IP Library Granted Patent US 7,931,459
Granted Patent B2
US 7,931,459 · App. 12/100,526 · Granted Apr 26, 2011

Tool for manufacturing ceramic casting cores for turbomachine blades

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Quick Facts
Patent No.
US 7,931,459
App. No.
12/100,526
Granted
Apr 26, 2011
Kind
B2
Abstract

A tool for manufacturing a casting core, for a turbomachine blade with a leading edge and a trailing edge, the core includes a thick part on the leading edge side and a thin part on the trailing edge side is disclosed. The tool includes first and second dies of the core that are moveable in a direction with respect to each other between a molding position and a demolding position, sub-components that are moveable relative to the dies, and mechanical ejectors that are provided on the first and second dies. The parts of the dies corresponding to the thin part of the core do not include a movable sub-component. The thin part of the core is demolded along the main direction of opening of the first and second dies.

Claims (14)

1. A tool for manufacturing a casting core, for a turbomachine blade with a pressure side, a suction side, a leading edge and a trailing edge, the core comprising a thick part on the leading edge side and a thin part on the trailing edge side, the tool comprising:

first and second dies of the core that are moveable in a direction with respect to the each other between a molding position and a demolding position;

sub-components that are moveable relative to the dies; and

mechanical ejectors which are provided on one of the first or second dies,

wherein the dies on said thin part are free of a movable sub-component,

wherein the thin part is demolded along a main direction of opening of the first and second dies,

wherein said thin part is substantially perpendicular to the main direction of opening of the first and second dies,

wherein the dies include decorations for the formation of cavities in the core, and

wherein a main axis of the decorations in the dies corresponding to the trailing edge extending from the pressure side on the first die to the suction side on the second die is substantially parallel to the main direction of opening of the first and second dies.

2. The tool as claimed in claim 1 , wherein the two dies are moveable translationally between the molding position and the demolding position.

3. The tool as claimed in claim 1 , wherein at least one of the two dies a location corresponding to the thin zone, is shaped so as to obtain padding parts which locally facilitates filling of the mold at injection, and the padding parts are machined to reduce their thickness.

4. The tool as claimed in claim 1 , wherein the dies on the thick part include the moveable sub-components.

5. The tool as claimed in claim 1 , wherein the ejectors move substantially parallel to the main axis of the decorations in the dies corresponding to the trailing edge.

6. The tool as claimed in claim 5 , wherein the main axis of the decorations in the dies corresponding to the trailing edge extend in a vertical direction.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 10, 2008
From: LOUESDON, YVON; PRIGENT, SERGE; VERGER, JEAN-LOUIS MARTIAL
To: SNECMA
Reel/Frame 020782/0251 →