Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...
Patent
1980-08-22
1983-05-17
Love, John J.
Fluid sprinkling, spraying, and diffusing
Reaction motor discharge nozzle
With means controlling amount, shape or direction of...
60430, 60465, 244110B, F02K 115
Patent
active
043836470
ABSTRACT:
The invention is an integrated hydraulic control circuit for actuating the thrust reversers and variable exhaust nozzle on high performance gas turbine engine powered aircraft. The hydraulic circuits for both systems are integrated into a single housing and are served by common elements. The circuit for the deployment and stowage of the thrust reverser buckets is hydraulically sequenced inhibiting the application of hydraulic power to the actuators prior to withdrawal of the locking pin. In a like manner, the thrust reversers must be fully retracted before the locking pin is deployed. The hydraulic circuit for the thrust reversers also includes a pressure compensating circuit which reduces the pressure applied to thrust reverser actuators with the thrust reversers in the stowed position.
REFERENCES:
patent: 3015936 (1962-01-01), Brewer et al.
patent: 3263623 (1966-08-01), Alexanderson et al.
patent: 3367109 (1968-02-01), Troeger et al.
patent: 3456881 (1969-07-01), Beitler et al.
patent: 3604662 (1971-09-01), Nelson, Jr. et al.
patent: 4210066 (1980-07-01), Aldrich
patent: 4212442 (1980-07-01), Fage
Ferguson, Jr. John H.
Hoffman John R.
Woodruff Frank
Cuoco Anthony F.
Forman Michael J.
Ignatowski James R.
Love John J.
The Bendix Corporation
LandOfFree
Integrated hydraulic control circuit for jet engine thrust rever does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Integrated hydraulic control circuit for jet engine thrust rever, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Integrated hydraulic control circuit for jet engine thrust rever will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1563670