Aircraft wire harness laying structure

Abstract

The invention relates to the technical field of electronics, and discloses an aircraft wire harness laying structure which comprises a main plug, a first adapter, a second adapter, a third adapter and a fourth adapter. One end of the first adapter is connected with the main plug, and the other end of the first adapter is provided with a plurality of branch structures; the second adapter is a broken line type structure; and the third adapter is a broken line type structure. According to the laying structure, wiring harness sub-channel arrangement is realized through the first adapter so that the structure is simplified, and the first adapter can be flexibly matched with the second adapter, the third adapter and the fourth adapter for use so that wiring harness branches are connected with equipment; and the second adapter and the third adapter are located on the two sides of the fourth adapter, the broken line type structural design is adopted, the bending degree of the two sides of the wire harness can be reduced, the occupied space of the wire harness is reduced, the fourth adapter is in a U shape, the structure is suitable for being used in a complex environment, and the requirement for wire harness laying in a narrow space is met.

Description

technical field [0001] The invention relates to the field of electronic technology, in particular to an aircraft wire harness laying structure. Background technique [0002] There are some special areas on the aircraft, such as the landing gear compartment, the water tank, and the engine area. The internal environment of these special areas is relatively complicated. In the prior art, during the laying of the wire harness, it is usually necessary to add a protective cover to the wire harness In order to improve the adaptability of the wire harness, the protective sleeve generally does not have good flexibility, and the overall diameter of the wire harness after the protective sleeve is also increased, so the turning radius required during the wiring harness laying process is also increased. However, the space in these special areas is relatively narrow. In such a space, it is very difficult to complete the laying of the wiring harness, and it is often impossible to meet the ...

AI Technical Summary

Problems solved by technology

[0002] There are some special areas on the aircraft, such as the landing gear compartment, the water tank, and the engine area. The internal environment of these special areas is relatively complicated. In the prior art, during the laying of the wire harness, it is usually necessary to add a protective cover to the wire harness In order to improve the adaptability of the wire harness, the protective sleeve generally does not have good flexibility, and the overall diameter of the wire harness after the protective sleeve is also increased, so the turning radius required during the wiring harness laying process is also increased. However, the space in these special areas is relatively narrow. In such a space, it is very difficult to complete the laying of the wiring harness, and often cannot meet the laying requirements of the wiring harness.

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