Cooling of turbine nozzle containment ring

Details Cooling of turbine nozzle containment ring Cooling of turbine nozzle containment ring

1989-12-08

1992-07-14

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3975, 415115, F02C 100, F03B 1100

Patent

active

051292246

ABSTRACT:
Inexpensive cooling of a gas turbine nozzle and shroud assembly (62, 66, 76) is obtained by locating cooling air passages (84) in the vanes (76) forming part of the nozzle structure (62, 66, 76) so as to allow cooling air to flow between the shrouds (62 and 66).

REFERENCES:
patent: 2149510 (1939-03-01), Darrieus
patent: 2924937 (1960-02-01), Leibach
patent: 3623318 (1971-11-01), Shank
patent: 3937013 (1976-02-01), Aspinwall
patent: 4152092 (1979-05-01), Swearingen
patent: 4162136 (1979-07-01), Parkes
patent: 4311431 (1982-01-01), Barbeau

Affiliated with

Also associated with

Rating

Cooling of turbine nozzle containment ring does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Cooling of turbine nozzle containment ring, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling of turbine nozzle containment ring will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-328391