Method and system for controlling gas turbine engine

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C060S039281

Reexamination Certificate

active

07051533

ABSTRACT:
In a control method of a gas turbine engine, an engine controller4outputs a combustor power command FD based on an engine condition from an engine condition detector3. Then, a combustion controller6determines each fuel flow rate based on the combustion power command FD. The combustor controller6overrides each fuel flow rate for a certain period, to realize smooth stage-process.

REFERENCES:
patent: 4716719 (1988-01-01), Takahashi et al.
patent: 5024055 (1991-06-01), Sato et al.
patent: 5054280 (1991-10-01), Ishibashi et al.
patent: 5806299 (1998-09-01), Bauermeister et al.
patent: 6092362 (2000-07-01), Nagafuchi et al.
patent: 6282885 (2001-09-01), Muramatsu et al.
patent: A 61-241425 (1986-10-01), None
patent: A 62-206237 (1987-09-01), None
patent: A 63-61725 (1988-03-01), None
patent: A 63-134825 (1988-06-01), None
patent: A 7-4265 (1995-01-01), None
patent: A 10-212976 (1998-08-01), None
patent: A 2000-248964 (2000-09-01), None
patent: A 2002-257345 (2002-09-01), None

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

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

Rate now

     

Profile ID: LFUS-PAI-O-3571900

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