Compressor turbojet engine whose rotor has a movable upstream st

Details Compressor turbojet engine whose rotor has a movable upstream st Compressor turbojet engine whose rotor has a movable upstream st

1994-11-01

1995-12-12

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3931, F02C 106, F02C 720, F02G 300

Patent

active

054738830

ABSTRACT:
Turbojet engine compressor . . . Its rotor (43) includes a movable end portion (45), such as a monoblock vaned disk able to be removed and replaced by a block. High and low pressure shaft lines (54) are formed into several portions to enable these operations to take place without having to dismantle the entire engine.

REFERENCES:
patent: 4744214 (1988-05-01), Monsarrat et al.
patent: 5220784 (1993-06-01), Wilcox
patent: 5224341 (1993-07-01), Munroe et al.
patent: 5307623 (1994-05-01), Antuna et al.

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