Diffuser/guide vane assembly for a turbomachine

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

Reexamination Certificate

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Details

C415S209300, C415S211200

Reexamination Certificate

active

07955051

ABSTRACT:
A diffuser/guide vane assembly for an aircraft turbojet or turboprop engine is disclosed. The diffuser includes annular flanges joined by blades and the guide vane assembly includes cylindrical shelves joined by vanes. The annular flanges and the cylindrical shelves are formed from metal sheets to which the vanes are assembled by brazing.

REFERENCES:
patent: 3909157 (1975-09-01), Wachtell et al.
patent: 4251183 (1981-02-01), Liu et al.
patent: 7094024 (2006-08-01), Nguyen et al.
patent: 2007/0036646 (2007-02-01), Nguyen et al.
patent: 1 143 108 (2001-10-01), None
patent: 823.442 (1938-01-01), None
patent: WO 01/29424 (2001-04-01), None
patent: WO 02/06676 (2002-01-01), None
patent: WO 2005/042946 (2005-05-01), None

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