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Title:
ガスタービンエンジン及びガスタービンエンジン部品
Document Type and Number:
Japanese Patent JP5009603
Kind Code:
B2
Abstract:
A gas turbine engine component with a deicing structure (50) that includes a first side (64), an opposite second side (66), at least one capillary (84) positioned adjacent to an external surface (88) of at least one of said first and second sides, and a composite layer (90) securing the at least one said capillary to said component.

Inventors:
Stephen Craig Mitchell
Application Number:
JP2006342207A
Publication Date:
August 22, 2012
Filing Date:
December 20, 2006
Export Citation:
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Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F01D25/12; F01D25/02; F01D25/24; F02C7/047
Domestic Patent References:
JP2005501168A
Foreign References:
US5228643
US4079903
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa