Aviation interface

An interface and aviation technology, applied in the aviation field, can solve the problems of short service life and low reliability, and achieve the effect of improving protection performance, reliability and service life

Pending Publication Date: 2020-01-24
GUIYANG AVIATION MOTOR
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the deficiencies of the prior art, the present invention provides an aviation inter

Method used

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Example Embodiment

[0026] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0027] see Figure 1-5 , including the wave protective shell 1 and the lateral displacement rod 6, the protective shell 1 is made of carbon fiber glass composite material, the carbon fiber has the advantages of high strength and light weight, and the carbon fiber has good electromagnetic shielding. The front of the protective shell 1 is equipped with ventilation The device 2, the right side wall of the protective casing 1 is fixedly c...

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Abstract

The invention relates to the technical field of aviation and discloses an aviation interface. The interface comprises a wave protection shell and a transverse displacement rod, wherein a ventilation device is arranged on a front face of the protection shell, and a wire connection interface is fixedly connected wit the position, close to the middle, of a right side wall of the protection shell. Theinvention discloses a high-reliability, long-service-life and light-weight aviation interface control device. Through cooperation of a pressure box, a support rod and a separation plate, internal equipment is damped in the vertical direction; through cooperation of a transverse displacement rod, a spring I, a longitudinal displacement rod and a spring II, shock absorption in horizontal directionis performed, horizontal damping is performed, influence of vibration on use of the equipment is prevented, the service life of the equipment is prolonged, internal circuit connection is contact connection, connection stability is high, use reliability is improved, the protective shell is made of a carbon fiber composite material, the carbon fiber has advantages of high strength and light weight,and the carbon fiber has good electromagnetic shielding performance.

Description

technical field [0001] The invention relates to the field of aviation technology, in particular to an aviation interface. Background technique [0002] The switches of aviation mechanical equipment are mostly controlled by electronic relays, and the protection of electronic relay circuit boards is extremely important. Aviation equipment is extremely sensitive to electromagnetics, so it is necessary to electromagnetically isolate the electronic relays. The protective effect is extremely important. The general protective shell has poor anti-shock effect, which affects its service life, and the protective shell is of high quality, which adds some burden to the aviation flight. SUMMARY OF THE INVENTION [0003] (1) Technical problems solved [0004] In view of the deficiencies of the prior art, the present invention provides an interface for aviation, which solves the problems of short service life and low reliability of common interface devices. [0005] (2) Technical solut...

Claims

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Application Information

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IPC IPC(8): H01H50/02H01H50/12F16F15/04
CPCF16F15/04H01H50/02H01H50/12
Inventor 王开登
Owner GUIYANG AVIATION MOTOR
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