Clearance control method for gas turbine engine

Power plants – Combustion products used as motive fluid

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60 3975, F02C 718

Patent

active

050053523

ABSTRACT:
A method for scheduling the flow of cooling air to a gas turbine engine achieves a varying clearance between the turbine blade tips and surrounding annular shroud responsive to the current engine power level. Excess clearance is provided during operation at less than maximum normal engine power to accommodate the transient decrease in clearance following a step change in engine power level.

REFERENCES:
patent: 4019320 (1977-04-01), Redinger, Jr. et al.
patent: 4304093 (1981-12-01), Schulze
patent: 4329114 (1982-05-01), Johnston et al.
patent: 4487016 (1984-12-01), Schwarz et al.
patent: 4513567 (1985-04-01), Deveau et al.
patent: 4576547 (1986-03-01), Weiner et al.
patent: 4815272 (1989-03-01), Laurello
patent: 4849895 (1989-07-01), Kervistin

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

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

Rate now

     

Profile ID: LFUS-PAI-O-2025320

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