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:
Aug. 11, 2020

Filed:

Jan. 10, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Christophe Scholtes, Moissy-Cramayel, FR;

Antoine Robert Alain Brunet, Moissy-Cramayel, FR;

Simon Jose Pierre Amoedo, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/047 (2006.01); F01D 25/02 (2006.01); F01D 25/24 (2006.01); F02K 3/06 (2006.01); B64D 15/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/02 (2013.01); B64D 15/04 (2013.01); F01D 25/246 (2013.01); F02C 7/047 (2013.01); F02K 3/06 (2013.01); F05D 2240/121 (2013.01);
Abstract

A deicer device deices both a splitter nose and inlet guide vanes of an aviation turbine engine. The device includes a splitter nose to split a stream coming from the fan into primary and secondary stream flow channels of annular shape and an inner shroud to which inlet guide vanes are fastened and including a hook that holds the inner shroud axially at its upstream end against the inner annular wall. An outer surface facing of the hook forms an angle of less than 90° with an injection orifice such that the outer surface comes progressively closer to the outer annular wall on going away from the injection orifice. The outer surface of the hook presents a minimum amount of clearance J relative to the outer annular wall such that 0.2≤J/D≤0.6 where D is the hydraulic diameter of an injection orifice.


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