Helicopter jet rotor power system

The utility model discloses a helicopter jet rotor power system which comprises an internal combustion engine, a charging turbine, a centrifugal compressor and a wingtip jet rotor, high-temperature and high-speed fuel gas of the internal combustion engine is introduced into the centrifugal compresso...

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Bibliographische Detailangaben
Hauptverfasser:	JIANG ANCHANG, FENG ZHUOFAN, CHENG TING, WU JINWU, LU SHUJUN, WANG YUN, YANG BEI, FENG YU
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The utility model discloses a helicopter jet rotor power system which comprises an internal combustion engine, a charging turbine, a centrifugal compressor and a wingtip jet rotor, high-temperature and high-speed fuel gas of the internal combustion engine is introduced into the centrifugal compressor through the charging turbine, and a gas outlet of the centrifugal compressor is communicated with an inlet end of a first electromagnetic reversing valve. Two outlet ends of the first electromagnetic directional valve are respectively communicated with the internal combustion engine and the wingtip jet rotor, an air outlet of the charging turbine is communicated with an inlet end of the second electromagnetic directional valve, and two outlet ends of the second electromagnetic directional valve are respectively communicated with the exhaust port and the wingtip jet rotor. According to the helicopter jet rotor power system adopting the structure, gas generated by turbocharging is utilized to jet and drive the wing