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:
Mar. 24, 2020

Filed:

May. 03, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Christophe Scholtes, Moissy-Cramayel, FR;

Cedric Michel Claude Chretien, Moissy Cramayel, FR;

Thomas Nolwenn Emmanuel Delahaye, Moissy Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01P 7/06 (2006.01); F04D 29/56 (2006.01); F01D 25/02 (2006.01); F02C 7/047 (2006.01); F01D 17/16 (2006.01); F01D 9/06 (2006.01); F01D 5/18 (2006.01); F02K 3/04 (2006.01); F04D 29/54 (2006.01); F04D 29/58 (2006.01);
U.S. Cl.
CPC ...
F04D 29/563 (2013.01); F01D 5/18 (2013.01); F01D 9/065 (2013.01); F01D 17/162 (2013.01); F01D 25/02 (2013.01); F02C 7/047 (2013.01); F02K 3/04 (2013.01); F04D 29/544 (2013.01); F04D 29/582 (2013.01); F05D 2220/323 (2013.01); F05D 2240/12 (2013.01); Y02T 50/676 (2013.01);
Abstract

A vane for turbomachinery, such as, for example, an aircraft turbojet or turbofan engine, or an aircraft turboprop engine. The vane includes: (i) a first deicing fluid flow circuit inside the vane; (ii) a second deicing fluid flow circuit inside the vane; and (iii) a selector for directing the majority of the fluid towards the first circuit when the turbomachinery is in a first operating state, and for directing the majority of the fluid towards the second circuit when the turbomachinery is in a second operating state.


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