Bypass conduit for gas turbine engine

Details Bypass conduit for gas turbine engine Bypass conduit for gas turbine engine

1989-06-23

1991-04-02

Stout, Donald E.

Power plants

Reaction motor

Air passage bypasses combustion chamber

60 3975, 60 3983, 415116, F02C 712

Patent

active

050037730

ABSTRACT:
A gas turbine engine (10) is provided with a bypass conduit (56) for venting air (52) leaking past a rotating compressor seal (46). The leakage air (58) is returned to the working fluid flow path (64) upstream of this first turbine stage (32).

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