A surface contact bus device

A bus device and surface contact technology, which is applied in the field of aviation communication, can solve the problems of complex interface definition requirements and difficult application of aircraft, and achieve the effects of avoiding physical interfaces, improving thermal protection ability, and improving the strength of projectiles

Active Publication Date: 2018-01-30
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the 1553B bus interface is used for communication between the aircraft platform and the mounted weapons. This interface is widely used in various types of weapons and equipment, and has complete relevant standards; however, this interface is a standard physical interface, and there are complex interface definition requirements. In order to meet the requirements of this interface, all types of weapons and equipment must be adaptively designed; at the same time, the interface is an open interface, and there are certain technical problems with sealing protection, short circuit protection, heat protection, etc., resulting in higher environmental requirements or higher speed The aircraft is difficult to apply

Method used

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Embodiment Construction

[0014] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific illustrations.

[0015] see Figure 1~Figure 2 A surface-contact bus device includes a missile 1, an airborne surface-contact bus 2, a wing 3, an airborne signal adjustment modulator 4, a missile-borne signal adjustment modulator 5, and a missile-borne surface contact bus 6.

[0016] In this embodiment, the missile-borne surface contact bus 6 is installed on the surface of the missile 1, and the missile-borne signal adjustment modulator 5 is connected with the missile-borne surface contact bus 6 and installed in the missile 1; the airborne surface contact bus 2 is installed on the wing 3, and is arranged in corresponding contact with the missile-borne surface contact bus 6, and the airborne signal conditioning modulator 4 is connected to the airborne surfac...

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Abstract

A surface contact bus device, wherein the missile-borne surface contact bus is installed on the surface of the airborne weapon, the missile-borne signal adjustment modulator is connected to the missile-borne surface contact bus, and the missile-borne signal adjustment modulator is installed in the airborne weapon; At the same time, the airborne surface contact bus is installed at the corresponding contact position between the aircraft surface and the missile-borne surface contact bus, and the airborne signal adjustment modulator is connected to the airborne surface contact bus; in addition, the airborne surface contact bus and the missile-borne surface contact bus are respectively It is composed of several contact plates, and the contact plate is a grid structure; the missile-borne signal adjustment modulator is used to demodulate the signal sent by the airborne signal adjustment modulator and process the demodulated signal into a feedback signal, and then inject the feedback signal into the In the AC power supply signal provided by the airborne weapon, the communication between the carrier aircraft and the airborne weapon is realized; the docking method between the carrier aircraft and the airborne weapon is greatly simplified, so as to maintain the structural integrity of the airborne weapon body, especially suitable for hypersonic platforms and weapon use.

Description

technical field [0001] The invention relates to the technical field of aviation communication, in particular to a surface contact bus device. Background technique [0002] At present, the 1553B bus interface is used for communication between the aircraft platform and the mounted weapons. This interface is widely used in various types of weapons and equipment, and has complete relevant standards; however, this interface is a standard physical interface, and there are complex interface definition requirements. In order to meet the requirements of this interface, all types of weapons and equipment must be adaptively designed; at the same time, the interface is an open interface, and there are certain technical problems with sealing protection, short circuit protection, heat protection, etc., resulting in higher environmental requirements or higher speed The aircraft is difficult to apply. Contents of the invention [0003] The technical problem solved by the present inventio...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D7/00H04L12/40
CPCB64D7/00H04L12/40032
Inventor 韩宝瑞刘涛张邦楚许文杰周学武杨会林普睿铁程一周盛
Owner JIANGXI HONGDU AVIATION IND GRP
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