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Title:
FUEL LANCE FOR LIQUID AND/OR GASEOUS FUEL AND METHOD FOR OPERATION THEREOF
Document Type and Number:
Japanese Patent JP3672597
Kind Code:
B2
Abstract:

PURPOSE: To enhance combustion efficiency while reducing emission of harmful components by providing an appropriate nozzle and a cooling air supply unit surrounding a lance like an outer shell and cooling the lance and fuel with cooling air thereby preventing early firing.
CONSTITUTION: A fuel lance for use in a combustion chamber defined by the casing of a gas turbine includes a liquid fuel pipe 7 surrounded by an elongated lance outer shell 11 and secured to the easing by a holding arm projecting sideways, a gas pipe 9 forming a gas passage around the liquid fuel pipe 7, and the lance outer shell 11 forming an air passage 10 around the gas pipe 9. An air/fuel nozzle 12 is provided on the side at the downstream end part of the fuel lance, a gas pipe 9 is provided with a gas nozzle 15 for ejecting gas from a gas passage 8 together with air, and the liquid fuel pipe 7 is provided with a liquid fuel nozzle 18 for ejecting liquid fuel through the air passage 10 and the air/fuel nozzle 12.


Inventors:
Adnan Eroguru
Franz Yose
Peter Novasek
Peter Zeniol
Application Number:
JP18858194A
Publication Date:
July 20, 2005
Filing Date:
August 10, 1994
Export Citation:
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Assignee:
ALSTOM
International Classes:
B05B1/00; F23D11/10; F23D14/22; F23D14/78; F23D17/00; (IPC1-7): F23D17/00
Domestic Patent References:
JP61043637U
JP63002726Y1
Foreign References:
GB2021254B
Attorney, Agent or Firm:
Toshio Yano
Toshiomi Yamazaki
Takuya Kuno
Einzel Felix-Reinhard