Compound type aircraft

A kind of aircraft and composite technology, applied in the field of aircraft, can solve the problems of low safety and stability, low efficiency, difficult take-off and landing, etc.

Active Publication Date: 2016-01-06
江苏雨能水利工程有限公司
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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, cannot take off and land vertically, and are not convenient for ultra-low speed or hovering f

Method used

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  • Compound type aircraft
  • Compound type aircraft
  • Compound type aircraft

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Embodiment Construction

[0011] Now in conjunction with accompanying drawing, the present invention is described in detail: a kind of composite aircraft, comprises fuselage 1, left composite wing 2, right composite wing 3, composite empennage and landing gear 7. 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. Composite empennage is positioned at the afterbody of fuselage 1, and composite empennage comprises vertical empennage 4, left electric propeller 5 and right electric propeller 6. The left electric propeller 5 and the right electric propeller 6 have the same structure, they turn to the opposite direction, and are symmetrically arranged on the left and right sides of the vertical empennage 4 horizontally. Left electric propeller 5 comprises propeller and motor, and motor is powered by lithium battery. Vertical...

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PUM

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Abstract

The invention relates to a compound type aircraft, which belongs to the technical field of aircrafts and comprises an airframe, a left composite wing, a right composite wing, a composite empennage and an undercarriage. A control system and an airborne device are arranged in the airframe. The composite empennage is located at the tail part of the airframe, and comprises a vertical empennage, a left power-driven propeller and a right power-driven propeller. The left power-driven propeller and the right power-driven propeller have the same structure and opposite rotation directions, and are symmetrically arranged on the left side and the right side of the vertical empennage. The undercarriage adopts a wheel type structure or a jumper and wheel type composite structure. The left composite wing and the right composite wing have the same structure and are symmetrically arranged on the left side and the right side of the airframe. The left composite wing is provided with two or three rotor wings internally, and each rotor wing is driven by an engine. Vanes of the left composite wing comprises front fixed vanes and rear vanes capable of deflecting around a wing axis. The rotor wings are all located under the wing axis. The compound type aircraft can be lifted vertically by only a small take-off and land zone. The compound type aircraft generates larger lifting force, and is safe, stable and flexible.

Description

technical field [0001] A composite aircraft belongs to the technical field of aircraft, and in particular relates to a composite aircraft. Background technique [0002] Traditional aircraft take-off and landing require a long runway, cannot take off and land vertically, and are not convenient for ultra-low speed or hovering 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 invention is to overcome the above-mentioned shortcomings of traditional airplanes and helicopters, and to invent a highly efficient, safe and stable composite aircraft that is convenient for short-distance take-off and landing and even vertical take-off and landing. [0004] A composite aircraft includes a fuselage, a left composite wing, a right composite wing, a composite empennage and landing gear. The fuselage is equipped...

Claims

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Application Information

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IPC IPC(8): B64C27/26B64C29/02
Inventor 王志成
Owner 江苏雨能水利工程有限公司
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