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. 09, 2020

Filed:

Oct. 30, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Vincent Bernard Serge Most, Le Plessis Robinson, FR;

Hubert Jean Marie Fabre, Melun, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23C 3/12 (2006.01); B23Q 35/10 (2006.01); B23Q 35/26 (2006.01); F01D 25/24 (2006.01); B23C 1/16 (2006.01); B23Q 35/28 (2006.01); B23C 3/00 (2006.01);
U.S. Cl.
CPC ...
B23C 3/12 (2013.01); B23C 1/16 (2013.01); B23C 3/00 (2013.01); B23Q 35/104 (2013.01); B23Q 35/26 (2013.01); B23Q 35/28 (2013.01); F01D 25/243 (2013.01); B23C 2215/04 (2013.01); B23C 2220/40 (2013.01); F05D 2230/10 (2013.01); F05D 2230/53 (2013.01); F05D 2240/14 (2013.01);
Abstract

A method of machining an attachment flange of an aircraft turbomachine case, the method also including a system to machine the two opposite surfaces of the flange, and including a shape follower machining module, this module being designed to follow the shape of the flange and including a first structure equipped with a first machining tool, and a second structure equipped with a second machining tool, the flange fitting between the structures such that its two opposite surfaces are machined by tools, the module also including shape follower elements carried by the structures; and a device to drive movement of the machining module along a circumferential direction of the flange.


Find Patent Forward Citations

Most, Vincent Bernard Serge. (2020). Method for machining an attachment flange of an aircraft turbomachine case (U.S. Patent No. 10675691). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10675691

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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