Aircraft escape seat shoulder harness connector disassembly device and method
By designing a fixed platform, limiting holes, and a T-shaped disassembly wrench for the disassembly device of the shoulder strap connector of the aviation life-saving seat, the problem of the existing technology requiring two people to work together and being unsafe to operate is solved, and a safe and convenient disassembly operation can be achieved by a single person.
Patent Information
- Application Number
- CN202310217092.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2023-03-08
- Publication Date
- 2026-02-06
- Estimated Expiration
- 2043-03-08
AI Technical Summary
The existing method for disassembling the shoulder strap connector of an aircraft lifesaving seat requires two people to work together. Furthermore, because the fixing screws are coated with adhesive, a lot of force is required during disassembly, which can easily cause the screws to slip out and injure people, making the operation inconvenient.
A device for removing shoulder strap fasteners for aircraft lifesaving seats has been designed, including a fixing platform, a limiting hole, a limiting rod, and a T-shaped removal wrench. The fastener is fixed by the groove of the fixing platform and the limiting rod, and the fixing screw is removed by the T-shaped wrench, which reduces the number of operators and improves safety.
It enables a single person to independently disassemble and reassemble the shoulder strap connector, avoiding the safety risks associated with two people working together, and improving the convenience and safety of operation.
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Figure CN116160409B_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the field of aviation lifesaving, in particular to a kind of aviation lifesaving seat shoulder strap connecting buckle dismounting device and its dismounting method. BACKGROUND
[0002] Since the fixed shaft pin of shoulder strap connecting buckle is round bar structure, it is installed in connecting buckle mounting hole by tail threaded hole using fixing screw.The dismounting method of existing shoulder strap connecting buckle is as shown in Fig. Figure 1 When dismounting fixed shaft pin, one person must use knife to fix shaft pin at one end, and another person simultaneously uses knife to unscrew fixing screw, so that fixed shaft pin is dismounted from connecting buckle.Since fixing screw is coated with fixing glue on its thread when installing for the purpose of preventing loosening, greater force is required when dismounting fixed shaft pin, and fixed shaft pin is round bar structure, which cannot be effectively fixed when applying force and is prone to rotate, which is not conducive to applying force by hand, and the operation effect is poor.And when two people simultaneously apply force to dismount, personnel injury is prone to occur due to knife slipping out of screw groove. SUMMARY
[0003] In order to solve the above problems, the present application provides a kind of aviation lifesaving seat shoulder strap connecting buckle dismounting device and its dismounting method.
[0004] A kind of aviation lifesaving seat shoulder strap connecting buckle dismounting device, including fixed platform matched with shoulder strap connecting buckle, fixed screw one matched with side end position of fixed platform, limiting hole and fixed hole arranged on fixed platform, limiting rod matched with limiting hole, dismounting wrench for dismounting fixed screw two on shoulder strap connecting buckle.
[0005] As a further improvement of the present application, the fixed platform is provided with a groove matching the size of the shoulder strap connecting buckle.
[0006] As a further improvement of the present application, the fixed platform is further provided with a dismounting hole matched with the dismounting wrench.
[0007] As a further improvement of the present application, the dismounting hole is arranged on the inner wall of the groove.
[0008] As a further improvement of the present application, the fixed screw one is provided with a knife edge matching the fixed shaft pin of the shoulder strap connecting buckle.
[0009] As a further improvement of the present application, the knife edge has a clockwise thread.
[0010] As a further improvement of the present application, the dismounting wrench is a T-shaped wrench.
[0011] As another improvement of the present application, a dismounting method of aviation lifesaving seat shoulder strap connecting buckle dismounting device is provided, and the specific steps are as follows:
[0012] S1, the fixed shoulder strap connecting buckle: when the fixed shaft pin needs to be disassembled from the shoulder strap connecting buckle, only one person needs to put the shoulder strap connecting buckle into the groove of the fixed platform, install the fixed screw one and the limiting rod, and fix the shoulder strap connecting buckle;
[0013] S2, disassemble the fixed screw two: use the disassembly wrench to unscrew the fixed screw two of the shoulder strap connecting buckle through the disassembly hole;
[0014] S3, fixed limiting rod: the limiting rod prevents the shoulder strap connecting buckle from rotating in the groove after installation, and the disassembly wrench prevents the disassembly wrench from slipping off and causing personal injury when disassembling the fixed screw two of the shoulder strap connecting buckle through the disassembly hole.
[0015] The beneficial effects of the present application are: considering the shape and function of the fixed shaft pin, without changing the fixed shaft pin and the connecting buckle, the use is safer and the use is better through the additional device; after the improvement of the present application, the number of operating personnel can be reduced, the operation mode during disassembly can be improved, and a single person can easily complete the disassembly operation of the shoulder strap connecting buckle. BRIEF DESCRIPTION OF DRAWINGS
[0016] The present application will be further described below in combination with the drawings and examples.
[0017] Figure 1 The present application is a disassembly structure diagram of the existing shoulder strap connecting buckle;
[0018] Figure 2 The present application is a three-dimensional structure diagram. DETAILED DESCRIPTION
[0019] In order to make the technical means, creative features, purposes and effects of the present application easy to understand, the present application will be further described below.
[0020] As shown in Figure 1 and Figure 2 , an aviation lifesaving seat shoulder strap connecting buckle disassembly device, comprising a fixed platform 4 cooperating with the shoulder strap connecting buckle 1, a fixed screw one 5 cooperating with the side end position of the fixed platform 4, a limiting hole 9 and a fixed hole 8 arranged on the fixed platform 4, a limiting rod 6 cooperating with the limiting hole 9, and a disassembly wrench 7 for disassembling the fixed screw two 3 on the shoulder strap connecting buckle 1.
[0021] Considering the shape and function of the fixed shaft pin 2, without changing the fixed shaft pin 2 and the shoulder strap connecting buckle 1, the use is safer and the use is better through the additional device, through the improvement of the present application, the number of operating personnel can be reduced, the operation mode during disassembly can be improved, and a single person can easily complete the disassembly operation of the shoulder strap connecting buckle 1.
[0022] The fixed platform 4 is provided with a groove matching the size of the shoulder strap connecting buckle 1.
[0023] Specifically, by adopting the specially made groove matched with the fixing screw 5 and the limiting rod 6, the problem of rotation of the fixing shaft pin 2 in the shoulder strap connecting buckle 1 during disassembly is overcome.
[0024] The fixed platform 4 is further provided with a disassembly hole 10 matched with the disassembly wrench 7.
[0025] Specifically, the limiting rod 6 can be screwed into the limiting hole 9.
[0026] The disassembly hole 10 is arranged on the inner wall of the groove, which is convenient for operation.
[0027] The fixing screw 5 is provided with a knife edge matched with the fixing shaft pin 2 of the shoulder strap connecting buckle 1, which is convenient for force application during disassembly.
[0028] The knife edge has a clockwise thread, and has good fastening and stability, and will not cause the problem of knife slipping out of the screw groove and causing personal injury.
[0029] The disassembly wrench 7 is a T-shaped wrench.
[0030] Specifically, the disassembly wrench 7 is a T-shaped wrench, and has a large force arm, and can screw and take out the fixing screw 3 of the shoulder strap connecting buckle 1 through the disassembly hole 10.
[0031] Specifically, the T-shaped wrench is used to disassemble the fixing shaft pin 2 of the shoulder strap connecting buckle 1 through the disassembly hole 10, which can be operated by one person, is safe, and has more force for force application.
[0032] A disassembly method of an aviation lifesaving seat shoulder strap connecting buckle disassembly device, and the specific steps are as follows:
[0033] S1, fixing the shoulder strap connecting buckle 1: when the fixing shaft pin 2 needs to be disassembled from the shoulder strap connecting buckle, only one person needs to put the shoulder strap connecting buckle into the groove of the fixed platform 4, install the fixing screw 5 and the limiting rod 6, and fix the shoulder strap connecting buckle 1;
[0034] S2, disassemble the fixing screw 3: use the disassembly wrench 7 to screw down the fixing screw 3 of the shoulder strap connecting buckle 1 through the disassembly hole 10;
[0035] S3, fix the limiting rod 6: after the limiting rod 6 is installed, the shoulder strap connecting buckle 1 is prevented from rotating in the groove, the disassembly wrench 7 is prevented from slipping off to cause personal injury when disassembling the fixing screw 3 of the shoulder strap connecting buckle, and the T-shaped disassembly wrench 7 has a large force arm and is labor-saving during disassembly.
[0036] The application improves the safety of dismounting and mounting of the fixing shaft pin 2 of the shoulder strap connecting buckle 1, overcomes the problem of rotation of the fixing shaft pin 2 in the shoulder strap connecting buckle 1 during dismounting, facilitates the force exertion of the dismounting and mounting personnel at the fixing screw two 3, and also reduces the number of operators during dismounting of the fixing shaft pin 2, and the dismounting operation of the fixing shaft pin 2 can be completed by a single person.
[0037] The basic principles, main features and advantages of the application are shown and described above. Those skilled in the art should understand that the application is not limited by the above examples, and the above examples and descriptions in the specification are only the principles of the application. Without departing from the spirit and scope of the application, various changes and improvements can be made to the application, and these changes and improvements all fall within the scope of the claimed application. The scope of protection of the application is defined by the appended claims and their equivalents.
Claims
1. A device for removing shoulder strap fasteners from an aircraft lifesaving seat, characterized in that: The device includes a fixed platform (4) that mates with the shoulder strap buckle (1), a fixing screw (5) that mates with the side of the fixed platform (4), a limiting hole (9) and a fixing hole (8) on the fixed platform (4), a limiting rod (6) that mates with the limiting hole (9), and a disassembly wrench (7) for removing the fixing screw (3) on the shoulder strap buckle (1). The fixed platform (4) is provided with a groove that matches the size of the shoulder strap buckle (1). The fixed platform (4) is also provided with a disassembly hole (10) that mates with the disassembly wrench (7). The disassembly hole (10) is located on the inner wall of the groove.
2. The device for removing the shoulder strap connector of an aircraft lifesaving seat according to claim 1, characterized in that: The fixing screw (5) is provided with a cutting edge that matches the fixing pin (2) of the shoulder strap connecting buckle (1).
3. The device for removing the shoulder strap connector of an aircraft lifesaving seat according to claim 2, characterized in that: The cutting edge has a clockwise thread.
4. The device for removing the shoulder strap connector of an aircraft lifesaving seat according to claim 1, characterized in that: The aforementioned disassembly wrench (7) is a T-shaped wrench.
5. A method for disassembling the shoulder strap fastener disassembly device for an aircraft lifesaving seat according to any one of claims 1 to 4, characterized in that: The specific steps are as follows: S1. Fixing the shoulder strap buckle (1): When it is necessary to remove the fixing pin (2) from the shoulder strap buckle, one person can simply put the shoulder strap buckle into the groove of the fixing platform (4), install the fixing screw (5) and the limiting rod (6) to fix the shoulder strap buckle (1). S2, Remove fixing screw two (3): Use the removal wrench (7) to unscrew the fixing screw two (3) of the shoulder strap connecting buckle (1) through the removal hole (10); S3, Fixed limit rod (6): After the limit rod (6) is installed, it prevents the shoulder strap buckle (1) from rotating in the groove. The disassembly wrench (7) removes the fixing screw (3) of the shoulder strap buckle through the disassembly hole (10) to prevent the disassembly wrench (7) from slipping and causing injury to personnel.
Citation Information
Patent Citations
Super-hand-distance bolt and nut dismounting and mounting device
CN215660046U