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:
Jun. 23, 2020
Filed:
Jun. 19, 2017
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Thierry Kohn, Moissy-Cramayel, FR;
Damien Cesar, Moissy-Cramayel, FR;
Julien Sayn-Urpar, Moissy-Cramayel, FR;
Assignee:
Safran Aircraft Engines, Paris, FR;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F04D 29/54 (2006.01); F04D 29/64 (2006.01); F01D 25/16 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 25/005 (2013.01); F01D 25/162 (2013.01); F04D 29/542 (2013.01); F04D 29/644 (2013.01); F05D 2240/121 (2013.01); F05D 2240/122 (2013.01); F05D 2260/30 (2013.01); F05D 2260/37 (2013.01); F05D 2260/38 (2013.01);
Abstract
The invention relates to part of a turbine engine comprising two arms passing through a stream of the turbine engine, wherein each arm comprises an outer surface and an aerodynamic linking device. The aerodynamic linking device comprises fairings extending between the two arms, compressible interface means interposed between the fairings and means for retaining the fairings in place by pressure in relation to the arms, which compress the interface means.