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. 04, 2019

Filed:

Oct. 20, 2015
Applicant:

Techspace Aero S.a., Herstal (Milmort), BE;

Inventors:

Ghislain Herbaut, Berloz, BE;

David Bouillon, Woluwe-Saint-Lambert, BE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/02 (2006.01); F01D 9/04 (2006.01); F01D 25/24 (2006.01); H05H 1/24 (2006.01); B64D 15/12 (2006.01); B64D 15/16 (2006.01); F02C 7/047 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F01D 25/02 (2013.01); B64D 15/12 (2013.01); B64D 15/163 (2013.01); B64D 33/02 (2013.01); F01D 9/041 (2013.01); F01D 25/24 (2013.01); F02C 7/047 (2013.01); H05H 1/2406 (2013.01); B64D 2033/0226 (2013.01); B64D 2033/0233 (2013.01); F05D 2220/30 (2013.01); F05D 2240/12 (2013.01); F05D 2270/172 (2013.01); F05D 2300/40 (2013.01); F05D 2300/603 (2013.01); H05H 2001/2425 (2013.01); Y02T 50/672 (2013.01);
Abstract

The invention deals with a splitter nose delimiting the inlet of a low-pressure compressor of an axial turbine engine. The splitter nose comprises a separation surface with an upstream circular edge suitable for separating a flow entering into the turbine engine into a primary flow and a secondary flow, and a plasma de-icing device. The device comprises two annular layers of dielectric material () partially forming the separation surface, an electrode forming the upstream edge, an electrode forming an outer wall of the splitter nose, an electrode forming an outer shroud which supports blades, an electrode delimiting the primary flow. The device generates plasmas () opposing the presence of ice on the partitions of the splitter nose. The invention also deals with a turbine engine with a splitter nose that is provided with a de-icing system downstream of the fan.


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