Title:
BLADE AND ROTOR ASSEMBLY FOR TURBINE ENGINE
Document Type and Number:
Japanese Patent JP2003148104
Kind Code:
A
Abstract:
To reduce engine weight of a turbine engine.
The blade 203 for the turbine engine having a center line includes a root part extended at a certain angle with respect to the center line and an air foil part 215 extended from the root part. The root part is directly adjacent to the air foil part 215. Namely, the blade 203 has no neck part. The blade 203 is part of the rotor assembly, and preferably, it is a fan blade.
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Inventors:
SUCIU GABRIEL L
BABU MICHAEL
MURDOCK JAMES R
BABU MICHAEL
MURDOCK JAMES R
Application Number:
JP2002326472A
Publication Date:
May 21, 2003
Filing Date:
November 11, 2002
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP
International Classes:
F01D5/14; F01D5/30; F02K3/06; F04D29/34; F04D29/38; (IPC1-7): F01D5/30; F02K3/06; F04D29/34
Attorney, Agent or Firm:
Fujiya Shiga (2 outside)
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