Title:
タービン・エンジン用の大量燃料ノズル
Document Type and Number:
Japanese Patent JP5411793
Kind Code:
B2
Abstract:
A fuel nozzle for a turbine engine is configured to deliver a large volume of a fuel which has a relatively low amount of energy per unit volume. The fuel nozzle includes a fuel swirler plate (120) having fuel delivery apertures (124/126/127/129) which are angled with respect to the flat surfaces of the swirler plate. A nozzle cap (130) covers the end of the fuel nozzle to create a swirl chamber (135) at the outlet end. The nozzle cap may include a plurality of air inlet apertures (136) to allow the air to enter the swirl chamber.
Inventors:
Joel Hall
Application Number:
JP2010101582A
Publication Date:
February 12, 2014
Filing Date:
April 27, 2010
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F23R3/28; F02C7/232
Domestic Patent References:
| JP9145058A | ||||
| JP2008185247A | ||||
| JP2000130757A |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka