Gas turbine combustor

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

C060S746000

Reexamination Certificate

active

06915637

ABSTRACT:
A gas turbine combustor is provided with a nozzle extension tube having an inclination outward in a diameter direction of a combustor inner cylinder and in a peripheral direction of the combustor inner cylinder. As a result, the premixed gas is transformed to a spiral flow passing into a combustion chamber while turning, i.e., an outward turning flow, thereby sufficiently mixing the premixed gas while the premixed gas is flowing in the combustion chamber.

REFERENCES:
patent: 5596873 (1997-01-01), Joshi et al.
patent: 5836164 (1998-11-01), Tsukahara et al.
patent: 6038861 (2000-03-01), Amos et al.
patent: 6068467 (2000-05-01), Mandai et al.
patent: 6082111 (2000-07-01), Stokes
patent: 1 103 767 (2001-05-01), None
patent: 7-248118 (1995-09-01), None
patent: 8-28871 (1996-02-01), None
Y. Kinoshita, et al., pps 53-61, “Research on Low NOxCombustion Technique in HYPR Project”, Dec. 14, 1999 (with English Translation).

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

Rate now

     

Profile ID: LFUS-PAI-O-3414427

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