Damping device for preventing pilot seat from suddenly moving backwards

By designing a damping device in the pilot seat and using the combination of liquid and a one-way valve, the problem of accidental sliding backward of the pilot seat is solved, and the stability of aircraft direction control and the convenience of seat adjustment are achieved.

CN222432589UActive Publication Date: 2025-02-07CIVIL AVIATION FLIGHT UNIV OF CHINA
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Patent Information

Application Number
CN202421391178.9
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-18
Publication Date
2025-02-07
Estimated Expiration
2034-06-18

AI Technical Summary

Technical Problem

When the pilot's seat is frequently adjusted in the aircraft and is affected by the flight movement force, it is prone to accidentally slide backward, causing the pilot to lose direction control and increase the risk of the aircraft losing control.

Method used

A damping device including a base, a pilot seat body, and a damping assembly is designed. The damping assembly uses a cylindrical cylinder, piston and liquid to cooperate with a one-way valve and sealing ring to achieve the slowing of the liquid flow rate and increase resistance when the seat slides backward, which limits the sliding speed of the seat.

Benefits of technology

Effectively prevent the pilot's seat from accidentally sliding backward, reduce the risk of aircraft out of control, and provide a fast and convenient operating experience when seat adjustments.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a damping device for preventing a pilot seat from suddenly moving backwards. The damping device comprises a base. When the pilot seat body is adjusted forwards, the pilot seat body drives the cylindrical cylinder body to move forwards, so that liquid on the rear portion of the piston flows towards the front portion of the piston, the liquid can flow through a small hole and a one-way valve in the piston at the moment, the flow speed of the liquid is large, resistance is small, and the seat can be conveniently and rapidly adjusted in place; when the pilot seat body is adjusted backwards, the pilot seat body drives the cylindrical cylinder body to move backwards, the one-way valve is closed at the moment, liquid can only flow through a small hole in the piston, the flow speed of the liquid is small, the resistance is large, and the moving speed of the pilot seat body is limited; the sliding speed is limited, the seat can slightly move backwards at a small speed, large influence on aircraft control of a pilot is avoided, meanwhile, the clamping rod and the clamping groove can be engaged again conveniently, the risk that the aircraft is out of control is avoided, and flight safety is guaranteed.
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Description

Technical Field

[0001] The utility model relates to the technical field of flight equipment, in particular to a damping device for preventing a pilot's seat from suddenly moving backwards. Background Art

[0002] The general aircraft seat adjustment method is manual adjustment. The front and rear adjustment is done by lifting the adjustment handle to disengage the seat teeth from the slide rail slots, allowing the seat to move forward and backward along the slide rails. Release the adjustment handle to engage the teeth with the slots to secure the seat.

[0003] Due to the small cockpit space of general aircraft, pilots have to adjust their seats every time they get on and off the plane, which makes the frequency of seat adjustment high and the teeth and slots are seriously worn. For training aircraft, there are still cases where the teeth and slots are not fully engaged due to improper operation by flight trainees. The pilot's rudder pedals put a lot of backward pressure on the seat, and the pressure is even greater when the aircraft accelerates rapidly or pitches up. These factors make the probability of the aircraft seat sliding backward accidentally high. Once the pilot's seat slides, due to the fast speed and strong force, it is difficult for the teeth and slots to bite again, and the seat usually slides directly to the last limit position. If the pilot's seat slides backward accidentally, the pilot's feet will leave the rudder pedals, and suddenly pull the stick to reduce the throttle, causing the aircraft to lose directional control and quickly lift up and slow down. If it occurs in the critical stage of flight, these operations will cause the aircraft to lose control and lead to serious consequences. During flight training, flight instructors will repeatedly emphasize and remind flight trainees to check their seats to prevent accidental backward sliding, but this situation still occurs from time to time. In order to ensure flight safety, we propose a damping device to prevent the pilot's seat from suddenly moving backward, which fundamentally prevents the pilot's seat from sliding accidentally. Utility Model Content

[0004] In view of the deficiencies of the prior art, the utility model provides a damping device to prevent the pilot seat from suddenly moving backwards, thereby solving the problem that the pilot seat accidentally slides backwards, causing the aircraft to lose directional control and quickly lift its head and decelerate.

[0005] The above technical objectives of the utility model are achieved through the following technical solutions:

[0006] A damping device for preventing a pilot seat from suddenly moving backwards comprises:

[0007] A base, wherein two slide rails are fixedly mounted on the top of the base;

[0008] A pilot seat body, wherein two slide posts are fixedly installed at the bottom of the pilot seat body, convex grooves are provided at the bottoms of the two slide posts, and the two slide rails are slidably installed in the two convex grooves respectively, a connection block is fixedly installed at the bottom surface of the pilot seat body, and a first mounting block and a second mounting block are fixedly installed at the top of the base;

[0009] A damping assembly is installed on the side where the second mounting block and the first mounting block are close to each other, and is used to buffer the backward movement impact of the pilot seat body.

[0010] Preferably, the damping assembly comprises:

[0011] A connecting rod, both ends of which are fixedly mounted on the sides of the second mounting block and the first mounting block that are close to each other;

[0012] A cylindrical cylinder body, the cylindrical cylinder body is fixedly installed on the bottom of the connecting block, one end of the connecting rod extends into the cylindrical cylinder body and is fixedly sleeved with a piston, a small hole is opened on the side of the piston, a connecting hole is opened on the side of the piston, a one-way valve is installed in the connecting hole, two sealing rings are fixedly installed on the inner wall of the cylindrical cylinder body, the outer side of the connecting rod is in contact with the inner walls of the two sealing rings, and liquid is arranged in the cylindrical cylinder body.

[0013] Preferably, a placement groove is provided on the top surface of the base, a breathable pad is fixedly installed inside the placement groove, and an installation groove is provided on the inner wall of the bottom side of the placement groove.

[0014] Preferably, a mounting box is fixedly installed inside the mounting groove, a plurality of through holes are respectively provided on the top surface and the front side of the mounting box, a cooling fan is fixedly installed inside the mounting box, an air inlet hole is provided on the rear side of one side of the mounting box, an air inlet pipe is fixedly installed on one side of the cooling fan, one end of the air inlet pipe is fixedly installed inside the air inlet hole, a mounting hole is provided on the inner wall of one side of the mounting groove, and one end of the air inlet pipe extends outside the mounting hole.

[0015] Preferably, a filter screen is fixedly installed inside the air intake pipe.

[0016] Preferably, a five-point safety belt is fixedly mounted on the outer wall surface of the pilot seat body.

[0017] Preferably, a protection groove is provided on one side of the pilot seat body, and a buffer pad is fixedly installed in the protection groove.

[0018] Preferably, a plurality of heating grooves are opened on one side of the interior of the protection groove, electric heating wires are fixedly installed inside the heating grooves, a heat conducting plate is fixedly installed on one side of the interior of the protection groove, and the heat conducting plate is arranged on the inner side of the buffer pad.

[0019] Preferably, a plurality of clamping holes are provided on the inner wall of the convex groove, and a clamping rod is installed in each of the plurality of clamping holes, a movable column is fixedly installed on one end of the plurality of clamping rods, a pulling frame is fixedly installed on one side of the movable column, a plurality of clamping slots are provided on the side of the slide rail, and the plurality of clamping rods are respectively moved into the plurality of clamping slots, a spring is sleeved on the clamping rod, and both ends of the spring are respectively fixedly installed on the sides of the movable column and the slide column close to each other.

[0020] In summary, the utility model mainly has the following beneficial effects:

[0021] In the utility model, when the pilot seat body is adjusted forward, the pilot seat body drives the cylindrical cylinder body to move forward, so that the liquid at the rear of the piston flows to the front of the piston. At this time, the liquid can flow through the small hole on the piston and the one-way valve. The liquid flow rate is large and the resistance is small, which is convenient for the seat to be quickly adjusted into place; when the pilot seat body is adjusted backward, the pilot seat body drives the cylindrical cylinder body to move backward. The one-way valve is closed at this time, and the liquid can only flow through the small hole on the piston. The liquid flow rate is small and the resistance is large, which limits the moving speed of the pilot seat body. When the seat accidentally slides backward due to the failure of the locking rod and the locking groove to engage well, the sliding speed is limited, and the seat will only move backward a small amount at a relatively small speed, which will not have a major impact on the pilot's control of the aircraft. At the same time, it is convenient for the locking rod and the locking groove to engage again, thereby avoiding the risk of aircraft loss of control and ensuring flight safety.

[0022] In the utility model, a breathable pad is provided to ventilate and dissipate heat to the driver's lower body, thereby preventing the buttocks from sweating due to long-term sitting and affecting the comfort level. A cooling fan is provided to allow external air to enter the interior of the installation box, and then the air flow is blown out through the through hole to take away the heat from the driver's lower body, thereby improving the heat dissipation effect.

[0023] In the utility model, a buffer pad is provided to comfortably wrap the driver's back, thereby preventing the driver from hitting the pilot seat body and causing damage to the driver, thereby improving the comfort level. A heating wire is provided to generate heat by energizing the heating wire, and then the heat is transferred to the buffer pad through the heat conduction plate. In an environment with a relatively low temperature, the driver can feel the temperature, thereby further improving the comfort level. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 This is a schematic diagram of the three-dimensional structure of the utility model from a first perspective;

[0025] Figure 2 It is a schematic diagram of the third perspective structure of the utility model;

[0026] Figure 3 yes Figure 2 Enlarged view of point A in the middle;

[0027] Figure 4 It is a side cutaway view of the utility model;

[0028] Figure 5 It is a schematic diagram of the installation box structure of the utility model;

[0029] Figure 6 It is a cutaway view of the installation box of the utility model;

[0030] Figure 7 It is a cross-sectional view of a cylindrical cylinder body of the utility model.

[0031] Figure numerals: 1. base; 2. slide rail; 3. slide column; 4. pilot seat body; 5. first mounting block; 6. connecting rod; 7. piston; 8. second mounting block; 9. cylindrical cylinder body; 10. sealing ring; 11. movable column; 12. breathable pad; 13. clamping rod; 14. mounting box; 15. through hole; 16. cooling fan; 17. air inlet hole; 18. air inlet pipe; 19. filter; 20. five-point safety belt; 21. spring; 22. pull frame; 23. valve; 24. one-way valve; 25. buffer pad; 26. heat transfer plate; 27. heating wire; 28. connecting block. DETAILED DESCRIPTION

[0032] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0033] Example 1

[0034] refer to Figure 1-Figure 7 , a damping device for preventing a pilot seat from suddenly moving backward, comprising:

[0035] A base 1, with two slide rails 2 fixedly mounted on the top of the base 1;

[0036] A pilot seat body 4, two slide posts 3 are fixedly installed at the bottom of the pilot seat body 4, convex grooves are provided at the bottoms of the two slide posts 3, two slide rails 2 are slidably installed in the two convex grooves respectively, a connection block 28 is fixedly installed on the bottom surface of the pilot seat body 4, and a first mounting block 5 and a second mounting block 8 are fixedly installed on the top of the base 1;

[0037] The damping assembly is installed on the sides of the second mounting block 8 and the first mounting block 5 that are close to each other, and is used to buffer the backward movement impact of the pilot seat body 4.

[0038] Preferably, the damping assembly comprises:

[0039] A connecting rod 6, both ends of which are fixedly mounted on the sides of the second mounting block 8 and the first mounting block 5 close to each other;

[0040] The cylindrical cylinder body 9 is fixedly mounted on the bottom of the connecting block 28. One end of the connecting rod 6 extends into the cylindrical cylinder body 9 and is fixedly sleeved with the piston 7. A small hole 23 is opened on the side of the piston 7. A connecting hole is opened on the side of the piston 7. A one-way valve 24 is installed in the connecting hole. Two sealing rings 10 are fixedly installed on the inner wall of the cylindrical cylinder body 9. The outer side of the connecting rod 6 contacts the inner walls of the two sealing rings 10. Liquid is arranged in the cylindrical cylinder body 9. The diameter of the one-way valve 24 is larger than the diameter of the small hole 23.

[0041] By means of the above structure: when the pilot seat body 4 is adjusted forward, the pilot seat body 4 drives the cylindrical cylinder body 9 to move forward, so that the liquid at the rear of the piston 7 flows to the front of the piston 7. At this time, the liquid can flow through the small hole 23 and the one-way valve 24 on the piston 7. The liquid flow rate is large and the resistance is small, which is convenient for the seat to be quickly adjusted into place; when the pilot seat body 4 is adjusted backward, the pilot seat body 4 drives the cylindrical cylinder body 9 to move backward, and the one-way valve 24 is closed at this time. The liquid can only flow through the small hole 23 on the piston 7. The liquid flow rate is small and the resistance is large, which limits the moving speed of the pilot seat body 4. When the seat accidentally slides backward due to the failure of the locking rod and the locking groove to engage well, the sliding speed is limited, and the seat will only move backward a small amount at a relatively small speed, which will not have a major impact on the pilot's control of the aircraft. At the same time, it is convenient for the locking rod and the locking groove to engage again, thereby avoiding the risk of aircraft loss of control and ensuring flight safety.

[0042] Example 2

[0043] A placement groove is provided on the top surface of the base 1, and a breathable pad 12 is fixedly installed inside the placement groove, and a mounting groove is provided on the inner wall of the bottom side of the placement groove; a mounting box 14 is fixedly installed inside the mounting groove, and a plurality of through holes 15 are respectively provided on the top surface and the front side of the mounting box 14, a cooling fan 16 is fixedly installed inside the mounting box 14, an air inlet hole 17 is provided at the rear side of one side of the mounting box 14, an air inlet pipe 18 is fixedly installed on one side of the cooling fan 16, one end of the air inlet pipe 18 is fixedly installed inside the air inlet hole 17, a mounting hole is provided on the inner wall of one side of the mounting groove, and one end of the air inlet pipe 18 extends outside the mounting hole; a filter screen 19 is fixedly installed inside the air inlet pipe 18. By providing a breathable pad 12, the driver's lower body can be ventilated and cooled through the breathable pad 12 to avoid sweating of the buttocks due to long-term sitting and affecting comfort. By providing a cooling fan 16, the outside air can enter the interior of the installation box 14 through the cooling fan 16, and then the air flow is blown out through the through hole 15 to take away the heat from the driver's lower body, thereby improving the heat dissipation effect.

[0044] A five-point safety belt 20 is fixedly installed on the outer wall surface of the pilot seat body 4. Through the arrangement of the five-point safety belt 20, safety is improved.

[0045] A protection groove is provided on one side of the pilot seat body 4, and a cushion pad 25 is fixedly installed in the protection groove; a plurality of heating grooves are provided on one side of the interior of the protection groove, and a heating wire 27 is fixedly installed in the interior of the heating groove, and a heat conducting plate 26 is fixedly installed on one side of the interior of the protection groove, and the heat conducting plate 26 is arranged on the inner side of the cushion pad 25. By providing the cushion pad 25, the back of the driver is comfortably wrapped, and the driver is prevented from hitting the pilot seat body 4, causing damage to the driver, and improving the comfort level. By providing the heating wire 27, the heating wire 27 is energized to generate heat, and then the heat is transferred to the cushion pad 25 through the heat conducting plate 26. In an environment with a relatively low temperature, the driver can feel the temperature, and the comfort level is further improved.

[0046] The inner wall of the convex groove is provided with a plurality of clamping holes, and clamping rods 13 are installed in each of the plurality of clamping holes. The moving column 11 is fixedly installed at one end of the plurality of clamping rods 13, and a pulling frame 22 is fixedly installed at one side of the moving column 11. The side of the slide rail 2 is provided with a plurality of clamping slots, and the plurality of clamping rods 13 are respectively moved into the plurality of clamping slots. The clamping rods 13 are sleeved with springs 21, and the two ends of the springs 21 are respectively fixedly installed on the sides of the moving column 11 and the slide column 3 that are close to each other. The position of the slide rail 2 can be fixed by setting the clamping slots and the clamping rods 13.

[0047] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A damping device for preventing a pilot's seat from suddenly moving backward, characterized in that: include: A base (1), wherein two slide rails (2) are fixedly mounted on the top of the base (1); A pilot seat body (4), wherein two slide posts (3) are fixedly mounted at the bottom of the pilot seat body (4), convex grooves are provided at the bottoms of the two slide posts (3), and the two slide rails (2) are respectively slidably mounted in the two convex grooves, a connection block (28) is fixedly mounted on the bottom surface of the pilot seat body (4), and a first mounting block (5) and a second mounting block (8) are fixedly mounted on the top of the base (1); A damping assembly is installed on the side of the second mounting block (8) and the first mounting block (5) close to each other, and is used to buffer the backward movement impact of the pilot seat body (4).

2. A damping device for preventing a pilot seat from suddenly moving backward according to claim 1, characterized in that: The damping assembly comprises: A connecting rod (6), both ends of which are fixedly mounted on the sides of the second mounting block (8) and the first mounting block (5) that are close to each other; A cylindrical cylinder body (9) is fixedly mounted on the bottom of the connecting block (28); one end of the connecting rod (6) extends into the cylindrical cylinder body (9) and is fixedly sleeved with a piston (7); a small hole (23) is provided on the side of the piston (7); a connecting hole is provided on the side of the piston (7); a one-way valve (24) is installed in the connecting hole; two sealing rings (10) are fixedly mounted on the inner wall of the cylindrical cylinder body (9); the outer side of the connecting rod (6) contacts the inner walls of the two sealing rings (10); and liquid is arranged in the cylindrical cylinder body (9).

3. A damping device for preventing a pilot seat from suddenly moving backward according to claim 1, characterized in that: The top surface of the base (1) is provided with a placement groove, a breathable pad (12) is fixedly installed inside the placement groove, and a mounting groove is provided on the bottom inner wall of the placement groove.

4. A damping device for preventing a pilot seat from suddenly moving backward according to claim 3, characterized in that: A mounting box (14) is fixedly installed inside the mounting groove, and a plurality of through holes (15) are respectively provided on the top surface and the front side of the mounting box (14), and a cooling fan (16) is fixedly installed inside the mounting box (14). An air inlet hole (17) is provided on the rear side of one side of the mounting box (14), and an air inlet pipe (18) is fixedly installed on one side of the cooling fan (16), and one end of the air inlet pipe (18) is fixedly installed inside the air inlet hole (17). A mounting hole is provided on the inner wall of one side of the mounting groove, and one end of the air inlet pipe (18) extends outside the mounting hole.

5. A damping device for preventing a pilot seat from suddenly moving backward according to claim 4, characterized in that: A filter screen (19) is fixedly installed inside the air intake pipe (18).

6. A damping device for preventing a pilot seat from suddenly moving backward according to claim 1, characterized in that: A five-point safety belt (20) is fixedly mounted on the outer wall surface of the pilot seat body (4).

7. A damping device for preventing a pilot seat from suddenly moving backward according to claim 1, characterized in that: A protection groove is provided on one side of the pilot seat body (4), and a buffer pad (25) is fixedly installed in the protection groove.

8. A damping device for preventing a pilot seat from suddenly moving backward according to claim 7, characterized in that: A plurality of heating grooves are provided on one side of the interior of the protection groove, and a heating wire (27) is fixedly installed inside the heating groove. A heat conducting plate (26) is fixedly installed on one side of the interior of the protection groove, and the heat conducting plate (26) is arranged on the inner side of the buffer pad (25).

9. A damping device for preventing a pilot seat from suddenly moving backward according to claim 1, characterized in that: A plurality of clamping holes are provided on the inner wall of the convex groove, and a clamping rod (13) is installed in each of the clamping holes. A moving column (11) is fixedly installed at one end of the clamping rod (13), and a pulling frame (22) is fixedly installed on one side of the moving column (11). A plurality of clamping slots are provided on the side of the slide rail (2), and the plurality of clamping rods (13) are respectively moved into the plurality of clamping slots. A spring (21) is sleeved on the clamping rod (13), and the two ends of the spring (21) are respectively fixedly installed on the sides of the moving column (11) and the slide column (3) close to each other.

Citation Information

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