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:
Mar. 09, 2021

Filed:

May. 05, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Axel Sylvain Loïc Thomas, Moissy-Cramayel, FR;

Maurice Guy Judet, Moissy-Cramayel, FR;

Gabrijel Radeljak, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 9/042 (2013.01); F01D 25/246 (2013.01); F05D 2230/64 (2013.01); Y02T 50/60 (2013.01);
Abstract

Assembly () comprising an annular turbine distributor () for turbomachinery (), an annular structural element () of the turbomachinery (), coaxial with the distributor () and at least one device () for attaching the annular distributor () with the annular structural element (), characterised in that: —the annular distributor () is crossed by at least two axial passages, and —the or each attachment device () comprises: at least two pins (), rigidly connected to the annular structural element () and passing through one of said passages of the distributor (), a first transverse stop () for stopping the distributor () axially and passing through two consecutive pins (), and two second stops () rigidly connected to the structural element () to retain, in the pins (), the first transverse stop () for stopping the distributor () radially.


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