); A shoulder nut (8), fixedly connected to the end of the pin (7) protruding outside the chassis (11); A U-shaped top disc (9), fixedly connected to the pin (7), and one end of the U-shaped top disc (9) is clamped on the outer side wall of the flanged bearing (22).

6. The electric aviation seat clutch according to claim 5, characterized in that, An assembly part (71) is opened at the middle position of the pin (7), and an assembly groove (91) is opened on the side of the U-shaped top disc (9) away from the flanged bearing (22). The assembly part (71) and the assembly groove (91) are fixedly connected by bolts.

7. The electric aviation seat clutch according to claim 5, characterized in that, The shoulder nut (8) is in an L-shaped structure, and an installation slot (81) is opened at the end of the shoulder nut (8) away from the pin (7) for installing a rotating handle.

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