Aero seat with automatic auxiliary fixing function

Abstract

The invention discloses an aero seat with an automatic auxiliary fixing function, and relates to the technical field of aero seats, the aero seat comprises a cushion bottom plate, a base, a supporting frame, a fixing shaft, a leg supporting plate and a backrest plate, and one end, away from the cushion bottom plate, of the backrest plate is fixedly connected with a reinforcing plate; a positioning mechanism for adjusting and positioning the backrest plate and the leg supporting plate is arranged on the supporting frame; a locking mechanism for synchronously fixing and locking the supporting frame, the base, the backrest plate and the leg supporting plate is arranged on the supporting frame; a reinforcing mechanism for connecting and reinforcing the cushion bottom plate and the backrest plate is arranged on the backrest plate. The angle of the backrest plate and the angle of the leg supporting plate can be independently adjusted through the positioning mechanism, so that the device can be suitable for the use experience of different users, meanwhile, the body of a special passenger can be bound in cooperation with a safety belt, and the device can temporarily serve as a stretcher to convey the special passenger who is inconvenient to move in a seamless connection mode.

Description

Technical Field

[0001] The invention relates to the technical field of aviation seats, in particular to an aviation seat with automatic auxiliary fixing. Background Art

[0002] Aviation refers to the flight activities of aircraft in the Earth's atmosphere, including lighter-than-air and heavier-than-air aircraft. It has the characteristics of fast transportation, safety, reliability, and no restrictions on ground conditions. However, it also has limitations such as high transportation costs and limited capacity. Aviation seats are seats for passengers in the aircraft cabin, and there are different types and layouts according to the cabin class and aircraft model.

[0003] Existing airline seats are mainly used for passengers to sit on when in use. For some special passengers, such as those with limited mobility due to mental illness or physical disabilities, their bodies are usually restrained by seat belts to ensure their safety, so as to avoid adverse effects on other passengers. However, when the plane lands and docks with the corresponding personnel, the seat belts need to be removed and a stretcher or cable tie equipped with seat belts needs to be used for transportation. In order to transport special passengers with limited mobility in a seamless manner, an airline seat with automatic auxiliary fixation is now provided, which can eliminate the disadvantages of existing devices. Summary of the invention

[0004] The object of the present invention is to provide an aviation seat with automatic auxiliary fixing function to solve the problems in the background technology.

[0005] To achieve the above object, the present invention provides the following technical solutions:

[0006] An aviation seat with automatic auxiliary fixing comprises a seat cushion bottom plate, a base is arranged below the seat cushion bottom plate, a support frame is arranged on the upper surface of the base, the seat cushion bottom plate is located on the inner side of the support frame, two groups of fixed shafts are symmetrically fixedly connected to the outer wall of the seat cushion bottom plate, both groups of fixed shafts are fixedly connected to the support frame, a leg support plate is slidably sleeved on the outer wall of one group of fixed shafts, the leg support plate is located at one end of the base, a backrest plate is slidably sleeved on the outer wall of the other group of fixed shafts, a reinforcing plate is fixedly connected to the end of the backrest plate away from the seat cushion bottom plate, and a positioning mechanism for adjusting and positioning the backrest plate and the leg support plate is arranged on the support frame;

[0007] The support frame is provided with a locking mechanism for synchronously fixing and locking the support frame, the base, the backrest plate, and the leg support plate;

[0008] The backrest plate is provided with a reinforcement mechanism for connecting and reinforcing the seat cushion bottom plate and the backrest plate.

[0009] On the basis of the above technical solution, the present invention also provides the following optional technical solution:

[0010] In an optional solution: the positioning mechanism includes:

[0011] A rotating assembly disposed on the support frame;

[0012] The rotating assembly comprises:

[0013] A positioning rotating plate is arranged inside the supporting frame, the positioning rotating plate is rotatably connected to the supporting frame, a gear is fixedly connected to the top end of the positioning rotating plate, the gear is located at the bottom end of the seat cushion bottom plate, and the gear is rotatably connected to the seat cushion bottom plate;

[0014] A moving component is arranged on the gear.

[0015] In an optional solution: the mobile component includes:

[0016] Two racks are symmetrically meshed and connected to the outer wall of the gear, and two connecting push plates are symmetrically arranged inside the support frame. The two connecting push plates are respectively located on the sides of the two racks away from each other, and the two connecting push plates are respectively fixedly connected to the two racks, and the connecting push plates and the racks are both slidably connected to the support frame;

[0017] A positioning assembly is arranged on the connecting push plate.

[0018] In an optional solution: the positioning component includes:

[0019] Two fixed push rods symmetrically fixedly connected to one end of the connecting push plate, the two fixed push rods are fixedly connected to the limited push plate on one side away from the connecting push plate, and a plurality of positioning plugs are fixedly connected to the limited push plate on the side away from the fixed push rod at equidistant intervals, and the plurality of positioning plugs are all penetrated to the inner side of the support frame, and the plurality of positioning plugs are all located on the outer side of the fixed shaft, and the outer wall of the positioning plug away from the limited push plate is hemispherical, and the backrest plate, the leg support plate and the positioning plug are all provided with positioning slots that match the outer wall of the positioning plug, and the positioning plug, the limited push plate and the fixed push rod are all slidably connected to the support frame;

[0020] A reset component is arranged on the fixed push rod.

[0021] In an optional solution: the reset component is a spring sleeved on the outer wall of the fixed push rod, one end of the spring contacts the inner wall of the support frame, and the other end of the spring contacts the outer wall of the limit push plate.

[0022] In an optional solution: the locking mechanism includes:

[0023] A docking assembly disposed on the support frame;

[0024] The docking assembly includes:

[0025] Two groups of docking plug-in trays are symmetrically fixedly connected to the bottom of the support frame, the outer wall of the bottom end of the docking plug-in tray is in the shape of a truncated cone, the bottom end of the support frame is fixedly connected with a docking plug-in frame, the docking plug-in frame is located between the two groups of docking plug-in trays, the outer walls on both sides of the docking plug-in frame are in the shape of an inclined surface, and the base is provided with a docking slot that matches the outer wall of the docking plug-in frame and the docking plug-in tray at the connection position with the docking plug-in frame and the docking plug-in tray;

[0026] The docking frame is provided with a rotating assembly.

[0027] In an optional solution: the rotating assembly includes:

[0028] A first knob is arranged at an end of the docking frame away from the leg support plate, one end of the first knob is fixedly connected to a transmission rod, the transmission rod is located inside the docking frame, the end of the transmission rod away from the first knob is fixedly connected to a bidirectional screw rod, and the transmission rod and the bidirectional screw rod are both rotatably connected to the docking frame;

[0029] The bidirectional screw rod is provided with a clamping assembly.

[0030] In an optional solution: the engaging assembly includes:

[0031] The two movable push plates are symmetrically sleeved on the outer wall of the two-way screw rod, and the two movable push plates are threadedly connected to the two-way screw rod, and the two movable push plates are slidably connected to the support frame and the docking frame. The ends of the two movable push plates close to each other are fixedly connected with locking plug blocks, and the outer wall of the locking plug block at the end away from the movable push plate is hemispherical. The locking plug block penetrates the support frame to the interior of the positioning rotating plate, and the outer walls of the two movable push plates are symmetrically fixedly connected with two locking card plates, and the two locking card plates penetrate the docking frame to the interior of the base, and the locking card plate is slidably connected to the docking frame. A limiting slot for the sliding of the locking card plate is provided at the connection position between the base and the locking card plate, and the inner wall of the limiting slot is L-shaped.

[0032] In an optional solution: the reinforcement mechanism includes:

[0033] The first support frame is arranged at the top of the backrest board, and the first support frame passes through the interior of the backrest board, and the bottom end of the first support frame is fixedly connected to the limit sliding bar, and the limit sliding bar is located in the interior of the backrest board, and the outer wall of the limit sliding bar is symmetrically fixedly connected with two groups of reinforcement plug rods, and the two groups of reinforcement plug rods are both located below the first support frame, and the bottom outer wall of the reinforcement plug rod is hemispherical, and the first support frame, the limit sliding bar, and the reinforcement plug rod are all slidably connected to the backrest board, and the seat cushion bottom plate is provided with a limit slot for the reinforcement plug rod to slide, and the reinforcement plate is provided with a second knob at the end of the reinforcement plate away from the backrest plate, and one end of the second knob is fixedly connected with a bolt, and the bolt passes through the reinforcement plate to the interior of the backrest board, and the bolt contacts the outer wall of the limit sliding bar, and the bolt is threadedly connected to the reinforcement plate.

[0034] In an optional solution: the top end of the leg support plate is fixedly connected to a limit rotation plate, the limit rotation plate is rotatably connected to the seat cushion bottom plate, and the bottom end of the leg support plate is fixedly connected to a second support frame.

[0035] Compared with the prior art, the beneficial effects of the present invention are as follows:

[0036] 1. The present invention can adjust the angles of the backrest and the leg support separately through the positioning mechanism, so as to be suitable for the use experience of different users. At the same time, it can restrain the body of special passengers in conjunction with the safety belt, and can temporarily serve as a stretcher to transport special passengers with limited mobility in a seamless manner.

[0037] 2. The present invention uses a locking mechanism to fix the backrest and the leg support plate while simultaneously docking and fixing the support frame and the base, thereby achieving the purpose of synchronously fixing and locking the support frame, the base, the backrest and the leg support plate.

[0038] 3. The present invention can reinforce the seat cushion bottom plate and the backrest plate at the rotation position through the reinforcement mechanism, thereby improving the stability of the seat when used as a stretcher. BRIEF DESCRIPTION OF THE DRAWINGS

[0039] Figure 1 It is a schematic diagram of the structure of the present invention.

[0040] Figure 2 It is a schematic diagram of the exploded structure of the support frame and the base of the present invention.

[0041] Figure 3 It is a schematic diagram of the reinforcement mechanism structure of the present invention.

[0042] Figure 4 It is a schematic diagram of the internal structure of the support frame of the present invention.

[0043] Figure 5 It is a schematic diagram of the positioning mechanism structure of the present invention.

[0044] Figure 6 It is a schematic diagram of the locking mechanism structure of the present invention.

[0045] Figure 7 For the present invention Figure 4 Schematic diagram of the local enlarged structure at A in the figure.

[0046] Figure 8 It is a schematic diagram of the limit slot structure of the present invention.

[0047] 1. Seat cushion bottom plate; 201. Connecting push plate; 202. Gear; 203. Positioning rotating plate; 204. Rack; 205. Positioning plug block; 206. Limiting push plate; 207. Fixed push rod; 208. Spring; 301. First knob; 302. Transmission rod; 303. Bidirectional screw rod; 304. Locking plug block; 305. Moving push plate; 306. Locking card plate; 307. Docking plug frame; 308. Docking plug plate; 309. Limiting card slot; 401. First support frame; 402. Limiting slide rod; 403. Bolt; 404. Second knob; 405. Reinforcement plug rod; 5. Support frame; 6. Base; 7. Backrest plate; 8. Reinforcement plate; 9. Limiting rotating plate; 10. Leg support plate; 11. Second support frame; 12. Fixed shaft. DETAILED DESCRIPTION

[0048] In order to make the purpose, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below in conjunction with the accompanying drawings and embodiments.

[0049] In one embodiment, Figure 1-Figure 8 As shown, an aviation seat with automatic auxiliary fixing comprises a seat cushion bottom plate 1, a base 6 is arranged below the seat cushion bottom plate 1, a support frame 5 is arranged on the upper surface of the base 6, the seat cushion bottom plate 1 is located on the inner side of the support frame 5, and the outer wall of the seat cushion bottom plate 1 is symmetrically fixedly connected with two groups of fixed shafts 12, both of which are fixedly connected to the support frame 5, a leg support plate 10 is slidably sleeved on the outer wall of one group of fixed shafts 12, the leg support plate 10 is located at one end of the base 6, and a backrest plate 7 is slidably sleeved on the outer wall of the other group of fixed shafts 12, and a reinforcing plate 8 is fixedly connected to the end of the backrest plate 7 away from the seat cushion bottom plate 1, a top end of the leg support plate 10 is fixedly connected with a limited rotation plate 9, and the limited rotation plate 9 is rotatably connected to the seat cushion bottom plate 1, and a second support frame 11 is fixedly connected to the bottom end of the leg support plate 10, and a positioning mechanism for adjusting and positioning the backrest plate 7 and the leg support plate 10 is provided on the support frame 5;

[0050] The support frame 5 is provided with a locking mechanism for synchronously fixing and locking the support frame 5, the base 6, the backrest plate 7, and the leg support plate 10;

[0051] The backrest plate 7 is provided with a reinforcement mechanism for connecting and reinforcing the seat cushion bottom plate 1 and the backrest plate 7;

[0052] The positioning mechanism includes: a rotating assembly arranged on the support frame 5;

[0053] The rotating assembly includes: a positioning rotating plate 203 disposed inside the supporting frame 5, the positioning rotating plate 203 is rotatably connected to the supporting frame 5, a gear 202 is fixedly connected to the top of the positioning rotating plate 203, the gear 202 is located at the bottom end of the seat cushion bottom plate 1, and the gear 202 is rotatably connected to the seat cushion bottom plate 1;

[0054] A moving assembly is provided on the gear 202;

[0055] The moving assembly includes: two racks 204 symmetrically meshed and connected to the outer wall of the gear 202, two connecting push plates 201 symmetrically arranged inside the support frame 5, the two connecting push plates 201 are respectively located on the sides of the two racks 204 away from each other, the two connecting push plates 201 are respectively fixedly connected to the two racks 204, and the connecting push plates 201 and the racks 204 are both slidably connected to the support frame 5;

[0056] A positioning assembly is provided on the connecting push plate 201;

[0057] In this embodiment, it is necessary to particularly explain that: the seat cushion bottom plate 1, the backrest plate 7 and the leg support plate 10 are all equipped with safety belts for restraining special passengers, and safety belt buckles are installed at the ends of the safety belts, and the safety belt buckles can be used to restrain the user's body, thereby ensuring that the safety belt can fit tightly on the occupant;

[0058] When in use, the user's body can be restrained by the safety belt to the seat cushion bottom plate 1, the backrest plate 7, and the leg support plate 10, so that the movement of the special passenger in the seat can be restricted in an emergency;

[0059] When the angles of the backrest board 7 and the leg support board 10 need to be adjusted, the locking mechanism can be used to release the locking of the positioning rotating plate 203, and then the backrest board 7 is pushed to rotate along the outer wall of a set of fixed shafts 12. In this process, the backrest board 7 can be flipped and positioned by the positioning mechanism, and then the leg support board 10 is pulled to rotate. At this time, the limiting rotating plate 9 is synchronously rotated under the drive of the leg support board 10, and the above operation is repeated at the same time, so as to realize the flipping and positioning of the leg support board 10, and then the backrest board 7 and the leg support board 10 can be fixed and locked by the locking mechanism;

[0060] When it is necessary to transport special passengers with limited mobility, the locking mechanism can be used to release the locking of the positioning rotating plate 203, and at the same time, the docking fixation of the support frame 5 and the base 6 can be released, and then the backrest board 7 and the leg support board 10 can be pushed to flip over respectively until the upper surfaces of the backrest board 7 and the leg support board 10 are in the same horizontal state as the upper surface of the seat cushion bottom plate 1. At this time, the reinforcement plate 8 is driven by the backrest board 7 to contact the outer wall of the support frame 5, so that the user can lie flat, and then the seat cushion bottom plate 1 and the backrest board 7 can be reinforced at the rotation position, and then the seat cushion bottom plate 1, the backrest board 7 and the leg support board 10 can be lifted by the second support frame 11 and the reinforcement mechanism, so that the seat can be temporarily used as a stretcher to transport special passengers with limited mobility in a seamless manner;

[0061] In one embodiment, Figure 4-Figure 7 As shown, the positioning assembly includes: two fixed push rods 207 symmetrically fixedly connected to one end of the connecting push plate 201, the two fixed push rods 207 are fixedly connected to the limited push plate 206 on one side away from the connecting push plate 201, and the limited push plate 206 is fixedly connected with a plurality of positioning plugs 205 equidistantly in the circumferential direction on one side away from the fixed push rod 207, and the plurality of positioning plugs 205 are all penetrated to the inner side of the support frame 5, and the plurality of positioning plugs 205 are all located on the outer side of the fixed shaft 12, and the outer wall of the side of the positioning plug 205 away from the limited push plate 206 is hemispherical, and the backrest plate 7, the leg support plate 10 and the positioning plug 205 are connected at the position where the positioning plug 205 is connected. The positioning plug 205, the limited push plate 206, and the fixed push rod 207 are all slidably connected to the support frame 5;

[0062] A reset assembly is provided on the fixed push rod 207;

[0063] The reset component is a spring 208 sleeved on the outer wall of the fixed push rod 207, one end of the spring 208 contacts the inner wall of the support frame 5, and the other end of the spring 208 contacts the outer wall of the limit push plate 206. Through the cooperation between the positioning component and the reset component, the backrest plate 7 and the leg support plate 10 can be adjusted and positioned at an angle;

[0064] In one embodiment, Figure 2-Figure 6 As shown, the locking mechanism includes: a docking assembly arranged on the support frame 5;

[0065] The docking assembly includes: two groups of docking plug-in trays 308 symmetrically fixedly connected to the bottom of the support frame 5, the bottom outer wall of the docking plug-in tray 308 is in the shape of a truncated cone, the bottom end of the support frame 5 is fixedly connected with a docking plug-in frame 307, the docking plug-in frame 307 is located between the two groups of docking plug-in trays 308, and the outer walls of both sides of the docking plug-in frame 307 are in the shape of an inclined surface, and the base 6 is provided with a docking slot that matches the outer wall of the docking plug-in frame 307 and the docking plug-in tray 308 at the connection position with the docking plug-in frame 307 and the docking plug-in tray 308, and the support frame 5 can be conveniently docked with the base 6 through the docking plug-in frame 307 and the docking plug-in tray 308;

[0066] A rotating assembly is provided on the docking frame 307;

[0067] In one embodiment, Figure 2-Figure 8 As shown, the rotating assembly includes: a first knob 301 arranged at one end of the docking plug-in frame 307 away from the leg support plate 10, one end of the first knob 301 is fixedly connected to a transmission rod 302, the transmission rod 302 is located inside the docking plug-in frame 307, and one end of the transmission rod 302 away from the first knob 301 is fixedly connected to a bidirectional screw rod 303, and the transmission rod 302 and the bidirectional screw rod 303 are both rotatably connected to the docking plug-in frame 307;

[0068] A clamping assembly is provided on the bidirectional screw rod 303;

[0069] The clamping assembly includes: two movable push plates 305 symmetrically sleeved on the outer wall of the bidirectional screw rod 303, the two movable push plates 305 are both threadedly connected to the bidirectional screw rod 303, the two movable push plates 305 are slidably connected to the support frame 5 and the docking frame 307, the ends of the two movable push plates 305 close to each other are fixedly connected with a locking plug 304, the outer wall of the end of the locking plug 304 away from the movable push plate 305 is hemispherical, the locking plug 304 passes through the support frame 5 to the interior of the positioning rotating plate 203, and the two movable push plates 305 The outer wall of the two locking cards 306 are symmetrically fixedly connected, and the two locking cards 306 are all through the docking plug-in frame 307 to the inside of the base 6. The locking card plate 306 is slidably connected to the docking plug-in frame 307. A limiting card slot 309 for the sliding of the locking card plate 306 is provided at the connecting position of the base 6 and the locking card plate 306. The inner wall of the limiting card slot 309 is L-shaped. Through the mutual cooperation of the rotating component and the locking component, the backrest plate 7 and the leg support plate 10 can be fixed, and the support frame 5 and the base 6 can be synchronously docked and fixed;

[0070] In one embodiment, Figure 1-Figure 3As shown, the reinforcement mechanism includes: a first support frame 401 arranged at the top of the backrest plate 7, the first support frame 401 penetrates into the interior of the backrest plate 7, the bottom end of the first support frame 401 is fixedly connected to a limit slide bar 402, the limit slide bar 402 is located inside the backrest plate 7, and the outer wall of the limit slide bar 402 is symmetrically fixedly connected with two groups of reinforcement plug rods 405, the two groups of reinforcement plug rods 405 are both located below the first support frame 401, and the bottom outer wall of the reinforcement plug rod 405 is hemispherical, and the first support frame 401, the limit slide bar 402, and the reinforcement plug rod 405 are all connected to the backrest plate 7. The backrest plate 7 is slidably connected, and a limiting slot for the sliding of the reinforcement rod 405 is provided at one end of the seat cushion base plate 1 close to the backrest plate 7, and a second knob 404 is provided at the end of the reinforcement plate 8 away from the backrest plate 7. A bolt 403 is fixedly connected to one end of the second knob 404. The bolt 403 passes through the reinforcement plate 8 to the inside of the backrest plate 7, and the bolt 403 contacts the outer wall of the limiting slide rod 402. The bolt 403 is threadedly connected to the reinforcement plate 8. The seat cushion base plate 1 and the backrest plate 7 can be reinforced at the rotation position through the reinforcement mechanism, so as to improve the stability of the seat when used as a stretcher.

[0071] The above embodiment discloses an aviation seat with automatic auxiliary fixation, wherein when in use, the user's body can be restrained to the seat cushion bottom plate 1, the backrest plate 7, and the leg support plate 10 respectively by the safety belt, so that the movement of the special passenger in the seat can be restricted in an emergency;

[0072] When the angles of the backrest plate 7 and the leg support plate 10 need to be adjusted, the first knob 301 is turned to drive the bidirectional screw rod 303 to rotate through the transmission rod 302. At the same time, the two movable push plates 305 drive the locking plug block 304 and the locking clamping plate 306 to move synchronously through the threads under the drive of the bidirectional screw rod 303. At this time, the locking plug block 304 is separated from the outer wall of the positioning rotating plate 203 by movement, so that the locking of the positioning rotating plate 203 can be released.

[0073] Then, the backrest plate 7 is pushed to rotate along the outer wall of a group of fixed shafts 12. In this process, the positioning plug block 205 is squeezed by the outer wall of the backrest plate 7, and the connecting push plate 201 is pushed to slide along the inner wall of the support frame 5 through the limiting push plate 206 and the fixed push rod 207. At this time, the limiting push plate 206 is contracted by the displacement extrusion spring 208, and at the same time, the rack 204 is driven by the connecting push plate 201 to drive the gear 202 to rotate through meshing. At this time, the positioning rotating plate 203 is driven by the gear 202 to rotate synchronously. When a positioning slot is driven by the backrest plate 7 and moves to the end of the positioning plug block 205, the spring 208 pushes the limiting push plate 206 to reset by rebounding. At the same time, the positioning plug block 205 is pushed by the limiting push plate 206 to be inserted into the inside of the positioning slot, so as to realize the flipping positioning of the backrest plate 7;

[0074] Then, the leg support plate 10 is pulled to rotate, and the limit rotating plate 9 rotates synchronously under the drive of the leg support plate 10. At the same time, the leg support plate 10 squeezes the end of the positioning plug 205 and repeats the above operation, so as to realize the flip positioning of the leg support plate 10, and then the first knob 301 is rotated in the opposite direction, so that the backrest plate 7 and the leg support plate 10 can be fixed and locked;

[0075] When the user needs to transport a special passenger with limited mobility, rotating the first knob 301 can make the locking card plate 306 move along the inner wall of the limiting slot 309 until the locking card plate 306 contacts the inner wall of one end of the limiting slot 309, thereby releasing the locking of the positioning rotating plate 203 and releasing the docking fixation of the docking frame 307 and the base 6, and then push the backrest board 7 and the leg support board 10 to flip over respectively until the upper surfaces of the backrest board 7 and the leg support board 10 are in the same horizontal state with the upper surface of the seat cushion bottom plate 1, at this time, the reinforcing plate 8 is driven by the backrest board 7 to contact the outer wall of the support frame 5, so that the user can be in a lying state, and then the second knob 404 is rotated, at this time, the bolt 403 is driven by the second knob 404 to move along the inner wall of the reinforcing plate 8 through the thread until the bolt 403 and the backrest board 7 are separated from each other, thereby releasing the limit of the limiting slide bar 402;

[0076] The first support frame 401 is then pushed to drive the limiting slide bar 402 to slide along the inner wall of the backrest plate 7. At this time, the reinforcing rod 405 is inserted into the inside of the limiting slot under the push of the limiting slide bar 402, so that the seat cushion base plate 1 and the backrest plate 7 can be reinforced at the rotation position. Then, the second knob 404 can be turned to reset the bolt 403, so that the limiting slide bar 402 can be limited and fixed. Then, the seat cushion base plate 1, the backrest plate 7, and the leg support plate 10 can be lifted through the second support frame 11 and the first support frame 401. In this process, the locking card plate 306 slides along the inner wall of the limiting card slot 309 through the docking plug-in frame 307 under the drive of the support frame 5 until the docking plug-in frame 307, the docking plug-in plate 308 and the base 6 are separated from each other, so that the seat can be temporarily used as a stretcher to transport special passengers with limited mobility in a seamless manner.

[0077] The above is only a specific implementation of the present disclosure, but the protection scope of the present disclosure is not limited thereto. Any person skilled in the art who is familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present disclosure, which should be included in the protection scope of the present disclosure. Therefore, the protection scope of the present disclosure should be based on the protection scope of the claims.

Claims

1. An aviation seat with automatic auxiliary fixation, comprising a seat cushion bottom plate (1), a base (6) is arranged below the seat cushion bottom plate (1), a support frame (5) is arranged on the upper surface of the base (6), the seat cushion bottom plate (1) is located on the inner side of the support frame (5), the outer wall of the seat cushion bottom plate (1) is symmetrically fixedly connected with two groups of fixed shafts (12), both groups of the fixed shafts (12) are fixedly connected to the support frame (5), the outer wall of one group of the fixed shafts (12) is slidably sleeved with a leg support plate (10), the leg support plate (10) is located at one end of the base (6), the outer wall of the other group of the fixed shafts (12) is slidably sleeved with a backrest plate (7), and the backrest plate (7) is fixedly connected with a reinforcing plate (8) at one end away from the seat cushion bottom plate (1), characterized in that: The support frame (5) is provided with a positioning mechanism for adjusting and positioning the backrest plate (7) and the leg support plate (10); The support frame (5) is provided with a locking mechanism for synchronously fixing and locking the support frame (5), the base (6), the backrest plate (7), and the leg support plate (10); The backrest plate (7) is provided with a reinforcement mechanism for connecting and reinforcing the seat cushion bottom plate (1) and the backrest plate (7).

2. The aviation seat with automatic auxiliary fixation according to claim 1, characterized in that: The positioning mechanism comprises: a rotating component arranged on a supporting frame (5); The rotating assembly comprises: a positioning rotating plate (203) arranged inside the supporting frame (5), the positioning rotating plate (203) being rotatably connected to the supporting frame (5), a gear (202) being fixedly connected to the top end of the positioning rotating plate (203), the gear (202) being located at the bottom end of the seat cushion bottom plate (1), and the gear (202) being rotatably connected to the seat cushion bottom plate (1); The gear (202) is provided with a moving component.

3. The aviation seat with automatic auxiliary fixation according to claim 2, characterized in that: The moving assembly comprises: two racks (204) symmetrically meshed and connected to the outer wall of the gear (202); two connecting push plates (201) are symmetrically arranged inside the support frame (5); the two connecting push plates (201) are respectively located on the sides of the two racks (204) that are away from each other; the two connecting push plates (201) are respectively fixedly connected to the two racks (204); and the connecting push plates (201) and the racks (204) are both slidably connected to the support frame (5); The connecting push plate (201) is provided with a positioning assembly.

4. The aviation seat with automatic auxiliary fixation according to claim 3, characterized in that: The positioning assembly comprises: two fixed push rods (207) symmetrically fixedly connected to one end of the connecting push plate (201); the two fixed push rods (207) are fixedly connected to a limiting push plate (206) on one side away from the connecting push plate (201); the limiting push plate (206) is fixedly connected to a plurality of positioning plugs (205) at equidistant intervals in the circumferential direction on one side away from the fixed push rods (207); the plurality of positioning plugs (205) are all inserted into the inner side of the support frame (5); The positioning plugs (205) are all located on the outside of the fixed shaft (12); the outer wall of the positioning plugs (205) on one side away from the limiting push plate (206) is hemispherical; the backrest plate (7), the leg support plate (10) and the positioning plugs (205) are all provided with positioning slots that match the outer wall of the positioning plugs (205); the positioning plugs (205), the limiting push plate (206) and the fixed push rod (207) are all slidably connected to the support frame (5); The fixed push rod (207) is provided with a reset assembly.

5. The aviation seat with automatic auxiliary fixation according to claim 4, characterized in that: The reset component is a spring (208) sleeved on the outer wall of the fixed push rod (207), one end of the spring (208) contacts the inner wall of the support frame (5), and the other end of the spring (208) contacts the outer wall of the limit push plate (206).

6. The aviation seat with automatic auxiliary fixation according to claim 1, characterized in that: The locking mechanism comprises: a docking assembly arranged on the support frame (5); The docking assembly comprises: two groups of docking plug-in trays (308) symmetrically fixedly connected to the bottom end of the support frame (5), the bottom outer wall of the docking plug-in tray (308) is in the shape of a truncated cone, the bottom end of the support frame (5) is fixedly connected with a docking plug-in frame (307), the docking plug-in frame (307) is located between the two groups of docking plug-in trays (308), the outer walls on both sides of the docking plug-in frame (307) are in the shape of an inclined surface, and a docking slot that matches the outer wall of the docking plug-in frame (307) and the docking plug-in tray (308) is provided at the position where the base (6) is connected to the docking plug-in frame (307) and the docking plug-in tray (308); The docking frame (307) is provided with a rotating assembly.

7. The aviation seat with automatic auxiliary fixation according to claim 6, characterized in that: The rotating assembly comprises: a first knob (301) arranged at one end of the docking frame (307) away from the leg support plate (10), one end of the first knob (301) is fixedly connected to a transmission rod (302), the transmission rod (302) is located inside the docking frame (307), one end of the transmission rod (302) away from the first knob (301) is fixedly connected to a bidirectional screw rod (303), and the transmission rod (302) and the bidirectional screw rod (303) are both rotatably connected to the docking frame (307); The bidirectional screw rod (303) is provided with a clamping assembly.

8. The aviation seat with automatic auxiliary fixation according to claim 7, characterized in that: The clamping assembly comprises: two movable push plates (305) symmetrically sleeved on the outer wall of the bidirectional screw rod (303); the two movable push plates (305) are both threadedly connected to the bidirectional screw rod (303); the two movable push plates (305) are both slidably connected to the support frame (5) and the docking frame (307); the ends of the two movable push plates (305) close to each other are fixedly connected with a locking plug block (304); the outer wall of the end of the locking plug block (304) away from the movable push plate (305) is hemispherical, and the locking plug block (304) is connected to the support frame (5) and the docking frame (307); The support frame (5) passes through the interior of the positioning rotating plate (203), and the outer walls of the two movable push plates (305) are symmetrically fixedly connected with two locking card plates (306). The two locking card plates (306) pass through the docking plug-in frame (307) to the interior of the base (6). The locking card plates (306) are slidably connected to the docking plug-in frame (307). A limiting card slot (309) for the locking card plate (306) to slide is provided at the connection position between the base (6) and the locking card plate (306), and the inner wall of the limiting card slot (309) is L-shaped.

9. The aviation seat with automatic auxiliary fixation according to claim 1, characterized in that: The reinforcing mechanism comprises: a first support frame (401) arranged at the top of the backrest plate (7), the first support frame (401) penetrates into the interior of the backrest plate (7), the bottom end of the first support frame (401) is fixedly connected to a limiting slide bar (402), the limiting slide bar (402) is located inside the backrest plate (7), the outer wall of the limiting slide bar (402) is symmetrically fixedly connected with two groups of reinforcing plug rods (405), the two groups of reinforcing plug rods (405) are both located below the first support frame (401), the bottom outer wall of the reinforcing plug rod (405) is hemispherical, and the first support frame (401) , a limiting slide bar (402) and a reinforcing plug rod (405) are all slidably connected to the backrest plate (7); a limiting slot for the reinforcing plug rod (405) to slide is provided at one end of the seat cushion base plate (1) close to the backrest plate (7); a second knob (404) is provided at one end of the reinforcing plate (8) away from the backrest plate (7); a bolt (403) is fixedly connected to one end of the second knob (404); the bolt (403) passes through the reinforcing plate (8) to the inside of the backrest plate (7); the bolt (403) contacts the outer wall of the limiting slide bar (402); and the bolt (403) is threadedly connected to the reinforcing plate (8).

10. The aviation seat with automatic auxiliary fixation according to claim 1, characterized in that: The top end of the leg support plate (10) is fixedly connected to a limit rotation plate (9), the limit rotation plate (9) is rotatably connected to the seat cushion bottom plate (1), and the bottom end of the leg support plate (10) is fixedly connected to a second support frame (11).

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