Arrangement for connecting a propeller blade ring to a turbine

A ring 22 which carries aircraft propeller blades 15, is connected to a turbine 9 by brackets 101 which extend between the ring and the turbine and are configured and disposed to accommodate thermal expansion of the turbine without significant deformation. The brackets may be V-shaped and are so con...

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Bibliographische Detailangaben
Hauptverfasser:	ROBERT PAUL CZACHOR, SIFARAT SETH HUSAIN, GERARD PAUL KROGER
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A ring 22 which carries aircraft propeller blades 15, is connected to a turbine 9 by brackets 101 which extend between the ring and the turbine and are configured and disposed to accommodate thermal expansion of the turbine without significant deformation. The brackets may be V-shaped and are so connected that during the thermal expansion there is no splaying of the arms of the V as in prior an arrangements.