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A stealth structure of a target drone paracord

A technology of parachute and target drone, which is applied in the field of stealth structure of the parachute of the target drone, which can solve the problems of being exposed on the outer surface of the body and not meeting the stealth requirements, and achieve the effect of solving the problem of stealth

Active Publication Date: 2018-04-13
沈阳飞机设计研究所扬州协同创新研究院有限公司
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  • Abstract
  • Description
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Problems solved by technology

[0002] The high-stealth target drone lands by opening the parachute in the air. The parachute is placed in the umbrella cabin when it is in flight. The parachute rope and the body are fixed at three points. When the fixed point outside the cabin is connected by a parachute, the parachute will be exposed on the outer surface of the fuselage, which does not meet the stealth requirements

Method used

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  • A stealth structure of a target drone paracord
  • A stealth structure of a target drone paracord
  • A stealth structure of a target drone paracord

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Embodiment Construction

[0015] 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 hiding structure for drone aircraft parachute lanyards, and belongs to the field of aircraft structure design. The hiding structure for the drone aircraft parachute lanyards comprises a parachute bay, two parachute lanyards, a parachute lanyard, a parachute and a strip-type groove, wherein the fixing points of the two parachute lanyards are formed inside the parachute bay, and the fixing point of the parachute lanyard is formed outside the parachute bay; the strip-type groove is formed in the position, from the parachute bay to the parachute lanyard of which the fixing point is formed outside the parachute bay, of the fixing point; the groove is formed in the surface of an aircraft body. When the parachute falls into the parachute bay, the groove is used for placing the parachute lanyard which is formed outside the parachute bay. According to the hiding structure for the drone aircraft parachute lanyards, exposure of the parachute lanyards on the outer surface of the aircraft body can be effectively avoided, and the hiding effect is improved.

Description

technical field [0001] The invention belongs to the field of aircraft structure design, and in particular relates to a parachute stealth structure for a target aircraft. Background technique [0002] The high-stealth target drone lands by opening the parachute in the air. The parachute is placed in the umbrella cabin when it is in flight. The parachute rope and the body are fixed at three points. When the fixed point outside the cabin is connected by a parachute, the parachute will be exposed on the outer surface of the fuselage, which does not meet the stealth requirements. Contents of the invention [0003] In order to solve the above problems, the present invention proposes a parachute stealth structure for a target drone, which includes an umbrella cabin, two umbrella ropes with fixed points arranged inside the umbrella cabin, a parachute with a fixed point arranged outside the umbrella cabin, and a parachute. It includes a rectifying plate arranged on the back side o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41J9/08B64D17/30
CPCB64D17/30F41J9/08
Inventor 马元春高洪涛卢文书许灯顺孟令赛周斌贺军
Owner 沈阳飞机设计研究所扬州协同创新研究院有限公司