Acoustically stiffened gas-turbine fuel nozzle

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C060S734000

Reexamination Certificate

active

07464552

ABSTRACT:
Under certain conditions, the fuel delivery system can contribute to the formation of strong dynamic pressures in the combustor of a turbine engine. Embodiments of the invention provide a system for dynamically stiffening the fuel supply passage to suppress damaging combustion dynamics. To that end, a Helmholtz resonator can be placed along and in branched relation to the fuel supply passage. The resonator can produce the effect of adding a pressure release opening at a selected location in the fuel line, causing a shift in the fuel line pressure wave pattern that blocks fuel flow fluctuations at the outlet of the fuel passage at the frequency of the oscillation. The pressure wave shift results in a shifting of the volume velocity wave pattern. Ideally, the resonator can be positioned along the flow path such that the volume velocity of the fuel at the fuel passage exit is minimized.

REFERENCES:
patent: 3987633 (1976-10-01), Ford, Jr.
patent: 4173122 (1979-11-01), Wilkinson
patent: 4546733 (1985-10-01), Fukami et al.
patent: 5123835 (1992-06-01), Richards et al.
patent: 5353598 (1994-10-01), Huck et al.
patent: 5373695 (1994-12-01), Aigner et al.
patent: 5791889 (1998-08-01), Gemmen et al.
patent: 5809769 (1998-09-01), Richards et al.
patent: 6058709 (2000-05-01), Richards et al.
patent: 6082108 (2000-07-01), Scheidl et al.
patent: 6205764 (2001-03-01), Hermann et al.
patent: 6370879 (2002-04-01), Stalder et al.
patent: 6430933 (2002-08-01), Keller
patent: 6530221 (2003-03-01), Sattinger et al.
patent: 6546729 (2003-04-01), Hellat et al.
patent: 6634457 (2003-10-01), Paschereit et al.
patent: 2 381 832 (2003-05-01), None
patent: 09004541 (1997-01-01), None
patent: WO 93/10401 (1993-05-01), 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

Acoustically stiffened gas-turbine fuel nozzle does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Acoustically stiffened gas-turbine fuel nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Acoustically stiffened gas-turbine fuel nozzle will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4046514

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