Variant tiltrotor aircraft and working method thereof

A tilt-rotor and variant technology, applied in the field of aviation aircraft, can solve the problems of low power utilization rate, poor flight performance, poor maneuverability, etc., to improve safety and reliability, improve coordination and maneuverability, and improve controllability Effect

Pending Publication Date: 2020-02-11
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the deficiencies of the above-mentioned prior art, the object of the present invention is to provide a variant tiltrotor and its working method, so as to solve the problems of poor flight performance, poor maneuverability and low power utilization rate of the existing tiltrotor.

Method used

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  • Variant tiltrotor aircraft and working method thereof
  • Variant tiltrotor aircraft and working method thereof
  • Variant tiltrotor aircraft and working method thereof

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Embodiment Construction

[0023] In order to facilitate the understanding of those skilled in the art, the present invention will be further described below in conjunction with the embodiments and accompanying drawings, and the contents mentioned in the embodiments are not intended to limit the present invention.

[0024] refer to figure 1 , figure 2 As shown, a variant tiltrotor of the present invention comprises: blade 1, fairing 2, wing 3, transition fuselage 4, high T-shaped tail 5, horizontal tail 6, vertical tail 7, engine short Cabin 8, landing gear 9, and fuselage 10; wherein, propeller blade 1 is fixedly connected on fairing 2, and fairing 2 is fixedly connected on the engine nacelle 8, and engine nacelle 8 is connected with fuselage 10 interior through transmission shaft respectively. The transmission system is connected, and the wing 3 is fixed on the top of the fuselage 10. The tiltrotor adopts a high T-shaped empennage 5 layout, which is fixed on the tail of the fuselage 10. The empennag...

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Abstract

The invention discloses a variant tiltrotor aircraft and a working method thereof. When the tiltrotor aircraft is in a helicopter mode, a propeller blade for providing a lifting force can automatically become longer in diameter, and meanwhile, the span of a wing becomes short, so that the flexibility of the propeller blade is improved to generate a larger lift force, the span of the wing is reduced, and the aerodynamic interference of a rotor wing to the wing is reduced; and when the tiltrotor aircraft is in a fixed-wing mode, a propeller for providing forward thrust can automatically become smaller in diameter, and meanwhile, the span of the wing becomes longer, so that the rigidity of the propeller is increased to produce larger thrust, and the span of the wing is increased to produce alarger lift force. According to the variant tiltrotor aircraft and the working method, the propeller and the wing can be optimized and matched in different flight modes according to the tiltrotor aircraft, the flight performance is remarkably improved, meanwhile, an advanced shape memory alloy material is adopted, no complex mechanical structure is required for variant, and the power of an engineis maximally utilized.

Description

technical field [0001] The invention belongs to the technical field of aviation aircraft, and in particular relates to a variant tilt rotor aircraft and a working method thereof. . Background technique [0002] As one of the greatest inventions, the helicopter has played an irreplaceable role in the economic construction of countries around the world, people's daily life and modern warfare by virtue of its outstanding hovering, low-altitude and low-speed and good maneuverability. As a typical military-civilian dual-use product, helicopters can be widely used in logistics transportation, rescue and ambulance, sightseeing and tourism, emergency rescue and disaster relief, forest protection and fire fighting and other civilian applications. Military applications have been widely used in low-altitude reconnaissance, battlefield search and rescue, equipment transportation, logistics support, electronic Countermeasures, anti-submarine attack and so on. However, conventional sing...

Claims

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Application Information

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IPC IPC(8): B64C3/38B64C7/02B64C27/28B64D29/00
CPCB64C3/38B64C7/02B64C27/28B64D29/00
Inventor 高泽明朱清华王昊陈思婧刘佳
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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