Control system for gas-turbine engine

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – With indicator or control of power plant

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C701S003000, C701S004000, C322S014000, C322S015000, C322S024000, C322S028000, C322S099000, C290S04000F, C290S04000F, C244S181000, C244S182000, C060S790000, C060S039281, C702S130000

Reexamination Certificate

active

07571045

ABSTRACT:
In a gas-turbine engine control system having a first control channel inputting the outputs of sensors to calculate and output a first command value indicative of a quantity of fuel to be supplied to the engine and a second control channel inputting the outputs of the sensors to calculate and output a second command value similarly indicative of the quantity of fuel, the second control channel calculates and outputs the second command value using the first command value so long as the instruction to switch the outputs is not generated, while calculates and outputs the second command value, without using the first command value, when the instruction to switch the outputs is generated. With this, immediately after switching to the second command value, the second command value is made substantially equal to and not greatly different from the preceding first command value.

REFERENCES:
patent: 3866109 (1975-02-01), Reed et al.
patent: 3898439 (1975-08-01), Reed et al.
patent: 3924140 (1975-12-01), Yannone
patent: 4031407 (1977-06-01), Reed
patent: 4039804 (1977-08-01), Reed et al.
patent: 4259835 (1981-04-01), Reed et al.
patent: 4494208 (1985-01-01), Chang
patent: 5067080 (1991-11-01), Farman
patent: 5436826 (1995-07-01), O'Flarity
patent: 5913917 (1999-06-01), Murphy
patent: 6063515 (2000-05-01), Epp et al.
patent: 6353790 (2002-03-01), Tsuzuki
patent: 6393355 (2002-05-01), Muramatsu
patent: 6434473 (2002-08-01), Hattori
patent: 7237382 (2007-07-01), Muramatsu et al.
patent: 7246024 (2007-07-01), Muramatsu et al.
patent: 7246495 (2007-07-01), Muramatsu et al.
patent: 2005/0217273 (2005-10-01), Muramatsu et al.
patent: 2005/0217274 (2005-10-01), Muramatsu et al.
patent: 2005/0222822 (2005-10-01), Muramatsu et al.
patent: 2007/0055435 (2007-03-01), Muramatsu et al.
patent: 2 355 081 (2001-04-01), None
Shutler, Control configuration design for the aircraft gas turbine engine, 1995, Internet. p. 22-28.
NASA Technical Memorandum, Jaw et al., Propulsion Control Technology Development in the U.S.—A Historical Perspective, 1940˜2002, Internet, p. 1-3.
Brunell et al., Nonlinear Model Predictive Control of an Aircraft Gas Turbine Engine, 2002, IEEE, p. 4649-4651.
Gorinevsky et al., Model-Based Diagnostics for an Aircraft Auxiliary Power Unit, 2002, Internet, IEEE, p. 1-6.
Spang et al., Jet Engine Control, Implementations, 1999, Internet, p. 14-26.
Chpter 14, Transition to Turbopropeller Power Airplanes, May 7, 2004, Internet, p. 14-1 to 14-12.
Hingston et al., Development of a digital excitation control system, 1989, IEEE, p. 125-129.

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

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

Rate now

     

Profile ID: LFUS-PAI-O-4093663

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