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:
Jun. 16, 2020

Filed:

May. 24, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Antoine Jean Jausovec, Tournan-en-Brie, FR;

Eric Roger Schwartz, Seine-Port, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); F01D 9/04 (2006.01); F01D 17/08 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F01D 9/041 (2013.01); F01D 17/08 (2013.01); F05D 2220/32 (2013.01); F05D 2230/237 (2013.01); F05D 2240/121 (2013.01); F05D 2240/128 (2013.01); F05D 2240/55 (2013.01); F05D 2260/20 (2013.01); F05D 2260/83 (2013.01);
Abstract

A device that measures turbomachine aerodynamic flow parameters is presented. The device includes the information collection elements relating to the flow parameters, and a body that includes the information collection elements. The body features a portion that is elongated in the longitudinal direction and configured to form the leading edge of a turbomachine vane, and a first side portion that laterally extends portion in an axial direction, wherein the information collection elements protrude from the leading edge of the portion and the portion includes internal channels that route the information and individually communicate with at least one information collection elements, wherein the first side portion features a first surface configured to fit, at least partially, onto a second surface of an intrados or extrados wall of a turbomachine vane.


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