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:
Dec. 15, 2020

Filed:

Jun. 28, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Matthieu Jean Luc Vollebregt, Asnieres sur Seine, FR;

Patrick Emilien Paul Emile Huchin, Tessancourt sur Aubette, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 33/76 (2006.01); F01D 5/18 (2006.01); B22C 9/10 (2006.01); F01D 5/20 (2006.01);
U.S. Cl.
CPC ...
B29C 33/76 (2013.01); B22C 9/103 (2013.01); F01D 5/187 (2013.01); F01D 5/20 (2013.01); F05D 2230/21 (2013.01); F05D 2260/607 (2013.01); Y02T 50/60 (2013.01);
Abstract

A core for the moulding of a turbine engine blade, this blade including a vane extending along a spanwise direction and ending in a top, this core including a first core element to delimit a first internal cavity and a second core element of which at least one portion delimits a second internal cavity. The second cavity is situated between the first cavity and the top of the blade along the spanwise direction, and the portion of the second core element delimiting the second cavity includes a through hole, which emerges in line with an end face of the first core element to constitute a de-dusting conduit of the first cavity, this conduit traversing the second cavity from end to end while emerging in the top of the blade.


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