Device for controlling the opening and closing of discharge valv

Power plants – Reaction motor – Interrelated reaction motors

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Details

60 39092, 60 3929, F02C 918

Patent

active

055156738

ABSTRACT:
A control device makes it possible to rapidly shift the bleed valves of an aircraft turbojet engine to a large opening position when the engine is under low power operation in order to prevent flame-out. The device allows for instantaneously interrupting the action of a control return cable when the valves are open from a certain given value. The device includes a drive support integral with a crank handle, in order to bring about the translation of the return cable, when the latter is not blocked by a translation stop member. The control device is used for opening of bleed valves of turbojet engines having two concentric annular jets.

REFERENCES:
patent: 4463552 (1984-08-01), Monhardt et al.
patent: 4702070 (1987-10-01), Cureton et al.
patent: 4815285 (1989-03-01), Martin
patent: 5044153 (1991-09-01), Mouton
patent: 5123240 (1992-06-01), Frost et al.

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