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Modular radar wing

A modular wing technology, which is applied in the field of modular radar wings and modular wings with built-in phased array radar, can solve the problems of poor ground search performance, large radar cross section, and high center of gravity of aircraft to meet the requirements of Liquid cooling cycle cooling requirements, small air resistance, good detection environment effect

Inactive Publication Date: 2018-11-23
JIANGSU CHANGTAN ROBOT CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, none of these design schemes can meet the radar search requirements of modern aircraft, especially fighter planes and early warning aircraft.
At the same time, the disc-type early warning radar leads to a high center of gravity of the aircraft, high resistance, and the radar cross-section machine is very large and heavy
And due to the limitations of the installation location, the ground search performance is very poor!

Method used

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Embodiment Construction

[0020] The present invention will be further described below in conjunction with the drawings.

[0021] Such as Figure 1 to Figure 3 As shown, a modular radar wing is characterized in that the modular radar wing consists of a wing skeleton 714, a phased array radar module 711, a wing skin 715, a wing hinge 1028, and an electro-hydraulic gas interface 1036. .

[0022] As a further improvement of the present invention, the arrayed radar module 711 is composed of a large number of small antenna elements 713.

[0023] As a further improvement of the present invention, the phased array radar module 711 is installed in the wing skeleton 714.

[0024] As a further improvement of the present invention, the wing skin 715 is wrapped on the outside of the wing skeleton 714 and the phased array radar module 711.

[0025] As a further improvement of the present invention, the wing hinge 1028 is installed on the side close to the aircraft body. Used to connect the wing to the body.

[0026] As a f...

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Abstract

The invention discloses a modular radar wing. The modular radar wing is prepared from a win skeleton, a phased array radar module, a wing cover, a wing hinge and an electro-hydraulic-gas interface, wherein the phased array radar module is formed by a large amount of small-sized antenna elements. The whole modular radar wing forms a wing shape and is modularly designed, and replacement is convenient; the modular radar wing can be arranged on wings at two sides, so that radar research of a combat aircraft to the ground can be well realized; the modular radar wing can be arranged on a vertical tail wing, so that radar research of the combat aircraft to positions at two sides can be well realized; meanwhile, wing-shaped design is very beneficial for heat dissipation of the phased array radar module, and the problem of heat dissipation of radar is effectively solved; omni-directional dead zone-free research of an airborne early warning aircraft is realized, and inherent early warning disadvantages of the airborne early warning aircraft are improved.

Description

Technical field [0001] The invention relates to a modular radar wing, in particular to a modular wing with a built-in phased array radar, belonging to the field of aircraft equipment. Background technique [0002] The current radars are all designed with the nose of the aircraft, but there are also fixed-wing early warning aircraft that have the radar design and the status quo above the fuselage. However, none of these design schemes can meet the radar search requirements of modern aircraft, especially fighter aircraft and early warning aircraft. At the same time, the disc-type early warning radar causes the aircraft to have a high center of gravity and high resistance, and the radar cross section plane is very large and heavy. And because of the limitation of the installation location, the ground search performance is very poor! [0003] It is imperative to redesign the side-view radar and the top-view radar to meet the high mobility, top-down and side-view requirements of early...

Claims

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Application Information

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IPC IPC(8): B64C3/00B64C3/56B64C1/36
CPCB64C3/00B64C1/36B64C3/56
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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