Title:
高温ダクト装置を支持する方法及び装置
Document Type and Number:
Japanese Patent JP4471612
Kind Code:
B2
Abstract:
A method enables a duct to be coupled to a gas turbine engine casing. The method comprises extending a first inner tube support member (220) circumferentially around the duct, such that a radially inner side (226) of the first inner tube support is against the duct, and wherein the first inner tube support member has a substantially curved cross sectional profile extending between the radially inner side of the first inner tube support, and a radially outer side (224) of the first inner tube support. The method also comprises extending an outer tube support member (204) circumferentially around the first inner tube support member such that the outer tube support member is against the first inner tube support member outer surface, and coupling the outer tube support member to the gas turbine engine casing.
Inventors:
Mark Douglas Swinford
Kevin Todd Bowers
Kevin Todd Bowers
Application Number:
JP2003327077A
Publication Date:
June 02, 2010
Filing Date:
September 19, 2003
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F02C6/06; F02C6/08; F01D9/02; F01D25/00; F01D25/02; F01D25/24; F02C7/00; F02C7/047; F02K1/80
Domestic Patent References:
JP11132399A | ||||
JP3234251A | ||||
JP58136893U | ||||
JP2001041005A | ||||
JP9178072A | ||||
JP57190193A |
Foreign References:
US3666251 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Nobukazu Ito
Hirokazu Ogura
Nobukazu Ito