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Expandable combined aircraft

A technology for aircraft and fuselage, applied in the field of aircraft, can solve the problems of increased storage and maintenance costs, long development cycle and high cost

Pending Publication Date: 2018-02-23
珠海天晴航空航天科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This single load needs to correspond to the design method of a single model, which not only has a long development cycle and high cost, but also causes continuous increase in storage and maintenance costs in the later period

Method used

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Embodiment Construction

[0014] The idea, specific structure and technical effects of the present invention will be clearly and completely described below in conjunction with the embodiments and accompanying drawings, so as to fully understand the purpose, features and effects of the present invention. Apparently, the described embodiments are only some of the embodiments of the present invention, rather than all of them. Based on the embodiments of the present invention, other embodiments obtained by those skilled in the art without creative efforts belong to The protection scope of the present invention.

[0015] refer to Figure 1 to Figure 2 , an expandable and combined aircraft, comprising at least two side-by-side fuselages 1, the two adjacent fuselages 1 are connected by connecting wings 2, and outer wings 3 are arranged on the outside of the fuselage 1 at the side end . This embodiment includes two side-by-side fuselages 1, the two fuselages 1 are connected by connecting wings 2, the outer s...

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Abstract

The invention discloses an expandable combined aircraft. The expandable combined aircraft comprises at least two parallel fuselages, the two adjacent fuselages are connected through a connecting wing,an outer wing is arranged at the outer side of the portion, located at the side end, of each fuselage, and the fuselages and the connecting wing and / or the fuselages and the outer wings are fixed through fixing devices. The parallel fuselages are connected through the connecting wing and the fixing devices to achieve modularization design of the aircraft, the aircraft capable of being formed by combining multiple single unmanned aerial vehicles is obtained, different load task requirements can be met by increasing the length of the connecting wing or the number of the fuselages and connectingwings, and therefore a freight house, an investigatin device, radar weapon, a guided missile rocket and other devices can be hung below the aircraft.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an expandable and combined aircraft. Background technique [0002] At present, in the research and development of UAVs, according to the requirements of different load tasks, it is generally necessary to design models with different load capabilities to achieve them, and each model needs to complete the corresponding research and development process. This single load needs to correspond to the design method of a single model, which not only has a long development cycle and high cost, but also causes continuous increase in storage and maintenance costs in the later period. Contents of the invention [0003] In view of the above problems, the present invention provides an expandable and combined aircraft, which has a modular design of multiple connectable fuselages, so that multiple single drone fuselages can be combined with each other. [0004] The technical scheme that the p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C37/02
CPCB64C37/02
Inventor 贺军房佳琦曲长征霍俭娃岳静雯王志刚孙英鑫杨鹏
Owner 珠海天晴航空航天科技有限公司