An engine arrangement

In a contra rotating propeller engine propeller blade assemblies 21, 22 are provided which rotate in opposite directions as a result of association with an epicyclic gear assembly 25 acting as a differential gearbox. A carrier 29 is provided to drive one propeller blade assembly 21. Actuators 36, 37...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	BEAVEN, DAVID MICHAEL
Format:	Patent
Sprache:	eng ; fre ; ger
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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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