A disconnectable aircraft wiring harness connector
Patent Information
- Application Number
- CN202521920933.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-09-08
- Publication Date
- 2026-08-18
- Estimated Expiration
- 2035-09-08
AI Technical Summary
针对现有技术的不足,本实用新型提供了一种分离式飞行器线束连接器,具备能够根据使用情况调整线束余量,安装便捷等优点,解决了无法增加线束余量,使用不方便的问题
1、该飞行器线束连接器,通过盒式分离面底座侧面开有不同高度的螺钉孔位,在孔的内侧预安装铆钉和托板螺母,盒式分离面对接的时候可通过固定侧面不同高度的孔位来控制线束余量。
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Figure CN224652805U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of aircraft technology, specifically to a detachable aircraft wiring harness connector. Background Technology
[0002] For electric vertical takeoff and landing (EVTOL) aircraft, batteries are used as the power source, and motors supply power to the batteries. High-voltage wiring harnesses connect the motors and batteries. To meet the requirements of vertical takeoff and landing, a high-power motor is needed. However, when transmitting large currents, the high-voltage wiring harnesses generate heat, which can easily cause a fire. Therefore, thicker high-voltage wiring harnesses are required to reduce resistance and thus reduce heat generation. At the same time, thicker wiring harnesses are heavier, making installation and disassembly more difficult. For example, in a 2.5-ton class EVTOL aircraft, the diameter of a single high-voltage wiring harness is approximately 17mm, and the total weight of the high-voltage wiring harness exceeds 100kg. For high-voltage wiring harnesses of this weight, the strength of the structural connections must be considered.
[0003] Chinese utility model patents, Publication No. CN111308618B and Application No. CN201911099757.X, disclose a pluggable active optical connector and a data transmission system. The device is modular with one or more channels and converts electrical signals into optical signals and vice versa. On one side, the device has a pluggable electrical interface for a field replaceable unit (LRU); on the other side, the device has a pluggable optical interface side for the aircraft's fiber optic cabling bundle. The device can accommodate different types of LRUs, including rack-mounted LRUs and bolt-mounted LRUs. The connector's separation surface is a flat plate, which does not allow for increased cabling slack.
[0004] Therefore, we propose a detachable aircraft wiring harness connector to solve the above problems. Utility Model Content
[0005] (a) Technical problems to be solved To address the shortcomings of existing technologies, this utility model provides a detachable aircraft wiring harness connector, which has the advantages of being able to adjust the wiring harness allowance according to usage conditions and being easy to install, thus solving the problems of not being able to increase the wiring harness allowance and inconvenience in use.
[0006] (II) Technical Solution To achieve the aforementioned goals of adjusting the wiring harness allowance according to usage and facilitating installation, this utility model provides the following technical solution: a detachable aircraft wiring harness connector, comprising a detachable base and a detachable box. One side of the detachable box is an opening, the size of which is determined according to the diameter of the wiring harness. The other side has a through-hole, the size of which is also determined according to the diameter of the wiring harness. A socket connector is also provided on the side of the detachable box with the through-hole, for connecting other devices. Both sides of the detachable base have through-holes, the size of which is determined according to the diameter of the wiring harness. The detachable base is fixedly connected to the detachable box, with two connection methods: one is that the detachable base extends into the detachable box through the opening and is fixedly connected to the detachable box; the other is that the detachable box extends into the detachable base through the through-hole and is fixedly connected to the detachable base. The wiring harness passes through the through-holes of the detachable base and the detachable box and connects to the socket connector.
[0007] As a further optimization of this utility model: the separation base includes a structural plate and a base, and double ear support plates are provided on both sides of the base. The base is fixed to the structural plate by the double ear support plates and screws and nuts. The wire hole is provided on the structural plate and the base on the opposite surface of the fixed surface of the structural plate, so that a wire harness channel is formed between the structural plate, the base and the separation box.
[0008] As a further optimization of this utility model: the circumference of the base is smaller than the circumference of the separation box, and the base extends into the separation box. By fitting the separation box over the base, the stability between the base and the separation box can be improved.
[0009] As a further optimization of this utility model: the opposite surfaces of the base are provided with multiple mounting holes along the wire harness direction, and a support plate nut is fixedly connected in the mounting holes. By setting multiple mounting holes and support plate nuts, the installation position of the screws can be controlled, thereby adjusting the position between the base and the separation box and controlling the length between the separation box and the base.
[0010] As a further optimization of this utility model: screws are provided on the opposite surfaces of the separation box, and the screws are connected with the tray nut to fix the separation box and the separation base. The separation box and the base can be fixed together by fixing the screws and the tray nut.
[0011] As a further optimization of this utility model: the circumference of the base is greater than the circumference of the separation box, and the separation box extends into the base. By fitting the base over the separation box, the stability between the base and the separation box can be improved.
[0012] As a further optimization of this utility model: the opposite surfaces of the separation box are provided with multiple mounting holes along the wire harness direction, and a support plate nut is fixedly connected in the mounting holes. By setting multiple mounting holes and support plate nuts, the installation position of the screw can be controlled, thereby adjusting the position between the base and the separation box and controlling the length between the separation box and the base.
[0013] As a further optimization of this utility model: screws are provided on the opposite surfaces of the base, and the screws are connected with the tray nut to fix the separation box and the separation base. The separation box and the base can be fixed together by fixing the screws and the tray nut.
[0014] As a further optimization of this utility model: the socket connector and the separation box are fixed by screws and a bracket nut, which facilitates the installation and disassembly of the socket connector.
[0015] As a further optimization of this utility model: the screw is a GB / T 70.1 M5 screw, and the plate nut is a GB / T 889.1 M5 anti-loosening self-locking nut, which further improves the stability between the separation box and the separation base.
[0016] (III) Beneficial Effects Compared with the prior art, this utility model provides a detachable aircraft wiring harness connector, which has the following advantages: 1. The aircraft wiring harness connector has screw holes of different heights on the side of the box-type split surface base. Rivets and support nuts are pre-installed on the inside of the holes. When the box-type split surface is connected, the wiring harness allowance can be controlled by fixing the holes of different heights on the side.
[0017] 2. The aircraft wiring harness connector has pre-installed support nuts and rivets in both the side holes of the box-type split surface base and the fixing holes of the box-type split surface connector. Therefore, workers only need a single tool to operate when installing the connector, avoiding the complexity of using tools. Attached Figure Description
[0018] Figure 1 This is a schematic diagram of the structure of this utility model; Figure 2 This is a schematic diagram of the structure of this utility model; Figure 3 This is a schematic diagram of the structure of this utility model.
[0019] In the diagram: 1. Structural plate; 2. Base; 3. Separator box; 4. Socket connector; 5. Wire hole; 6. Support plate nut; 7. Screw; 8. Wire harness. Detailed Implementation
[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.
[0021] Please see Figure 1-3 A detachable aircraft wiring harness connector includes a detachable base and a detachable box 3. One side of the detachable box 3 is an opening, the size of which is determined according to the diameter of the wiring harness 8. The other side has a wire-passing hole 5, the size of which is determined according to the diameter of the wiring harness 8. A socket connector 4 is also provided on the side of the detachable box 3 with the wire-passing hole 5. The socket connector 4 is used to connect other devices. Both sides of the detachable base have wire-passing holes 5, the size of which is determined according to the diameter of the wiring harness 8. The detachable base is fixedly connected to the detachable box 3. There are two connection methods: one is that the detachable base extends into the detachable box 3 through the opening of the detachable box 3 and is fixedly connected to the detachable box 3; the other is that the detachable box 3 extends into the detachable base through the wire-passing hole 5 and is fixedly connected to the detachable base. The wiring harness 8 passes through the detachable base and the wire-passing hole 5 of the detachable box 3 and is connected to the socket connector 4.
[0022] The separation base includes a structural plate 1 and a base 2. The base 2 has double ear plates on both sides. The base 2 is fixed to the structural plate 1 by the double ear plates and screws and nuts. The wire hole 5 is set on the fixed surface of the structural plate 1 and the opposite surface of the fixed surface of the base 2, so that a wire harness channel is formed between the structural plate 1, the base 2 and the separation box 3.
[0023] The circumference of base 2 is smaller than that of separation box 3. Base 2 extends into separation box 3. By fitting separation box 3 over base 2, the stability between base 2 and separation box 3 can be improved. Multiple mounting holes are provided on the opposite surfaces of base 2 along the wire harness direction. A support plate nut 6 is fixedly connected in the mounting holes. By setting multiple mounting holes and support plate nuts 6, the installation position of screw 7 can be controlled, thereby adjusting the position between base 2 and separation box 3 and controlling the length between separation box 3 and base 2. Screws 7 are provided on the opposite surfaces of separation box 3. Screws 7 are connected to support plate nuts 6 to fix separation box 3 and separation base. By fixing with screws 7 and support plate nuts 6, separation box 3 and base 2 can be fixed together.
[0024] The circumference of base 2 is greater than that of separation box 3. Separation box 3 extends into base 2. By fitting base 2 over separation box 3, the stability between base 2 and separation box 3 can be improved. Multiple mounting holes are provided on the opposite surfaces of separation box 3 along the wire harness direction. A support plate nut 6 is fixedly connected in the mounting holes. By setting multiple mounting holes and support plate nuts 6, the installation position of screw 7 can be controlled, thereby adjusting the position between base 2 and separation box 3 and controlling the length between separation box 3 and base 2. Screws 7 are provided on the opposite surfaces of base 2. Screws 7 are connected to support plate nuts 6 to fix separation box 3 and separation base. By fixing with screws 7 and support plate nuts 6, separation box 3 and base 2 can be fixed together.
[0025] The socket connector 4 is fixed to the separation box 3 by screws 7 and bracket nuts 6, which facilitates the installation and removal of the socket connector 4. Screws 7 are GB / T 70.1 M5 screws, and bracket nuts 6 are GB / T 889.1 M5 anti-loosening self-locking nuts, which further improves the stability between the separation box 3 and the separation base.
[0026] Working principle: First, fix the base 2 to the structure plate 1 with screws 7 and nuts. Then, fix the base 2 and the separation box 3 with screws 7 and support plate nuts 6. Determine the length between the base 2 and the separation box 3 according to the length of the wire harness 8. Then fix the socket connector 4 to the separation box 3. After completion, the wire harness 8 passes through the wire hole 5 of the structure plate 1, the base 2 and the separation box 3 and connects to the socket connector 4. The excess wire harness 8 can be placed in the space inside the base 2 and the separation box 3.
[0027] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A detachable aircraft wiring harness connector, comprising a detachable base and a detachable housing (3), characterized in that: The separation box (3) has an opening on one side and a wire hole (5) on the other side. The side of the separation box (3) with the wire hole (5) is also provided with a socket connector (4). Both sides of the separation base are provided with wire holes (5). The separation base is fixedly connected to the separation box (3). The wire harness (8) passes through the wire holes (5) of the separation base and the separation box (3) and is connected to the socket connector (4).
2. The detachable aircraft wiring harness connector according to claim 1, characterized in that: The separation base includes a structural plate (1) and a base (2). The base (2) is fixed on the structural plate (1). The wire hole (5) is provided on the structural plate (1) and the base (2) on the opposite side of the fixed surface of the structural plate (1).
3. A detachable aircraft wiring harness connector according to claim 2, characterized in that: The circumference of the base (2) is smaller than the circumference of the separation box (3), and the base (2) extends into the separation box (3).
4. A detachable aircraft wiring harness connector according to claim 3, characterized in that: The base (2) has multiple mounting holes on its opposite surfaces along the wire harness direction, and a support plate nut (6) is fixedly connected in the mounting holes.
5. A detachable aircraft wiring harness connector according to claim 4, characterized in that: Screws (7) are provided on the opposite surfaces of the separation box (3), and the screws (7) are connected to the tray nut (6) to fix the separation box (3) and the separation base.
6. A detachable aircraft wiring harness connector according to claim 2, characterized in that: The circumference of the base (2) is greater than the circumference of the separation box (3), and the separation box (3) extends into the base (2).
7. A detachable aircraft wiring harness connector according to claim 6, characterized in that: The separation box (3) has multiple mounting holes on its opposite sides along the wire harness direction, and a support plate nut (6) is fixedly connected in the mounting holes.
8. A detachable aircraft wiring harness connector according to claim 7, characterized in that: Screws (7) are provided on the opposite surfaces of the base (2), and the screws (7) are connected to the tray nut (6) to fix the separation box (3) and the separation base.
9. A detachable aircraft wiring harness connector according to claim 1, characterized in that: The socket connector (4) is fixed to the separation box (3) by screws (7) and plate nuts (6).
10. A detachable aircraft wiring harness connector according to claim 9, characterized in that: The screw (7) is a GB / T 70.1 M5 screw, and the plate nut (6) is a GB / T 889.1 M5 anti-loosening self-locking nut.
Citation Information
Patent Citations
Connectable to active optical connectors and data transmission systems
CN111308618B