Gas turbine engine active clearance control

Power plants – Combustion products used as motive fluid

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415178, F02G 300, F01D 1108

Patent

active

045135673

ABSTRACT:
Method for controlling the clearance between rotating and stationary components of a gas turbine engine are disclosed. Techniques for achieving close correspondence between the radial position of rotor blade tips and the circumscribing outer air seals are disclosed. In one embodiment turbine case temperature modifying air is provided in flow rate, pressure and temperature varied as a function of engine operating condition. The modifying air is scheduled from a modulating and mixing valve supplied with dual source compressor air. One source supplies relatively low pressure, low temperature air and the other source supplies relatively high pressure, high temperature air. After the air has been used for the active clearance control (cooling the high pressure turbine case) it is then used for cooling the structure that supports the outer air seal and other high pressure turbine component parts.

REFERENCES:
patent: 3039737 (1962-06-01), Kolthoff
patent: 3911354 (1975-10-01), Stanton
patent: 3914952 (1975-10-01), Barbier
patent: 3957391 (1976-05-01), Vollinger
patent: 3966354 (1976-06-01), Patterson
patent: 3975112 (1976-08-01), Brown et al.
patent: 3975901 (1976-08-01), Hallinger et al.
patent: 4005946 (1977-02-01), Brown et al.
patent: 4019320 (1977-04-01), Redinger et al.
patent: 4069662 (1978-01-01), Redinger et al.
patent: 4213296 (1980-07-01), Schwarz
patent: 4230436 (1980-10-01), Davison
patent: 4242042 (1980-12-01), Schwarz
patent: 4279123 (1981-07-01), Griffin et al.
patent: 4304093 (1981-12-01), Schulze
patent: 4317646 (1982-03-01), Steel 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

Gas turbine engine active clearance control does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine engine active clearance control, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine engine active clearance control will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1961900

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