Gas turbine engine control

Power plants – Reaction motor – Method of operation

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60242, F02K 115

Patent

active

045818894

ABSTRACT:
In one form of the present invention, the thrust of a gas turbine engine is inferred. If a droop in thrust is predicted, components of the engine are modulated in response to restore thrust.

REFERENCES:
patent: 2971326 (1961-02-01), Peters et al.
patent: 2979889 (1961-04-01), Hurtle et al.
patent: 3747344 (1973-07-01), Porter et al.
patent: 4139887 (1979-02-01), Levesque
patent: 4467600 (1984-08-01), Peikert

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

Rate now

     

Profile ID: LFUS-PAI-O-1431837

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