Hollow cooled vane for a gas turbine engine

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

1974-11-14

1981-02-24

Bentley, Stephen C.

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

416 96A, 416 97R, F01D 518

Patent

active

042525012

ABSTRACT:
A hollow cooled vane for a gas turbine engine comprises at least two apertured members each mounted spaced from a separate part of the vane interior surface. The first of these members is provided with a supply of cooling air which passes through the apertures in the form of jets to impingement cool the respective first surface, and an interconnecting passage is provided to take this air to the second apertured member where it impingement cools the respective second surface.

REFERENCES:
patent: 3540810 (1970-11-01), Kercher
patent: 3628880 (1971-12-01), Smuland et al.
patent: 3781129 (1973-12-01), Aspinwall
patent: 3806275 (1974-04-01), Aspinwall

Affiliated with

Also associated with

Rating

Hollow cooled vane for a gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Hollow cooled vane for a gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Hollow cooled vane for a gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1406797