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:
Nov. 12, 2019

Filed:

Oct. 12, 2015
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Roland Tran, Colombes, FR;

Eric Eberschveiler, L'isle-Adam, FR;

Anthony Le Fay, Jouy en Josas, FR;

Patrick Pourfilet, Asnieres sur Seine, FR;

Yvan Rappart, Montreuil, FR;

Monique Tirel, Saint Denis, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B22C 7/02 (2006.01); B22C 9/04 (2006.01); B22C 9/10 (2006.01); B22C 9/20 (2006.01); B22C 9/24 (2006.01); B22D 25/02 (2006.01); B22D 29/00 (2006.01); F01D 5/18 (2006.01); F04D 29/32 (2006.01); F04D 29/58 (2006.01);
U.S. Cl.
CPC ...
B22C 9/20 (2013.01); B22C 7/02 (2013.01); B22C 9/04 (2013.01); B22C 9/108 (2013.01); B22C 9/24 (2013.01); B22D 25/02 (2013.01); B22D 29/001 (2013.01); F01D 5/187 (2013.01); F04D 29/324 (2013.01); F04D 29/582 (2013.01); F05D 2220/323 (2013.01); F05D 2230/211 (2013.01); F05D 2300/10 (2013.01);
Abstract

A stack molding pattern and a shell for manufacturing aircraft turbine engine blades via lost wax casting. The stack molding shell includes a plurality of shell blade elements, each intended for producing a blade, wire elements being arranged within the shell blade elements; and a metal feeder including a plurality of metal outlets, each one radially open towards one of the shell blade elements and connected with the second end portion of the element. The shell includes a protective screen, associated with each second end portion and intended to protect a sensitive portion of the wire elements against the direct impact of a flow of metal from the feeder. The sensitive portion is located in the second end portion, downstream from the protective screen.


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