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:
Dec. 31, 2024
Filed:
Jan. 07, 2020
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventor:
Marc Missout, Moissy-Cramayel, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B33Y 80/00 (2015.01); F01D 5/28 (2006.01); F01D 9/04 (2006.01); F02C 7/20 (2006.01); F02K 3/06 (2006.01); F04D 29/02 (2006.01); F04D 29/54 (2006.01); B33Y 10/00 (2015.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B33Y 80/00 (2014.12); F01D 5/28 (2013.01); F01D 9/041 (2013.01); F02C 7/20 (2013.01); F02K 3/06 (2013.01); F04D 29/023 (2013.01); F04D 29/542 (2013.01); B33Y 10/00 (2014.12); F05D 2220/323 (2013.01); F05D 2230/31 (2013.01); F05D 2240/12 (2013.01);
Abstract
An aerodynamic arm for an aircraft turbine engine casing includes a tubular outer shell having a generally elongate shape extending substantially along an axis. The shell has axial ends configured to be connected to a turbine engine casing. An electrically conductive core extends inside the shell and has ends configured to electrically connect to the ends of the shell. An insulating material occupies a space between the core and the shell.