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. 02, 2020

Filed:

May. 09, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Sylvie Judith Devaux, Maisons-Alfort, FR;

Pierre Yves Heinry, Morsang sur Orge, FR;

Olivier Richard Lefebvre, Melun, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/14 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
B64C 11/14 (2013.01); F02C 7/04 (2013.01); F05D 2260/31 (2013.01); F05D 2260/36 (2013.01); F05D 2260/37 (2013.01);
Abstract

The invention relates to a rotating front part of an aircraft turbomachine intake comprising bolts for attaching a cone tip to an internal support, each bolt comprising a rear end that is screwed into the support and a front end that receives a clamping nut, a rotation-prevention portion of non-circular cross section of each bolt engaging with a hole of corresponding cross section of a rotation-prevention ring. Also provided are extraction bolts, of which a rear end is screwed into the filling piece, each bolt passing through a cone tip flange. Finally, the invention is configured such that, after removal of the nuts, forward tension on the bolts allows the removal of an assembly comprising the tip and the filling piece, while keeping the bolts screwed to the support.


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