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A long range vibrating wing aircraft

An aircraft and vibrating wing technology, which is applied in the field of aircraft, can solve the problems affecting the safety of aircraft take-off and landing, the limitation of take-off and landing sites, and the high price, and achieve the effects of simple structure, improved efficiency and energy saving.

Active Publication Date: 2019-04-12
HARBIN ENG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, fixed-wing aircraft has the following disadvantages: expensive
Both the fixed-wing aircraft itself and the fuel consumed by the fixed-wing aircraft are much more expensive than other modes of transportation; it is greatly affected by weather conditions
Severe wind, rain, snow, fog and other meteorological conditions will still affect the safety of aircraft take-off and landing; there are restrictions on the take-off and landing sites

Method used

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  • A long range vibrating wing aircraft
  • A long range vibrating wing aircraft
  • A long range vibrating wing aircraft

Examples

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Embodiment Construction

[0023] The present invention is described in more detail below in conjunction with accompanying drawing:

[0024] Such as figure 2 As shown, the motor 9 is installed on the bracket inside the aircraft fuselage 1, the output shafts on both sides of the motor 9 are connected to the crank 10, and the crank 10 is connected to one end of the connecting rod 8, and the other end of the connecting rod 8 is fixedly connected to the wing shaft 7, and the wing The shaft 7 traverses through the slideway 3 and connects with the aircraft fuselage 1 and the main vibrating wing 2. There is an opening at the corresponding position of the aircraft fuselage 1; when the motor 9 is running, it drives the crank linkage mechanism, and then drives the main vibrating wing 2 along the slideway. 3 Do vertical reciprocating motion and rotational motion.

[0025] When the main vibrating wing 2 moves to the highest point or the lowest point, the chord direction of the main vibrating wing 2 forms an attac...

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Abstract

The invention discloses a long-voyage oscillating-wing aircraft which comprises an aircraft body 1, main oscillating wings 2, a support 5, a motor 9, a crank connecting rod mechanism, a slide rail 3,an empennage 4 and a control system. The main oscillating wings 2 are arranged at the front of the middle of the aircraft body 1, and the main oscillating wings 2 on the left side and the right side of the aircraft body are connected with each other by wing axles 7 which transversely penetrate the aircraft body 1. Two ends of each connecting rod 8 are fixedly connected with a corresponding crank 10 and the corresponding wing axle 7. The main oscillating wings 2 can be driven by the connecting rods 8 to carry out vertical reciprocating movement and rotation movement along the slide rail 3. Theslide rail 3 is arranged on a support inside the aircraft body 1. Lifting force can be generated under the movement of the main oscillating wings 2, so that the weight of the long-voyage oscillating-wing aircraft can be balanced, and the long-voyage oscillating-wing aircraft can be pushed to advance by generated horizontal thrust. The long-voyage oscillating-wing aircraft has the advantages that merits of fixed-wing aircrafts and merits of the oscillating wings are combined with one another, movement postures of the main oscillating wings 2 are controlled, accordingly, gliding and accelerationmovement and the like can be implemented, and takeoff and landing actions and the like can be implemented under the matching effects of the main oscillating wings and the empennage 4; integral movement mechanisms are high in efficiency and low in noise, and the long-voyage oscillating-wing aircraft can fly over long distances in wide ranges.

Description

technical field [0001] The invention belongs to the technical field of aircraft, in particular to a long-range vibrating-wing aircraft. Background technique [0002] Vibrating or flapping wing flight is an imitation of the flight of birds in nature. Birds have superb flying skills. People have been exploring the mysteries of flight, imitating the flight of birds, and inventing airplanes and various aircraft for military and civilian use. However, fixed-wing aircraft need to install additional thrusters to fly, and the noise is very loud. The aircraft based on the principle of bionic dynamics can meet the requirements of low noise and high efficiency. The current bird-like flapping wing aircraft has a complex structure, low structural reliability and low efficiency, and it is difficult to meet the needs of the long-range aircraft. [0003] The patent publication number is CN105204370A. The fixed-wing aircraft real-time simulation system and simulation method simulate the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C33/02
Inventor 许国冬麻彩朋庞顺翔
Owner HARBIN ENG UNIV