TURBOPROP POWER PLANT CONTROL METHOD

FIELD: automatic control of aircraft. SUBSTANCE: axial air velocity downstream of propeller 2 is measured by transducer 8 made, for example, in the form of pitot tube. For metering fuel flow, engine control lever is shifted to vary setting of turbocompressor fuel flow controller 4 that changes flow...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Gorelov G.M, Mikhajlov S.V, Kamotskij Eh.T
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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