Title:
燃料ノズルのためのシステム及び方法
Document Type and Number:
Japanese Patent JP6416248
Kind Code:
B2
Abstract:
A system includes an oxidant compressor and a gas turbine engine turbine, which includes a turbine combustor, a turbine, and an exhaust gas compressor. The turbine combustor includes a plurality of diffusion fuel nozzles, each including a first oxidant conduit configured to inject a first oxidant through a plurality of first oxidant openings configured to impart swirling motion to the first oxidant in a first rotational direction, a first fuel conduit configured to inject a first fuel through a plurality of first fuel openings configured to impart swirling motion to the first fuel in a second rotational direction, and a second oxidant conduit configured to inject a second oxidant through a plurality of second oxidant openings configured to impart swirling motion to the second oxidant in a third rotational direction. The first fuel conduit surrounds the first oxidant conduit and the second oxidant conduit surrounds the first fuel conduit.
Inventors:
Zuo By Fan
Jiminsky Willie Steve
Stevenson Christian Xavier
Throbojansky Ilya Alexandrovich
Jiminsky Willie Steve
Stevenson Christian Xavier
Throbojansky Ilya Alexandrovich
Application Number:
JP2016523784A
Publication Date:
October 31, 2018
Filing Date:
June 16, 2014
Export Citation:
Assignee:
Exxon Mobil Upstream Research Company
International Classes:
F23R3/12; F02C3/30; F02C3/34; F02C7/22; F23D11/24; F23D14/22; F23D14/24; F23R3/00; F23R3/28
Domestic Patent References:
| JP2009041838A | ||||
| JP2011141112A | ||||
| JP2005106305A |
Foreign References:
| WO2012003077A1 | ||||
| US20130098048 |
Attorney, Agent or Firm:
Takaki Nishijima
Disciple Maru Ken
Shinichiro Tanaka
Mitsuru Matsushita
Ichiro Kurasawa
Disciple Maru Ken
Shinichiro Tanaka
Mitsuru Matsushita
Ichiro Kurasawa