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Integral sealing structure capable of realizing rapid disassembly of fixed wing and pod

A packaging structure and fixed-wing technology, applied in the field of fixed-wing pods, can solve problems such as troublesome disassembly and assembly, unsightly interior space of the cabin, messy electrical circuits, etc., and achieve the effect of shortening installation time, saving preparation time, and quick disassembly.

Pending Publication Date: 2019-10-01
深圳市科卫泰实业发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The fixed-wing UAV pod faces problems such as disassembly and assembly troubles and messy electrical circuits during use, which increases the preparation time before the flight of the fixed-wing UAV. Short circuit problem between lines

Method used

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  • Integral sealing structure capable of realizing rapid disassembly of fixed wing and pod
  • Integral sealing structure capable of realizing rapid disassembly of fixed wing and pod
  • Integral sealing structure capable of realizing rapid disassembly of fixed wing and pod

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Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] see Figure 1-8 , the present invention provides a technical solution: an integral packaging structure that facilitates the quick disassembly of the fixed-wing pod, including a nacelle 1 and a pod 5, the nacelle 1 includes a nacelle upper cover 2 and a nacelle lower cover 3, and the interior of the nacelle lower cover 3 The engine room battery bottom plate 4 is installed on the rear side, the pod 5 is located at the front end of the engine room lower co...

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Abstract

The invention discloses an integral sealing structure capable of realizing the rapid disassembly of a fixed wing and a pod. The integral sealing structure comprises an engine room and the pod, whereinthe engine room comprises an engine room upper cover and an engine room lower cover, the pod is located at the front end of the engine room lower cover, the pod is fixedly connected with the engine room through an engine room pod bottom plate, a sealing hood enclosing plate is arranged at the upper end of the engine room pod bottom plate, a pod picture transmitting / receiving machine is arranged on a sealing hood cover plate, an engine room end electric joint welding plate is mounted on a sealing hood support base, an engine room end electric joint is arranged on the engine room end electric joint welding plate, fasteners for a pod end electric joint welding plate are fixedly arranged on a sealing hood bottom plate through bolts, the pod end electric joint welding plate is fixedly arrangedon the fasteners for the pod end electric joint welding plate, and a pod end electric joint is arranged on the pod end electric joint welding plate. The structure realizes the rapid disassembly of afixed wing unmanned plane and the pod and the rapid change of the pod and increases the working efficiency.

Description

technical field [0001] The invention belongs to the technical field of fixed-wing pods, and in particular relates to an integral packaging structure that facilitates quick disassembly of the fixed-wing pod. Background technique [0002] The pod refers to a streamlined nacelle section that is installed with certain airborne equipment and hung under the fuselage or wing. It can be fixedly installed (such as an engine pod) or detachable (such as a weapon pod). The addition of pods can make the aircraft have functions that it does not have. The addition of pods usually requires the support of onboard electronic equipment and consideration of the overall aerodynamics of the aircraft. [0003] The fixed-wing UAV pod faces problems such as disassembly and assembly troubles and messy electrical circuits during use, which increases the preparation time before the flight of the fixed-wing UAV. Short circuit problem between lines. In view of this, it is necessary to design an overal...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00
CPCB64D47/00
Inventor 高建琦姜敏丁红亮罗桥伟宋宝路
Owner 深圳市科卫泰实业发展有限公司