Gas turbine engine power availability measurement

Details Gas turbine engine power availability measurement Gas turbine engine power availability measurement

G - Physics

01

M

354/24

G01M 15/00 (2006.01) B64D 31/00 (2006.01) F02C 9/00 (2006.01) F02D 41/24 (2006.01) G01L 3/24 (2006.01)

Patent

CA 1181852

ABSTRACT OF THE DISCLOSURE A method of determining the power which may be produc- ed by a gas turbine engine is described in which the engine has a compressor and power turbine and is instrumented to provide signals commensurate with a plurality of operating parameters and limits. The method determines the maximum parmissible engine gas generator speed for the existing engine inlet conditions, corrects the maximum permissible gas generator speed for deviation in performance of the engine from a predetermined normal, employs the corrected maximum permissible speed to determine the maximum torque which can be produced for the existing inlet conditions; and compares the determined torque with the engine torque limit to ascertain the maximum obtainable torque.

426111

Affiliated with

Also associated with

Rating

Gas turbine engine power availability measurement 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 power availability measurement, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine engine power availability measurement will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1278897