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Oil-electricity hybrid vertical take-off and landing fixed wing aircraft

A vertical take-off and landing, fixed-wing technology, applied in the direction of vertical take-off and landing aircraft, rotorcraft, aircraft, etc., can solve the problems of low flight efficiency and inability to realize tilting, and achieve high flight efficiency, long cruising distance, and broad application prospects Effect

Inactive Publication Date: 2019-08-23
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] This type of aircraft has the capabilities of vertical take-off and landing, hovering, low-altitude flight, high-speed cruising, and long range. It plays a specific role in emergency rescue and disaster relief and has broad application prospects. However, the existing vertical take-off and landing fixed-wing aircraft are mainly electric, which cannot reach long-term endurance. lower

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  • Oil-electricity hybrid vertical take-off and landing fixed wing aircraft

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Embodiment Construction

[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0024] Such as figure 1 As shown, the present invention discloses an oil-electric hybrid vertical take-off and landing fixed-wing aircraft, including a fuselage 8, wings 6, landing gear (not shown in the figure), a tilting mechanism, an empennage 10, an engine 7, and a drive motor 3 , the engine 7 is installed on the front end of the fuselage 8 as the main power for level flight cruise; The tail of body 8. The tilting mechanism comprises a left tilting part 4, a right tilting part 5, a left tilting motor 2 and a right tilting motor 1, and the left tilting part 4 and the right tilting part 5 make the left tilting motor 2 and the right tilting motor 1 mounted on it in a vertical position. Straight up or horizontal state; the drive motor 3 is used to provide power during vertical take-off and landing together with the left tilting moto...

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Abstract

The invention discloses an oil-electricity hybrid vertical take-off and landing fixed wing aircraft. The oil-electricity hybrid vertical take-off and landing fixed wing aircraft comprises an aircraftbody, wings and an engine, wherein the engine is arranged at the front end of the aircraft body and serves as the active force for cruising cruise, and the wings are arranged at the middle section ofthe aircraft body; and the fixed wing aircraft further comprises a tilting mechanism which is arranged at the front middle section of the aircraft body and a driving motor, wherein the tilting mechanism comprises a left-leaning rotating part, a right-leaning rotating part, a left-leaning rotating motor and a right-leaning rotating motor, the left-leaning rotating part and the right-leaning rotating part are enabled the left-leaning rotating motor and the right-leaning rotating motor which are arranged on the left-leaning rotating part and the right-leaning rotating part respectively to be a vertical upward or horizontal state, the right-leaning rotating motor is in a vertical upward or horizontal state, the driving motor is used for providing power together with the left-leaning rotating motor and the right-leaning rotating motor which are in the vertical upward state during vertical take-off and landing. The oil-electricity hybrid vertical take-off and landing fixed wing aircraft hasthe advantages of being long in navigation time, long in cruising distance, high in flight efficiency and the like.

Description

technical field [0001] The invention mainly relates to the field of flight equipment, in particular to an oil-electric hybrid vertical take-off and landing fixed-wing aircraft. Background technique [0002] A vertical take-off and landing fixed-wing aircraft is a unique aircraft that can hover, take off and land vertically like a traditional multi-rotor aircraft, and can also cruise at high speed like a propeller fixed-wing aircraft. [0003] This type of aircraft has the capabilities of vertical take-off and landing, hovering, low-altitude flight, high-speed cruising, and long range. It plays a specific role in emergency rescue and disaster relief and has broad application prospects. However, the existing vertical take-off and landing fixed-wing aircraft are mainly electric, which cannot reach long-term endurance. lower. Contents of the invention [0004] The technical problem to be solved by the present invention is: aiming at the technical problems existing in the pri...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/28B64C29/00B64D27/02
CPCB64C27/28B64C29/0008B64D27/02B64U2101/00B64D27/026
Inventor 赵述龙喻煌超贺光贾圣德肖乃经王欢余立
Owner NAT UNIV OF DEFENSE TECH
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