Gas turbine engine

Details Gas turbine engine Gas turbine engine

1983-09-12

1992-04-28

Bentley, Stephen C.

Power plants

Reaction motor

Interrelated reaction motors

60232, 23926535, F02K 306

Patent

active

051076756

ABSTRACT:
A gas turbine engine of the type comprising a first compressor 4, a second compressor 6, a combustor 8 and turbines 10 for driving the compressors 4 and 6 is provided with an air intake 16, leading to the second compressor 6. The flow from the first compressor 4 is discharged through vectorable nozzles 12,14. The nozzles 12,14 are movable between a first position where they discharge to ambient and a second position where they register with the intake 16 and the flow from the first compressor 4 discharges to the second compressor 6.

REFERENCES:
patent: 2968452 (1961-01-01), Cook
patent: 3913321 (1975-10-01), Snell
patent: 4038818 (1977-08-01), Snell
patent: 4474345 (1984-10-01), Musgrove

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