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:
May. 09, 2017

Filed:

Jan. 27, 2014
Applicant:

Snecma, Paris, FR;

Inventors:

Nadege Hugon, Montgeron, FR;

Gilles Alain Charier, La Grande Paroisse, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); F01D 25/18 (2006.01); F01D 9/06 (2006.01); F01D 25/28 (2006.01); F01D 25/16 (2006.01); F02K 3/072 (2006.01); F02C 3/067 (2006.01);
U.S. Cl.
CPC ...
F01D 9/065 (2013.01); F01D 25/16 (2013.01); F01D 25/18 (2013.01); F01D 25/28 (2013.01); F02C 3/067 (2013.01); F02C 7/32 (2013.01); F02K 3/072 (2013.01); F05D 2220/323 (2013.01); F05D 2230/64 (2013.01); F05D 2240/50 (2013.01); F05D 2240/61 (2013.01); F05D 2250/70 (2013.01); F05D 2260/30 (2013.01); F05D 2260/40 (2013.01); F05D 2260/96 (2013.01); Y02T 50/671 (2013.01); Y10T 29/49826 (2015.01);
Abstract

The invention relates to a fixed turbine engine receiver part comprising a fixed hollow shaft for carrying ancillary systems of a turbine engine, centered on the turbine engine axis, turbine engine ancillary systems, an assembly for holding ancillary systems in position situated inside the fixed hollow shaft. The assembly for holding ancillary systems in position comprises at least one first ancillary system support ring, having an axis substantially parallel with the turbine engine axis, a first distance sleeve for holding the first ancillary system support ring in position, having an axis substantially parallel with the turbine engine axis, the first distance sleeve bearing against the first support ring, such that the first support ring comprises a plurality of mutually separated through holes, each through hole defining a passage for at least one ancillary system, each through hole being traversed by at least one of the ancillary systems of the turbine engine.


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