HIGH SPEED ENGINE REDUCTION GEARBOXES

An engine reduction gear system includes at least two self-contained, independent engine reduction gearboxes (202a, 202b), each capable of connecting to an aircraft engine. Each of the engine reduction gearboxes (202a, 202b) provides redundant, reduced speed to a main rotor gearbox (208) via a shaft...

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Hauptverfasser:	Poster, Scott David, Riley, Walter, Speller Jr., Charles Hubert, Cope, Gary
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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creator	Poster, Scott David Riley, Walter Speller Jr., Charles Hubert Cope, Gary
description	An engine reduction gear system includes at least two self-contained, independent engine reduction gearboxes (202a, 202b), each capable of connecting to an aircraft engine. Each of the engine reduction gearboxes (202a, 202b) provides redundant, reduced speed to a main rotor gearbox (208) via a shaft (206a, 206b).
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language	eng ; fre ; ger
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subjects	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
title	HIGH SPEED ENGINE REDUCTION GEARBOXES
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