Aero-engine starting fuel oil flow control method

The invention relates to the technical field of aero-engine starting control, and provides an aero-engine starting fuel flow control method in order to conveniently control starting fuel flow. Comprising the steps that 1, the oil supply amount and the actual rotating speed of a gas compressor corres...

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Bibliographische Detailangaben
Hauptverfasser:	HU HUIFANG, CHENG CHUN, ZHAO KE, CHEN MINGAN, LI YANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CALCULATING COMBUSTION ENGINES COMPUTING CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COUNTING ELECTRIC DIGITAL DATA PROCESSING GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MEASURING MECHANICAL ENGINEERING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS
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