HYDROMECHANICAL OVERSPEEDING PROTECTIVE SYSTEM AND METHOD TO PROTECT AIRCRAFT ENGINE FROM OVERSPEEDING Russian patent published in 2006 - IPC F01D21/02 

Abstract RU 2278275 C2

FIELD: aircraft industry.

SUBSTANCE: turbomachine, whose speed is controlled by electronic control circuit by means of throttle control lever, is furnished with device to prevent overspeeding which contains means to limits delivery of fuel in turbomachine to preset rate Wps when speed exceeds maximum tolerable speed of revolution, means to maintain said fuel delivery at preset fuel rate when revolution speed drops below said maximum tolerable revolution speed, and means to bring fuel delivery to rate Wr corresponding to idling rate, said throttle control lever is set to idling position.

EFFECT: provision of overspeed protection.

9 cl, 8 dwg

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RU 2 278 275 C2

Authors

Mehjar David

Garassino Alen P'Er

Mehjar Klod Marsel'

Dessen Karolin

Vedzhotti Izabel'

Dates

2006-06-20Published

2001-12-20Filed