Ducted fan gas turbine engine accessory drive

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60 39161, F02C 732, F02K 304

Patent

active

056875614

ABSTRACT:
A ducted fan gas turbine engine includes a fan which is driven by a low pressure turbine via a load transmitting shaft. The load transmitting shaft additionally drives the accessories of the engine and the aircraft upon which it is mounted. In the event of an engine failure, the power produced by the windmilling of the engine fan is sufficient to provide continuity of drive to the accessories.

REFERENCES:
patent: 3348379 (1967-10-01), Wilde
patent: 3792586 (1974-02-01), Kasmarik
patent: 4068470 (1978-01-01), Sargisson et al.

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