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Patent Searching and Data


Title:
TURBOJET DIFFUSER
Document Type and Number:
Japanese Patent JP2005220904
Kind Code:
A
Abstract:

To provide a method to separably fix a diffuser in a turbojet.

This turbojet diffuser is arranged between a compressor and a combustion chamber, and secured to an outer upstream annular flange of an outer casing of the combustion chamber by a suspension means. The suspension means comprises a first frustoconical wall extending from the outer longitudinal wall of the diffuser towards the combustion chamber and a second frustoconical wall extending towards the compressor between the first frustoconical wall and the outer casing of the combustion chamber.


Inventors:
Sablayrolles, Pierre
Pieussergues, Christophe
Trahot, Denis
Marnas, Laurent
Application Number:
JP2005000016575
Publication Date:
August 18, 2005
Filing Date:
January 25, 2005
Export Citation:
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Assignee:
SNECMA MOTEURS
International Classes:
F23R3/04; F04D29/54; F23R3/60; (IPC1-7): F04D29/54; F23R3/04
Attorney, Agent or Firm:
川口 義雄
小野 誠
大崎 勝真
坪倉 道明