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:
Sep. 17, 2019

Filed:

Nov. 07, 2017
Applicants:

Olivier DE Vriendt, Bassenge, BE;

Laurent Schuster, Erezee, BE;

Inventors:

Olivier De Vriendt, Bassenge, BE;

Laurent Schuster, Erezee, BE;

Assignee:

Other;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/04 (2006.01); F02C 7/047 (2006.01); F01D 25/02 (2006.01); F02K 3/02 (2006.01); F02K 3/06 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F02C 7/047 (2013.01); F01D 25/02 (2013.01); F02K 3/02 (2013.01); F02K 3/06 (2013.01); F04D 29/321 (2013.01); F05D 2220/323 (2013.01); F05D 2240/12 (2013.01); F05D 2250/313 (2013.01); F05D 2260/20 (2013.01);
Abstract

The invention relates to a de-icing splitter nose () of an axial turbine engine, notably a de-icing splitter nose of a turbo-jet engine compressor. The splitter nose includes an annular row of vanes (), each of which has a radially extending leading edge (), and a de-icing system () based on hot-air injection. The injection is pulsed, i.e. discontinuous. The system () includes an annular row of injection orifices for injecting de-icing fluid () onto the vanes () in respective injection directions (). Each injection orifice is associated with a vane such that the injection directions thereof are substantially parallel to the leading edge () of the related vane, enabling said vane () to be de-iced.


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