Hollow cooled blade or vane for a gas turbine engine

Details Hollow cooled blade or vane for a gas turbine engine Hollow cooled blade or vane for a gas turbine engine

1974-10-02

1979-01-23

Feinberg, Samuel

Fluid reaction surfaces (i.e., impellers)

With fluid passage in working member communicating with...

Air and watercraft propellers

415115, F01D 518

Patent

active

041358554

ABSTRACT:
A hollow cooled blade or vane for a gas turbine engine is provided with cooling on certain areas of its interior surface by an impingement plate which is supported from and sealed to the blade interior by a pair of ribs.

REFERENCES:
patent: 3528751 (1970-09-01), Quinones et al.
patent: 3799696 (1974-04-01), Reedman

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