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Gas-electric hybrid system and vertical take-off and landing flying vehicle with same

A fuel-electric hybrid and aircraft technology, which is applied in the field of vertical take-off and landing flying cars and gasoline-electric hybrid systems, can solve the problems of large propeller noise, poor safety, and insufficient battery power, and achieve high safety, simple structure, and low noise. small effect

Active Publication Date: 2018-02-16
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

[0011] The invention provides an oil-electric hybrid power system and a vertical take-off and landing flying car with it, to solve the problem of insufficient battery power due to the large lift force required for vertical take-off / landing and relying on pure electric power, and to avoid the use of turboshaft engines to drive propellers with large noise and Technical issues such as poor security

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  • Gas-electric hybrid system and vertical take-off and landing flying vehicle with same
  • Gas-electric hybrid system and vertical take-off and landing flying vehicle with same

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Embodiment Construction

[0046] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0047] Aiming at the power requirements of the vertical take-off and landing flying vehicle, the present invention proposes an oil-electric hybrid power system solution. When driving on the road, it uses battery power and the motor drives the wheels, which is a complete electric vehicle; when flying, the motor is switched to drive the air compressor to compress the small flow of air, and the gas generated by the compressed air and gasoline combustion is used to drive the turbofan and generators, which provide vertical take-off and flight power for the car, and recharge the batteries during cruising flight.

[0048] refer to figure 1 , in a preferred embodiment of the present invention, this e...

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Abstract

The present invention discloses a gas-electric hybrid system and a vertical take-off and landing flying vehicle with the same. The gas-electric hybrid system comprises an air inlet provided on the windward surface and a pressurization system which communicates with the air inlet and is used for pressurizing air entered through the air inlet. The pressurization system comprises a compressor. The inlet of the compressor communicates with the outlet of the air inlet. The outlet of the compressor communicates with the air inlet of a gas generator. The gas generator is provided with a fuel inlet and a plurality of gas outlets. The plurality of gas outlets communicate with a plurality of turbofan thrusters through gas pipelines. The plurality of turbofan thrusters are used for providing liftingforce for take-off and landing of the aircraft and / or adjusting the flying attitude of the aircraft. The gas-electric hybrid system further comprise a motor for providing driving force and a battery module for supplying power for the motor. The motor is connected with the compressor and / or a ground traveling mechanism through a switching device so as to realize the switching control between driving the ground traveling mechanism and driving the compressor.

Description

technical field [0001] The present invention relates to the field of automobile engines, in particular, to an oil-electric hybrid power system. In addition, the present invention also relates to a vertical take-off and landing flying vehicle comprising the above-mentioned fuel-electric hybrid power system. Background technique [0002] Automobiles are the most important means of transportation for people to go out at present, but commonly used cars can only run on roads built. When encountering road obstacles or having no way to go, drivers are often at a loss what to do. Flying cars can not only drive on the road, but also fly in the air. It is a powerful tool to solve road obstacles, traffic in remote areas and three-dimensional traffic problems in future cities, and has broad development prospects. [0003] In 1917, Glenn Curtiss of the United States invented the first flying car, AutoPlane. A double-layer wing with a wingspan of 12.3 meters was added to the top of the o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B60F5/02B60K6/00B64C29/00B64D27/02
CPCB64C29/0033B64D27/02B60F5/02B60K6/00B64D27/026
Inventor 刘卫东刘世杰
Owner NAT UNIV OF DEFENSE TECH
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