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:
Oct. 15, 2019

Filed:

Sep. 18, 2017
Applicant:

Stephane Hiernaux, Oupeye, BE;

Inventor:

Stephane Hiernaux, Oupeye, BE;

Assignee:

Other;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 25/24 (2006.01); F02C 7/04 (2006.01); F04D 29/68 (2006.01); F01D 5/14 (2006.01); F01D 9/06 (2006.01); F02C 9/18 (2006.01); F01D 25/16 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F01D 9/04 (2013.01); F01D 5/145 (2013.01); F01D 9/06 (2013.01); F01D 9/065 (2013.01); F01D 25/24 (2013.01); F02C 7/04 (2013.01); F02C 9/18 (2013.01); F04D 29/682 (2013.01); F04D 29/684 (2013.01); B64D 2033/0226 (2013.01); F01D 25/162 (2013.01); F05D 2270/17 (2013.01); Y02T 50/673 (2013.01);
Abstract

The invention concerns a support casing () for a rotor () of a turbine engine such as a ducted fan turbojet engine used for propulsion of an aircraft. The casing () comprises: an outer annular wall () with an inner annular surface (); an inner hub () able to support the rotor () of the axial turbine engine and comprising an outer annular surface (); an annular passage () between the annular wall () and the inner hub (); an annular row of arms () passing radially through the annular passage (). Each arm () of the casing () comprises an orifice () arranged in the annular passage () radially at the level of one of said annular surfaces (). Inserts are fitted to the orifices () to control the flow passing through.


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