Aviation wiring harness pin cable marker assembling device
By introducing an adsorption connection component and an assembly component into the aviation wiring harness pin number tube assembly device, and utilizing the combination of an inner arc-shaped airbag and a magnetic suction plate, the problem of insufficient connection strength in the prior art is solved, achieving a stable connection between the number tube and the pin, adapting to different tube diameters, and improving assembly efficiency and reliability.
Patent Information
- Application Number
- CN202423295735.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-31
- Publication Date
- 2025-11-28
- Estimated Expiration
- 2034-12-31
AI Technical Summary
The existing aviation wiring harness pin number tube assembly device lacks clamping components that can adapt to different tube diameters during insertion, resulting in low connection strength, easy slippage, and affecting normal arrangement and use.
An assembly device for aviation connector pin number tubes was designed, comprising an adsorption connection component and an assembly component. The adsorption connection component achieves tight contact and magnetic connection of the number tubes through the combination of an inner arc-shaped air bladder and a magnetic suction plate, thereby enhancing the assembly strength. The assembly component completes the initial assembly through the contact of the magnetic suction plate and uses an air pump to supply gas to inflate the inner arc-shaped air bladder, ensuring a stable connection.
It improves the connection strength between the number tube and the pin, prevents slippage, ensures good arrangement effect, adapts to pins of different tube diameters, and improves the use effect of the assembly device.
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Figure CN223604291U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to wiring terminal number pipe coding assembly technical field, concretely is an aviation wiring harness pin number pipe assembly device. BACKGROUND
[0002] In the aviation field, as the key component of the aircraft electrical system, the wiring harness undertakes the important responsibility of signal transmission and power transmission. In order to ensure the stable operation of the aircraft electrical system, the accurate identification and connection of each pin in the wiring harness are crucial. The number pipe, as a key component for identifying the function and number of the wiring harness pin, directly affects the maintenance convenience, fault troubleshooting efficiency of the aviation wiring harness and the reliability of the entire aircraft electrical system.
[0003] The prior art discloses a secondary aviation wiring harness pin number pipe assembly platform with a workbench, a metal conductive plate, a digital display plate and a power module are arranged on the workbench, and a slot is arranged for accommodating the secondary aviation plug. The metal conductive plate, the digital display plate, the power module, the slot and the secondary aviation plug in the slot form an electrical control loop. The slot has a conductive hole corresponding to each conductive metal terminal column of the secondary aviation plug, and the numbers on the digital display plate correspond to the numbers of each conductive metal terminal column of the secondary aviation plug. The number pipe coding and assembly are carried out on the workbench, the process is simple and reliable, the production efficiency is high, the error rate is greatly reduced, the labor cost, equipment installation and maintenance cost of the enterprise are also very low, and the production efficiency of the related electrical components is improved.
[0004] The above-mentioned aviation wiring harness pin number pipe assembly device inserts the required coding and assembled number pipe into the slot on the workbench, so that the number pipe coding and assembly can be carried out on the workbench. The above-mentioned wiring harness pin number pipe is simply inserted during assembly, but no clamping assembly for adapting pins of different pipe diameters is provided during insertion, resulting in low connection strength after pipe insertion, easy sliding off from the rear and affecting normal arrangement and use. The effect is not good during use, and improvement is needed. UTILITY MODEL CONTENTS
[0005] The utility model aims at providing an aviation wiring harness pin number pipe assembly device to solve the problems in the above background.
[0006] To achieve the above-mentioned purpose, the utility model provides the following technical scheme: an aviation wiring harness pin number pipe assembly device, comprising a workbench plate, a pin placement plate is arranged on the back of the workbench plate, a suction connection assembly is arranged on the top of the pin placement plate, and an assembly assembly is arranged on the top of the suction connection assembly.
[0007] The adsorbing connecting assembly comprises a gas pump, a hollow strip plate, an arc hollow connecting pad, an inner arc-shaped air bag, a first magnetic plate, a second magnetic plate and a connecting air pipe, the gas pump is fixedly connected to the top of the pin placing plate, the connecting air pipe is fixedly connected to the right side of the gas pump, the hollow strip plate is fixedly connected to the top of the pin placing plate, the inner arc-shaped air bag is connected to the inside of the pin placing plate, the arc hollow connecting pad is fixedly connected to the back of the hollow strip plate, the hollow strip plate and the arc hollow connecting pad are in communication, the inner arc-shaped air bag is connected to the back of the arc hollow connecting pad, the first magnetic plate is fixedly connected to the top of the pin placing plate, and the second magnetic plate is fixedly connected to the top of the pin placing plate.
[0008] Preferably, the assembling assembly comprises a number tube, a pin, a connecting block, a placing piece and a magnetic plate piece, the number tube is inserted into the inside of the inner arc-shaped air bag, the pin is fixedly connected to the front of the number tube, the connecting block is fixedly connected to the top of the number tube, the placing piece is fixedly connected to the side of the connecting block, and the magnetic plate piece is fixedly connected to the bottom of the placing piece.
[0009] Preferably, the number of the magnetic plate pieces is two, and the distance between the two magnetic plate pieces is equal to the distance between the first magnetic plate and the second magnetic plate.
[0010] Preferably, the top area of the first magnetic plate is equal to the bottom area of one magnetic plate piece.
[0011] Preferably, the magnetic plate piece is magnetically connected to the first magnetic plate, the magnetic plate piece is magnetically connected to the second magnetic plate, the magnetic plate piece is in contact with the first magnetic plate and the second magnetic plate, and the first magnetic plate and the second magnetic plate are magnetically connected together after being in contact, thereby achieving magnetic limiting, increasing the connecting strength of the number tube after assembling, and preventing the number tube from slipping off.
[0012] Preferably, the top of the pin placing plate is provided with a number tube insertion semicircular groove, and the diameter of the number tube insertion semicircular groove is matched with the diameter of the inner arc-shaped air bag.
[0013] Preferably, the top left side of the inner arc-shaped air bag is fixedly connected with a connecting pipe piece, one end of the connecting pipe piece, away from the top of the inner arc-shaped air bag, is fixedly connected to the back of the arc hollow connecting pad, gas can enter the inside of the inner arc-shaped air bag to make the inner arc-shaped air bag inflate, the inner arc-shaped air bag can be tightly combined with the surface of the number tube, thereby achieving the purpose of limiting connection, and the connecting pipe piece is arranged to realize the communication between the arc hollow connecting pad and the inner arc-shaped air bag, thereby ensuring that the gas can enter the inside of the inner arc-shaped air bag and ensuring that the device can be normally used.
[0014] Compared with the prior art, the device has the following beneficial effects:
[0015] 1. The aviation plug wire harness pin number tube assembly device, by setting up the adsorption connection assembly, the inner arc air bag can cover the large half position of the number tube surface, the adsorption connection area is large, the connection strength is high, so that the device can set the clamping assembly of the pin of different pipe diameters, the connection strength is enough after the pipe body is inserted, it is not easy to slip from the rear and affect the normal arrangement use, the effect is good when using.
[0016] 2. The aviation plug wire harness pin number tube assembly device, by setting up the assembly assembly, the number tube is aligned with the inside of the inner arc air bag and inserted, when inserted, it can be inserted into the last end first, then pushed forward from back to front, and continuously pushed until the magnetic attraction plate part at the bottom of the placing part contacts the first magnetic attraction plate and the second magnetic attraction plate, after the two contact, they can be magnetically connected together, completing the preliminary assembly of the number tube and the pin. BRIEF DESCRIPTION OF DRAWINGS
[0017] Figure 1 It is the overall three-dimensional structure schematic diagram of the utility model;
[0018] Figure 2 It is the utility model Figure 1 The enlarged structure schematic diagram in A place of the utility model;
[0019] Figure 3 It is the utility model Figure 1 The enlarged structure schematic diagram in B place of the utility model;
[0020] Figure 4 It is the pin placing plate and adsorption connection assembly three-dimensional structure schematic diagram of the utility model;
[0021] Figure 5 It is the utility model Figure 4 The enlarged structure schematic diagram in C place of the utility model.
[0022] In the drawing: 1, workbench plate; 2, pin placing plate; 3, adsorption connection assembly; 301, air pump; 302, hollow strip plate; 303, arc hollow connection pad; 304, inner arc air bag; 305, first magnetic attraction plate; 306, second magnetic attraction plate; 307, connecting air pipe; 4, assembly assembly; 401, number tube; 402, pin; 403, connecting block; 404, placing part; 405, magnetic attraction plate part. DETAILED DESCRIPTION
[0023] The technical scheme in the embodiments of the utility model will be described clearly and completely in combination with the drawings in the embodiments of the utility model, obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor belong to the scope of protection of the utility model.
[0024] Please refer to Figures 1-5 The utility model provides the following technical scheme:
[0025] An aviation plug wire harness pin number tube assembly device, including workbench plate 1, the back of workbench plate 1 is provided with pin placement plate 2, the top of pin placement plate 2 is provided with suction connection assembly 3, the top of suction connection assembly 3 is provided with assembly component 4.
[0026] Suction connection assembly 3 includes air pump 301, hollow strip plate 302, arc hollow connection pad 303, inner arc air bag 304, first magnetic suction plate 305, second magnetic suction plate 306 and connecting air pipe 307, air pump 301 is fixedly connected to the top of pin placement plate 2, connecting air pipe 307 is fixedly connected to the right side of air pump 301, hollow strip plate 302 is fixedly connected to the top of pin placement plate 2, inner arc air bag 304 is connected to the inside of pin placement plate 2, arc hollow connection pad 303 is fixedly connected to the back of hollow strip plate 302, hollow strip plate 302 and arc hollow connection pad 303 are communicated, inner arc air bag 304 is connected to the back of arc hollow connection pad 303, first magnetic suction plate 305 is fixedly connected to the top of pin placement plate 2, second magnetic suction plate 306 is fixedly connected to the top of pin placement plate 2, the top left side of inner arc air bag 304 is fixedly connected with connecting pipe piece, the end, away from the top of inner arc air bag 304, of connecting pipe piece is fixedly connected to the back of arc hollow connection pad 303, gas can enter the inside of inner arc air bag 304 so that inner arc air bag 304 inflates and expands, can be closely attached to the surface of number tube 401, and play the purpose of limiting connection, and the setting of connecting pipe piece lets arc hollow connection pad 303 and inner arc air bag 304 be communicated, ensure that gas can enter the inside of inner arc air bag 304, ensure that the device can be normally used, the top area of first magnetic suction plate 305 is equal to the bottom area of a magnetic suction plate piece 405, the top of pin placement plate 2 is provided with number tube insertion semicircular groove, and the diameter of number tube insertion semicircular groove is adapted to the diameter of inner arc air bag 304.
[0027] The assembling component 4 comprises a number tube 401, a pin 402, a connecting block 403, a placing piece 404 and two magnetic plate pieces 405, the number tube 401 is inserted into the inner arc-shaped air bag 304, the pin 402 is fixedly connected to the front surface of the number tube 401, the connecting block 403 is fixedly connected to the top of the number tube 401, the placing piece 404 is fixedly connected to the side surface of the connecting block 403, the two magnetic plate pieces 405 are fixedly connected to the bottom of the placing piece 404, the distance between the two magnetic plate pieces 405 is equal to the distance between the first magnetic plate 305 and the second magnetic plate 306, the magnetic plate piece 405 is magnetically connected to the first magnetic plate 305, the magnetic plate piece 405 is magnetically connected to the second magnetic plate 306, the magnetic plate piece 405 contacts the first magnetic plate 305 and the second magnetic plate 306, and the two are magnetically connected together after contacting, thereby magnetically limiting the position, increasing the connection strength of the number tube 401 after assembling, and preventing the number tube 401 from slipping off.
[0028] In use, the number tube 401 is aligned with the inner arc-shaped air bag 304 and is inserted, the number tube 401 can be inserted into the end first, and then is pushed forward from back to front, and the pushing is continued until the magnetic plate piece 405 at the bottom of the placing piece 404 contacts the first magnetic plate 305 and the second magnetic plate 306, the two are magnetically connected together after contacting, thereby completing the preliminary assembly of the number tube 401 and the pin 402, and then the subsequent limiting and fixing need to be performed by using the adsorption connecting component 3, after the number tube 401 is placed, the air pump 301 is started to cooperate with the connecting air pipe 307 to input the gas into the inside of the hollow strip plate 302, the hollow strip plate 302 and the arc-shaped hollow connecting pad 303 are both connected with the inner arc-shaped air bag 304, so that the gas can enter the inside of the inner arc-shaped air bag 304 to make the inner arc-shaped air bag 304 inflate and expand, the inner arc-shaped air bag 304 can tightly contact the surface of the number tube 401, and the inner arc-shaped air bag 304 can cover more than half of the surface of the number tube 401, the adsorption connection area is large, the connection strength is high, the device can be provided with the clamping assembly suitable for the pins with different diameters, the connection strength after the pipe body is inserted is sufficient, the device is not easy to slip off from the rear to affect the normal arrangement and use, and the effect in use is good.
[0029] Although the embodiments of the present application have been shown and described, it should be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to the embodiments without departing from the principles and spirits of the present application, and the scope of the present application is defined by the appended claims and their equivalents.
Claims
1. An aircraft wiring harness pin numbering tube assembly device comprising a worktable plate (1), characterized in that: The back of the workbench plate (1) is provided with a pin placement plate (2), the top of the pin placement plate (2) is provided with a suction connection assembly (3), and the top of the suction connection assembly (3) is provided with an assembly assembly (4). The suction connection assembly (3) comprises a gas pump (301), a hollow strip plate (302), an arc hollow connection pad (303), an inner arc air bag (304), a first magnetic plate (305), a second magnetic plate (306) and a connecting air pipe (307), the gas pump (301) is fixedly connected to the top of the pin placement plate (2), the connecting air pipe (307) is fixedly connected to the right side of the gas pump (301), the hollow strip plate (302) is fixedly connected to the top of the pin placement plate (2), the inner arc air bag (304) is connected to the inside of the pin placement plate (2), the arc hollow connection pad (303) is fixedly connected to the back of the hollow strip plate (302), the hollow strip plate (302) and the arc hollow connection pad (303) are communicated, the inner arc air bag (304) is connected to the back of the arc hollow connection pad (303), the first magnetic plate (305) is fixedly connected to the top of the pin placement plate (2), and the second magnetic plate (306) is fixedly connected to the top of the pin placement plate (2).
2. An aircraft wiring harness pin numbering tube assembly according to claim 1, wherein: The assembly assembly (4) comprises a number tube (401), a pin (402), a connecting block (403), a placement piece (404) and a magnetic plate piece (405), the number tube (401) is inserted into the inner arc air bag (304), the pin (402) is fixedly connected to the front of the number tube (401), the connecting block (403) is fixedly connected to the top of the number tube (401), the placement piece (404) is fixedly connected to the side of the connecting block (403), and the magnetic plate piece (405) is fixedly connected to the bottom of the placement piece (404).
3. An aircraft wiring harness pin numbering tube assembly according to claim 2, wherein: The number of the magnetic plate piece (405) is two, and the distance between the two magnetic plate pieces (405) is equal to the distance between the first magnetic plate (305) and the second magnetic plate (306).
4. An aircraft wiring harness pin numbering tube assembly according to claim 2, wherein: The top area of the first magnetic plate (305) is equal to the bottom area of the magnetic plate piece (405).
5. An aircraft wiring harness pin numbering tube assembly according to claim 2, wherein: The magnetic plate piece (405) is magnetically connected to the first magnetic plate (305), and the magnetic plate piece (405) is magnetically connected to the second magnetic plate (306).
6. An aircraft wiring harness pin numbering tube assembly as defined in claim 1 wherein: The top of the pin placement plate (2) is provided with a number tube insertion semicircular groove, and the diameter of the number tube insertion semicircular groove is matched with the diameter of the inner arc air bag (304).
7. An aircraft wiring harness pin numbering tube assembly as defined in claim 1 wherein: The top left side of the inner arc air bag (304) is fixedly connected with a connecting pipe piece, and the end of the connecting pipe piece away from the top of the inner arc air bag (304) is fixedly connected to the back of the arc hollow connection pad (303).
Citation Information
Patent Citations
Secondary aviation plug wire harness pin number tube assembling platform
CN204480928U