Exit stator mounting

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

Reexamination Certificate

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Details

C415S215100, C415S227000

Reexamination Certificate

active

06881032

ABSTRACT:
A gas turbine engine has an intermediate case. At least one compressor exit stator shroud is welded to the intermediate case.

REFERENCES:
patent: 5249921 (1993-10-01), Stueber et al.

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