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. 10, 2019

Filed:

Mar. 06, 2013
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventor:

Sebastien Marin, Portsmouth, NH (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/20 (2006.01); F04D 29/32 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01);
U.S. Cl.
CPC ...
F01D 5/20 (2013.01); F01D 5/147 (2013.01); F01D 5/286 (2013.01); F04D 29/324 (2013.01); F05D 2240/303 (2013.01); F05D 2300/133 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01);
Abstract

A turbomachine rotor blade, which includes a body radially extending and an insert covering the body tip, the insert being made of a first portion radially covering the blade tip and of a second portion partly covering the intrados face of the blade. The cross-section of the insert along a radial plane with respect to an axis of a rotor is corner-shaped and the first portion of the insert extends tangentially with respect to the main axis of the rotor and the second portion extends globally radially with respect to the main axis of the rotor.


Find Patent Forward Citations

Quick Actions:

Marin, Sebastien. (2019). Turbomachine blade comprising an insert protecting the blade tip (U.S. Patent No. 10408067). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10408067

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

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