Engine starting system for rotorcraft in flight

A rotorcraft engine starting system includes a starting system controller 13 in communication with a flight control computer; an electric engine starter 9; an electronic engine controller 2 in communication with the electric engine starter; an electrical power distributor 8; and a plurality of power...

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Bibliographische Detailangaben
Hauptverfasser:	SMILEY, ALFRED RUSSEL, STRAUSS, MICHAEL PETER, CYCON, JAMES PETER
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES 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 INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDEDFOR STARTING OF COMBUSTION ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A rotorcraft engine starting system includes a starting system controller 13 in communication with a flight control computer; an electric engine starter 9; an electronic engine controller 2 in communication with the electric engine starter; an electrical power distributor 8; and a plurality of power sources coupled to the electrical power distributor; the starting system controller selecting at least one of the plurality of power sources and instructing the electrical power distributor to use the at least one of the plurality of power sources to power the electric engine starter.