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A kind of radar assembly and its aircraft

A technology of radar and assembly, which is applied in the field of radar assembly and aircraft with it, can solve the problems affecting the aerodynamic characteristics of aircraft and the inability to realize circumferential 360° detection, etc.

Active Publication Date: 2017-03-08
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1. Since the infrared detection system will protrude from the airframe, it will affect the aerodynamic characteristics of the aircraft;
[0004] 2. Due to the occlusion of the body, the infrared detection system cannot realize 360° detection in the circumferential direction

Method used

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  • A kind of radar assembly and its aircraft

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Embodiment Construction

[0018] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a radar assembly and an aircraft with the same. The radar assembly is arranged on the aircraft and comprises a radome, a rotating table, radar supports in the radome, and radar array planes in the radome. The radome, the radar supports and the radar array planes are arranged on the rotating table. The rotating table can rotate relative to the aircraft. Detection windows are formed in the radome. The radar assembly further comprises infrared radar arranged in the radome and supported by the radar supports. Probes of the infrared radar can detect the external situation of the radome through the detection windows in the radome. In the radar assembly, the probes of the infrared radar can detect the external situation of the radome through the detection windows in the radome. Compared with the prior art, the infrared radar and radome are integrated, the infrared radar is prevented from protruding out of an aircraft body, and the aerodynamic force and performance of the aircraft can not be influenced.

Description

technical field [0001] The invention relates to the technical field of aircraft radar, in particular to a radar assembly and an aircraft with the same. Background technique [0002] In the prior art, the infrared detection system is usually installed at the nose position of the aircraft, and the installation at this position has the following disadvantages: [0003] 1. Since the infrared detection system will protrude from the airframe, it will affect the aerodynamic characteristics of the aircraft; [0004] 2. Due to the occlusion of the body, the infrared detection system cannot realize 360° detection in the circumferential direction. [0005] Therefore, it is desirable to have a technical solution to overcome or at least alleviate at least one of the above-mentioned drawbacks of the prior art. Contents of the invention [0006] It is an object of the present invention to provide a radar assembly that overcomes or at least alleviates at least one of the above-mentioned...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D47/00
Inventor 梁欣杰董强王永超
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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