Fixed-wing aircraft realizing vertical take-off and landing

A vertical take-off and landing, fixed-wing technology, applied in the field of aircraft, can solve problems such as reducing aircraft performance, pressure differential resistance loss, increasing costs, etc., to reduce manufacturing costs, reduce difficulty and improve reliability.

Inactive Publication Date: 2015-11-25
HUNAN AIRTOPS INTELLIGENT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, since the V-22 Osprey uses two helicopter rotors, in the vertical take-off and landing mode, the rotors need an automatic tilter to control the stability of the attitude of the aircraft, which increases the difficulty of control, and the blades use a cyclic pitch change device, which also increases In addition,

Method used

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  • Fixed-wing aircraft realizing vertical take-off and landing
  • Fixed-wing aircraft realizing vertical take-off and landing
  • Fixed-wing aircraft realizing vertical take-off and landing

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Embodiment 1

[0027] For the vertical take-off and landing fixed-wing aircraft described in this embodiment, see Figure 1-3 , it comprises fuselage 1, empennage 8 and 2 power units with tilting mechanism, described power unit with tilting mechanism comprises fixed-pitch propeller 4, engine (not shown in the figure), slipstream rudder 12. Wing, tilting wing 2, engine compartment 3 and steering gear (not shown in the figure), the engine is installed in the engine compartment 3, the fixed-pitch propeller 4 is connected to the output shaft of the engine, and one end of the tilting wing 2 is fixed Connected to the engine compartment 3, the other end is rotatably connected to the wing, the slipstream rudder 12 is movably connected to the tilting wing 2, the steering gear drives the slipstream rudder 12, and the power with the tilting mechanism The device is symmetrically arranged on both sides of the fuselage 1, and is connected to the fuselage 1 through a connecting part, and is arranged horizo...

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Abstract

The invention provides a fixed-wing aircraft realizing vertical take-off and landing. The fixed-wing aircraft comprises an aircraft body, a tail and power devices provided with tilting mechanisms, wherein each power device provided with the tilting mechanism comprises a fixed-pitch propeller, an engine, an engine cabin, a slipstream rudder, a wing, a tilting wing and a steering engine, the engine is mounted in the engine cabin, the fixed-pitch propeller is connected with an output shaft of the engine, one end of the tilting wing is fixedly connected onto the engine cabin, the other end is rotationally mounted onto the wing, the slipstream rudder is movably connected onto the tilting wing, and the steering engine drives the slipstream rudder; the power devices provided with the tilting mechanisms are symmetrically arranged on two sides of the aircraft body, the wings are horizontally arranged, a through hole is formed in the head of the aircraft body, and a ducted fan is arranged in the through hole. The size of the aircraft rotor wings and the aircraft is smaller, a complex automatic tilting device and a periodic pitch-variable device are omitted, the structure is simple, the trim difficulty and flight control system complexity are reduced, the system reliability is high, and the cost is low.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a vertical take-off and landing fixed-wing aircraft. Background technique [0002] Since the 21st century, more and more aircraft developers have turned their attention to fixed-wing aircraft that take off and land vertically. This type of aircraft has similar functions to helicopters and can take off and land vertically without using a runway. The difference is that this This type of aircraft can accelerate from a hovering state to level flight through power tilt and transition to a fixed-wing flight mode. [0003] At present, practical vertical take-off and landing fixed-wing aircraft are mainly AV-8 Harrier fighter jet, V-22 Osprey tilt-rotor aircraft, and F-35 fighter jet. The AV-8 Harrier fighter uses a Pegasus engine, and on the basis of a jet engine, it adopts a thrust reversing scheme with a rotatable exhaust nozzle. In actual use, this type of aircraft often has reliability prob...

Claims

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Application Information

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IPC IPC(8): B64C27/26B64C27/28
Inventor 罗世彬刘轩岑吴雷
Owner HUNAN AIRTOPS INTELLIGENT TECH CO LTD
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