Reverse-flow gas turbine combustion system

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

C060S760000, C060S772000

Reexamination Certificate

active

07966822

ABSTRACT:
A gas turbine combustion system for burning air and fuel into exhaust gases. The gas turbine combustion system may include a combustor, a turbine nozzle integral with the combustor for providing the air to the combustor, and a fuel injector for providing the fuel to the combustor. The turbine nozzle and the fuel injector are positioned within the combustor such that a mixture of the air and the fuel flows in a first direction and the exhaust gases flow in a second direction.

REFERENCES:
patent: 2922279 (1960-01-01), Roberson et al.
patent: 2930192 (1960-03-01), Johnson
patent: 3608309 (1971-09-01), Hill et al.
patent: 3831854 (1974-08-01), Sato et al.
patent: 4040252 (1977-08-01), Mosier et al.
patent: 4211073 (1980-07-01), Guillot
patent: 4474014 (1984-10-01), Markowski
patent: 4549402 (1985-10-01), Saintsburry et al.
patent: 4628687 (1986-12-01), Strom
patent: 4719748 (1988-01-01), Davis et al.
patent: 4944152 (1990-07-01), Shekleton
patent: 5255742 (1993-10-01), Mikus
patent: 5404952 (1995-04-01), Vinegar
patent: 5515680 (1996-05-01), Fujimura et al.
patent: 5862858 (1999-01-01), Wellington et al.
patent: 5899269 (1999-05-01), Wellington et al.
patent: 6019172 (2000-02-01), Wellington et al.
patent: 6269882 (2001-08-01), Wellington et al.
patent: 6599119 (2003-07-01), Wood et al.
patent: 6752620 (2004-06-01), Heier et al.
patent: 2004/0011055 (2004-01-01), Inoue et al.
patent: 2124747 (1984-02-01), None
Title: Ultralow-Nox Combustor for Nonpremixed & Premixed Gaseous and Liquid Fuels; Authors: Yedidia Neumeir, et al.; ASME Technical Publication GT2005-69118; 1 pg.
Title: Laseroptical Investigation of Highly Preheated Combustion with Strong Exhaust Gas Recirculation; Twenty-Seventh Symposium (International) on Combustion/The Combustion Institute; Authors: Tobias Plessing, et al.; date 1998, pp. 3197-3204.
AFRC-JFRC International Combustion Symposium; Title: Flameless Combustion or Stagnation Point Reverse Flow Combustor (SPRFC); Authors: Zinn, et al.; Dated: Oct. 11, 2004; pp. 1-7.
Proceedings of GT2005, ASME Turbo Expo 2005: Power for Land, Sea & Air; Title Fundamental of Low-NOX Gas Turbine Adiabatic Combustor; Authors: Levy, et al; Date: 2005; pp. 1-11.

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

Reverse-flow gas turbine combustion system does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-2727896

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