Antriebsvorrichtung für Hydraulikpumpe und Luftkompressor

A dual drive system (5) for a hydraulic pump (30) and an air boost compressor (40) is provided. Reversible power (10) is transmitted to a shaft (12) connected to clockwise (20) and counterclockwise (22) overrunning clutches connected to different vehicle or equipment subsystems (30,40). Reversing th...

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Bibliographische Detailangaben
Hauptverfasser:	PROVOST, MICHAEL JOHN, CARTER III, HOWARD, JOHNSON, RICHARD N, BROWN, JOHN DAVID
Format:	Patent
Sprache:	ger
Schlagworte:	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 HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS PARACHUTES PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A dual drive system (5) for a hydraulic pump (30) and an air boost compressor (40) is provided. Reversible power (10) is transmitted to a shaft (12) connected to clockwise (20) and counterclockwise (22) overrunning clutches connected to different vehicle or equipment subsystems (30,40). Reversing the drive (10) allows power to be alternately transmitted to one or the other of the subsystems. The invention includes utilizing the dual drive for hydraulic (30) and air conditioning systems (40) for an aircraft, with the provision of an additional drive motor (60) providing constant power to one or more of the subsystems.