A kind of composite aircraft with empennage

An aircraft and composite technology, applied in the field of aircraft, can solve the problems of inconvenient ultra-low speed flight, low safety and stability, and low efficiency.

Active Publication Date: 2017-12-01
BEIJING INST OF REMOTE SENSING EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional aircraft take-off and landing require a long runway, and it is not convenient for ultra-low-speed flight, and it is also difficult to take off and land in a short distance
Traditional helicopters have high energy consumption, low efficiency, low safety and stability

Method used

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  • A kind of composite aircraft with empennage
  • A kind of composite aircraft with empennage
  • A kind of composite aircraft with empennage

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Embodiment Construction

[0009] Now in conjunction with accompanying drawing the present invention is described in detail: a kind of composite aircraft with empennage, comprises fuselage 1, left composite wing 2, right composite wing 3, empennage 4 and landing gear 5. The fuselage 1 is equipped with a control system and airborne equipment. The left compound wing 2 and the right compound wing 3 have the same structure, and they are symmetrically installed on the left and right sides of the fuselage 1. The empennage 4 is located at the tail of the fuselage 1 , and the empennage 4 includes a horizontal empennage 41 and a vertical empennage 42 . The horizontal empennage 41 comprises a front section fixed part and a rear section movable part, and the rear section of the vertical empennage 42 can deflect left and right. The horizontal stabilizer 41 functions as a horizontal stabilizer and an elevator, and the vertical stabilizer 42 functions as a vertical stabilizer and a rudder. Landing gear 5 adopts whe...

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Abstract

A composite aircraft with empennage belongs to the technical field of aircraft and includes a fuselage, a left composite wing, a right composite wing, an empennage and a landing gear. The fuselage is equipped with a control system and airborne equipment. Empennage is positioned at the afterbody of fuselage, and empennage comprises horizontal empennage and vertical empennage. The landing gear adopts wheel structure. The left composite wing and the right composite wing have the same structure, and they are symmetrically installed on the left and right sides of the fuselage. Inside the left compound wing are two rotors, each powered by an engine. The flaps of the left compound wing consist of a fixed front flap and a rear flap that is deflectable around the wing axis. All rotors are located below the wing shaft. The composite aircraft with empennage has a small take-off and landing site and can vertically ascend and descend. The generated lift is large, safe, stable and flexible.

Description

technical field [0001] The invention relates to a composite aircraft with an empennage, belonging to the technical field of aircraft, in particular to a composite aircraft with an empennage. Background technique [0002] Traditional aircraft take-off and landing require a long runway, and it is not convenient for ultra-low-speed flight, and it is also difficult to take off and land in a short distance. Traditional helicopters have high energy consumption, low efficiency, and low safety and stability. Contents of the invention [0003] The purpose of the present invention is to overcome the above-mentioned deficiency of traditional airplane and helicopter, invent a kind of efficient safe and stable composite aircraft with empennage that is convenient for short-distance take-off and landing. [0004] The utility model relates to a composite aircraft with an empennage, comprising a fuselage, a left composite wing, a right composite wing, an empennage and a landing gear. The...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/26B64C9/14
Inventor 王志成
Owner BEIJING INST OF REMOTE SENSING EQUIP
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