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Surface contact type bus device

A bus device and surface contact technology, 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 capabilities, and reducing missile weight.

Active Publication Date: 2016-10-12
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, goals 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 surface con...

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Abstract

The invention provides a surface contact type bus device. A missile-borne surface contact bus is installed on the surface of an airborne weapon. A missile-borne signal adjustment modulator is connected with the missile-borne surface contact bus. The missile-borne signal adjustment modulator is installed in the airborne weapon. Meanwhile, an airborne surface contact bus is installed in the position, in contact with the missile-borne surface contact bus correspondingly, of the surface of an aircraft. An airborne signal adjustment modulator is connected with the airborne surface contact bus. In addition, the airborne surface contact bus and the missile-borne surface contact bus are each composed of a plurality of contact plates. The contact plates are of a grid structure. The missile-mounted signal adjustment modulator is used for modulating a signal transmitted from the airborne signal adjustment modular and processing the modulated signal into a feedback signal, then the feedback signal is modulated and input into an alternating-current power supply signal provided by the airborne weapon, and therefore communication between a carrying aircraft and the airborne weapon is achieved. The butt joint mode between the carrying aircraft and the airborne weapon is substantially simplified, the integrity of an airborne weapon missile structure is maintained, and the surface contact type bus device is especially suitable for hypersonic platforms and weapons.

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 Applications(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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