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:
Feb. 01, 2022

Filed:

Jun. 20, 2019
Applicant:

Safran Aero Boosters SA, Herstal, BE;

Inventor:

Morgan Vyvey, Flemalle, BE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01); F04D 29/56 (2006.01); F04D 29/64 (2006.01);
U.S. Cl.
CPC ...
F01D 17/162 (2013.01); F04D 29/563 (2013.01); F04D 29/644 (2013.01); F05D 2220/32 (2013.01); F05D 2240/128 (2013.01);
Abstract

The invention relates to a turbine engine () compressor shroud, comprising: first and second sections () and respective flanges (), the flanges () making it possible to hold the two sections () together, the first section () comprising a cylindrical surface () forming a seat for an actuating device () for orienting stator blades (), characterised in that the first shroud () comprises a tubular wall () axially overlapping both flanges () and said cylindrical surface () is an outer surface of the tubular wall (). The invention also relates to an assembly with the shroud (), the blade () and means () for actuating the orientation of the blade (), the shroud being produced using the kit described above. The invention finally relates to a method for assembling a compressor with such an assembly.


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