Cooling system for a gas turbine engine compressor

Power plants – Reaction motor – Interrelated reaction motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60266, 415115, F02C 718, F02K 304

Patent

active

052973867

ABSTRACT:
A cooling system for an axial flow compressor of a gas turbine engine is disclosed having a device to tap a portion of air from the primary air flow flowing through the axial compressor and a control device associated with the tap to control the amount of air tapped from the primary air flow. The system also includes a cooling device to cool the portion of air tapped from the primary air flow, which cooled air is directed into a cooling air chamber. The cooling air chamber is located between the last rotor stage of the compressor and a cone attached to the last stage and extending downstream from the rotor wheel. Nozzles associated with the cooling air chamber direct cooling air from the chamber onto the rotating rotor wheel such that a portion of the cooling air passes into the peripheral groove defined by the rotor wheel between the wheel and the blade root, while another portion of the cooling air from the nozzles is directed onto the surface of the cone in order to cool the blades and the cone.

REFERENCES:
patent: 3647313 (1972-03-01), Koff
patent: 4187675 (1980-02-01), Wakeman
patent: 4254618 (1981-05-01), Elovic
patent: 4645415 (1987-02-01), Hovan et al.
patent: 4657482 (1987-04-01), Neal
patent: 4795307 (1989-01-01), Liebl
patent: 4849895 (1989-07-01), Kervistin
patent: 4920741 (1990-05-01), Liebl
patent: 5163285 (1992-11-01), Mazeaud et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Cooling system for a gas turbine engine compressor 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 system for a gas turbine engine compressor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling system for a gas turbine engine compressor will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-784554

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.