B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
60/85
B64C 11/00 (2006.01) B64C 11/02 (2006.01) F01D 5/02 (2006.01) F01D 25/16 (2006.01)
Patent
CA 1331697
FLEXIBLE CONNECTOR FOR USE IN AIRCRAFT ABSTRACT OF THE DISCLOSURE The invention concerns a connector, in an aircraft engine, for mounting a ring to a turbine rotor which the ring surrounds. The ring carries propeller blades, and the connector transmits both thrust and torque loads between the ring and the rotor, without significant deformation. However, the connector does deform in order to accommodate differential thermal growth between the ring and the rotor.
609294
Hauser Ambrose Andreas
Wakeman Thomas George
Company General Electric
Craig Wilson And Company
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