retractable electrical connector

Abstract

The invention provides a retractable electrical connector, which includes: a housing, an electrical connector joint, an electric rotating shaft, a control cable, a telescopic mechanism and a control box. Among them: the electrical connector joint is installed in the fixed vertebral body structure of the housing, which is used to connect the airborne equipment and the aircraft pylon; the control box is installed in the fixed box structure of the housing; the electrical connector joint, the electric shaft , The control cable and the telescopic mechanism are arranged between the two ends of the shell in a telescopic structure; the electric shaft is installed at the root of the electrical connector joint; the telescopic mechanism is arranged between the electric shaft and the control box; the control cable stretches along the Inside the mechanism, the control box and the electric shaft are connected. The embodiment of the present invention releases the fixed constraint of the airborne hanger on the position of the equipment separation plug, without affecting the shape design and flight performance of the aircraft; it is not only applicable to small air-to-air aircraft, but also to large airborne equipment.

Description

technical field [0001] The invention relates to the technical field of launch of airborne equipment, in particular to a retractable electrical connector. Background technique [0002] The existing airborne equipment launch hanger is generally connected with an electrical connector and a separate plug of the airborne equipment to provide information and energy exchange between the airborne equipment and the equipment. [0003] The current electrical connectors are generally fixed electrical connectors. Due to the fixed position of this electrical connector, the equipment that needs to be mounted must be designed to separate the plug according to the corresponding position, which brings great difficulties to the design of the equipment, especially For airborne equipment such as aircraft, due to the influence of equipment such as engines, the separation plug needs to bypass these equipment for position arrangement, which will adversely affect the shape design and flight perform...

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is: the electrical connector cannot be used universally, and can only be applied to small air-to-air aircraft, but cannot be applied to large-scale airborne equipment; it affects the shape design and flight performance of the aircraft

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