Axial flow gas turbines

Details Axial flow gas turbines Axial flow gas turbines

1984-01-18

1993-12-07

Walsh, Donald P.

Rotary kinetic fluid motors or pumps

With changing state confined heat exchange mass

415175, F02C 718

Patent

active

052678318

ABSTRACT:
An axial flow gas turbine is provided with a shroud ring which is defined by two axially adjacent heat pipes. The radially inner face of the shroud ring has a plurality of axially extending cooling air passages located adjacent to it. Cooling air, which in operation is directed through the passages serves to provide cooling of the shroud ring and the substantial elimination of any radial heat flux in the shroud ring.

REFERENCES:
patent: 4017207 (1977-04-01), Bell
patent: 4199300 (1980-04-01), Tubbs
patent: 4419044 (1983-12-01), Barry

Affiliated with

Also associated with

Rating

Axial flow gas turbines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Axial flow gas turbines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Axial flow gas turbines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2012254