Control mechanism for swivel tail of an aircraft

1,136,338. Convertiplane propeller control. UNITED AIRCRAFT CORP. 16 June, 1967 [8 July, 1966], No. 27866/67. Headings B7G and B7W. [Also in Division F2] A convertiplane having a variable pitch tail rotor 24, swivellable about a vertical axis 18 between an anti-torque helicopter position, shown, and...

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Bibliographische Detailangaben

1. Verfasser:	JR. JOHN A. KEDER
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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