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.
Patent No.:
Date of Patent:
May. 16, 2023
Filed:
Sep. 04, 2019
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Antonin Etienne Diego Tessiereau, Moissy-Cramayel, FR;
Cyrille François Antoine Mathias, Moissy-Cramayel, FR;
Wouter Balk, Moissy-Cramayel, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); F01D 25/00 (2006.01); F01D 25/24 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F01D 25/28 (2013.01); F01D 9/02 (2013.01); F01D 25/005 (2013.01); F01D 25/24 (2013.01); F05D 2240/14 (2013.01); F05D 2250/231 (2013.01); F05D 2250/232 (2013.01); F05D 2260/31 (2013.01); F05D 2260/606 (2013.01); F05D 2300/603 (2013.01);
Abstract
The invention relates to an assembly for a turbomachine with a longitudinal axis comprising a first annular wall (), panels () being arranged around the longitudinal axis (A) and extending radially opposite said first annular wall () so as to form a flow surface for a flow of air, each panel () being secured to the first annular wall () by at least one fixing member () passing through an orifice in the panel () and secured to the first annular wall () by means of a sleeve and a stud forming a spacer.