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. 02, 2021

Filed:

Oct. 08, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Jeremy Giordan, Arcueil, FR;

Thibault Xavier Alexis Berranger, Maincy, FR;

Guillaume Jose Rodrigues, St. Fargeau-Ponthierry, FR;

Stephane Rousselin, Hericy, FR;

Mathieu Raymond Paul Sezeur, Antony, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); G01M 15/14 (2006.01); G01P 5/00 (2006.01); G01M 9/06 (2006.01); G01F 1/34 (2006.01); G01F 15/18 (2006.01);
U.S. Cl.
CPC ...
F01D 25/285 (2013.01); G01F 1/34 (2013.01); G01M 9/065 (2013.01); G01M 15/14 (2013.01); G01P 5/00 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2260/83 (2013.01); F05D 2300/43 (2013.01); G01F 15/18 (2013.01);
Abstract

A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.


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