Title:
ターボ機械用のデュアル燃料燃焼器ノズル
Document Type and Number:
Japanese Patent JP5588803
Kind Code:
B2
Abstract:
A dual fuel combustor nozzle includes a body member including a first end portion that extends to a second end portion through an intermediate portion. The intermediate portion includes an outer wall portion and an inner wall portion with the inner wall portion defining a first fuel plenum. The dual fuel nozzle also includes an inner nozzle member arranged within the first fuel plenum. The inner nozzle member includes a first end section that extends to a second end section through an intermediate section. The intermediate section defines a second fuel plenum. The second end section being spaced from the second end portion of the body member so as to define a pre-emergence zone.
Inventors:
アブデュル Raffee Kern
Christian ゼイヴィアー Stevenson
Bay fan ズオ
Christian ゼイヴィアー Stevenson
Bay fan ズオ
Application Number:
JP2010199435A
Publication Date:
September 10, 2014
Filing Date:
September 07, 2010
Export Citation:
Assignee:
General Electric Co.
International Classes:
F23R3/36; F02C7/22; F23R3/28
Attorney, Agent or Firm:
Satoshi Arakawa
Hiroshi Ogura
Toshihisa Kurokawa
Hiroshi Ogura
Toshihisa Kurokawa