Title:
INTER BLADE PLATFORM OF SIDE DEFLECTION TYPE FOR SUPPORTING BLADE OF TURBO JET ENGINE
Document Type and Number:
Japanese Patent JP2005054784
Kind Code:
A
Abstract:
To provide an inter blade platform of a side deflection type for supporting blades of a turbo jet engine.
The inter blade platform 3 for a blade supporting disc 1 of the turbo jet engine comprises a central portion 5 connected to the supporting disc 1 between two adjacent blades and two side portions 6, 7 extending from two side edges 6, 7 of the central portion 5 and so constructed that each of them is deflected by the impact of the blades 2 facing each other.
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Inventors:
QUERIAULT MICHELE JACQUELINE
LEJARS CLAUDE ROBERT LOUIS
LEJARS CLAUDE ROBERT LOUIS
Application Number:
JP2004221230A
Publication Date:
March 03, 2005
Filing Date:
July 29, 2004
Export Citation:
Assignee:
SNECMA MOTEURS
International Classes:
F01D5/22; F01D11/00; F01D21/04; F02C3/04; F01D5/30; F02C7/04; F04D29/34; (IPC1-7): F04D29/34; F02C3/04; F02C7/04
Attorney, Agent or Firm:
Yoshio Kawaguchi
Akio Ichiiri
Makoto Ono
Katsuma Osaki
Mitsuaki Tsubokura
Akio Ichiiri
Makoto Ono
Katsuma Osaki
Mitsuaki Tsubokura
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