IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0384045
(2003-03-06)
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우선권정보 |
HK-02105975 (2002-08-15) |
발명자
/ 주소 |
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대리인 / 주소 |
Blakely Sokoloff Taylor &
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인용정보 |
피인용 횟수 :
3 인용 특허 :
4 |
초록
▼
Provided is a disc-type jet turbine engine with controllable and rotational discharge ports at two sides of a discharge chamber, a fuel tank, and an operation lever connected with the discharge ports. The rotor shaft of the jet turbine engine is connected with a start-up electrical motor through a c
Provided is a disc-type jet turbine engine with controllable and rotational discharge ports at two sides of a discharge chamber, a fuel tank, and an operation lever connected with the discharge ports. The rotor shaft of the jet turbine engine is connected with a start-up electrical motor through a clutch and with a fuel pump through a gearbox. The fuel nozzle of the engine is connected with the fuel tank via the accelerator control valve and the fuel pump. The operation lever controls the clutch. The handle of the operation lever is provided with an electrical switch, a direction controller and an accelerator controller. The switch is electrically connected with the start-up electrical motor, the accelerator controller is connected to control the accelerator control valve, and the direction controller is connected with the discharge ports. Around the combustion chamber is an air-flow guide chamber having an air cooling and heat-insulate layer.
대표청구항
▼
1. A superman air motor, to attach to a human comprising a disc-type jet turbine engine, a plurality of controllable and rotational discharge ports provided at two sides of the discharge chamber for the turbo-jet engine, a fuel tank, and an operation lever connected with the controllable and rotatio
1. A superman air motor, to attach to a human comprising a disc-type jet turbine engine, a plurality of controllable and rotational discharge ports provided at two sides of the discharge chamber for the turbo-jet engine, a fuel tank, and an operation lever connected with the controllable and rotational discharge ports, characterized in that,a rotor shaft of the disc-type jet turbine engine is connected with a start-up electrical motor through a clutch; the rotor shaft is connected with a fuel pump through a gearbox; a plurality of fuel nozzles of the disc-type jet turbine engine are connected with the fuel tank containing fuel through a plurality of fuel pipes via an accelerator control valve and the fuel pump; a handle of the operation lever is provided with an electrical switch, a direction controller and an accelerator controller, the switch is electrically connected with the start-up electrical motor and a power source, the accelerator controller is connected to control the accelerator control valve, the direction controller is connected with the controllable and rotational discharge ports. 2. A superman air motor as set forth in claim 1, characterized in that, the disc-type jet turbine engine is constructed as, the rotor shaft is pivotally provided within a flat and circular housing with one end thereof provided with a turbine and an other end thereof provided with a centrifugal air compressing impeller; and air guide vanes are provided around the centrifugal air compressing impeller, air flow guide chambers and combustion chambers are provided behind said guide vanes;and the air flow guide chambers comprising an air cooling and heat insulation layer provided around the combustion chamber; an air inlet is provided at a location corresponding to a center of the centrifugal air compressing impeller combusted air guide vanes facing the turbine are provided at a discharge outlet, and discharge chambers are provided behind the turbine, discharge pipes are provided on said discharge chambers, the controllable and rotational discharge ports are provided at one end of the discharge pipes. 3. A superman air motor as set forth in claim 1, characterized in that, the operation lever is able to be opened or taken in, so that the space occupied by the superman air motor can be reduced when unused.4. A superman air motor as set forth in claim 1 characterized in that, the discharge pipes are radially provided at two sides of the discharge chambers.5. A superman air motor as set forth in claim 1, characterized in that, the discharge pipes are radially provided at one side of the discharge chambers.6. A superman air motor as set forth in claim 1, characterized in that, a fuel filter is provided between the accelerator control valve and the fuel pump.7. A disc-type jet turbine engine as defined in claim 1, characterized in that, a plurality of the disc-type jet turbine engines can be connected in series so as to provide greater pushing power.
이 특허에 인용된 특허 (4)
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Dmitrowsky Igor (92-36 54th Ave. Elmhurst NY 11373), Aircraft attachable to the body of a pilot.
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Frick Alexander,LIX, Flight device.
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Moore Thomas M. (Huntsville AL), Lockwood airfoil used in conjunction with man transport device.
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Michael Moshier, Single passenger aircraft.
이 특허를 인용한 특허 (3)
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Zapata, Frankie, Device and system for propelling a passenger.
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Zapata, Frankie, Device and system for propelling a passenger.
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Duru, Catalin Alexandru, Personal flight vehicle.
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