The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 26, 2007

Filed:

Mar. 23, 2005
Applicants:

Sébastien Imbourg, Yerres, FR;

Claude Mons, Savigny le Temple, FR;

Philippe Pabion, Vaux le Penil, FR;

Jean-iuc Soupizon, Vaux le Penil, FR;

Inventors:

Sébastien Imbourg, Yerres, FR;

Claude Mons, Savigny le Temple, FR;

Philippe Pabion, Vaux le Penil, FR;

Jean-Iuc Soupizon, Vaux le Penil, FR;

Assignee:

SNECMA Moteurs, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbine stator casing comprising a jacket and fastener hooks for fastening a turbine distributor nozzle, the hooks projecting from the inside face of the jacket, said jacket being made of a first alloy by hot isostatic compression using metal powder, said fastener hooks being made out of a second alloy that is more refractory than the first, and being secured to said jacket by diffusion welding during the hot isostatic compression. The casing also comprises inserts passing through the fastener hooks and through said jacket. These inserts, which are likewise secured to the jacket by diffusion welding, serve during manufacture of the casing to fasten the hooks to a mold portion inside which the jacket is formed. The invention is applicable to the turbines of airplane turbojets.


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