IP Library Granted Patent US 10,835,951
Granted Patent B2
US 10,835,951 · App. 16/320,666 · Granted Nov 17, 2020

Method for creating a nonpermanent model

Inventors: Adrien Bernard Vincent Rollinger (Moissy-Cramayel, FR); Mathieu Jean Luc Vollebregt (Moissy-Cramayel, FR); Joseph Toussaint Tami Lizuzu (Moissy-Cramayel, FR); Vincent Marc Herb (Moissy-Cramayel, FR); Didier Maurice Marceau Guerche (Moissy-Cramayel, FR); Ramzi Bohli (Moissy-Cramayel, FR)
Assignees: Safran; Safran Aircraft Engines
B22C9/103B22C9/108B22C9/24B22C21/14
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Quick Facts
Patent No.
US 10,835,951
App. No.
16/320,666
Granted
Nov 17, 2020
Kind
B2
Abstract

The invention provides a method of assembling together a first core ( 12 ) and a second core ( 14 ) in order to make a non-permanent model configured for use in lost wax molding to form a part having a first cavity and a second cavity corresponding respectively to the first core and to the second core. The invention is characterized by the fact that the first and second cores ( 12, 14 ) are assembled together with a first spacer ( 20 ), the first spacer ( 20 ) being arranged between the first and second cores.

Claims (19)

1. A method of assembling together a first core and a second core in order to make a non-permanent model configured for use in lost wax molding to form a part having a first cavity and a second cavity corresponding respectively to the first core and to the second core, wherein the first and second cores are assembled together with a first spacer, the first spacer being arranged between the first and second cores, wherein the first and second cores are separated by a first distance, wherein the first spacer presents a thickness less than the first distance, so as to define a first gap between the first spacer and one of the first or second cores, and wherein the first gap is dimensioned in such a manner as to prevent wax from penetrating into a space defined between the first and second cores while wax is being injected.

2. The method according to claim 1 , wherein the first spacer includes a meltable material.

3. The method according to claim 1 , wherein the first gap is dimensioned as a function of a viscosity of wax used for making the non-permanent model.

4. The method according to claim 1 , wherein the gap between the first spacer and one of the first or second cores lies in the range 0.01 mm to 0.35 mm.

5. The method according to claim 1 , further comprising a step in which the first spacer is fixed on one of the first or second cores.

6. The method according to claim 1 , wherein the gap between the first spacer and one of the first or second cores lies in the range 0.03 mm to 0.30 mm.

7. The method according to claim 1 , wherein the gap between the first spacer and one of the first or second cores lies in the range 0.05 mm to 0.25 mm.

8. The method according to claim 1 , wherein the first spacer includes wax.

9. The method according to claim 1 , wherein the first spacer is fixed on one of the first or second cores.

10. The method according to claim 9 , wherein the first spacer is fixed to the one of the first or second cores via complementary shapes.

11. The method according to claim 1 , wherein one or more of the first or second cores includes at least one complex surface.

12. The method according to claim 11 , wherein the first spacer includes one or more of a cavity, an orifice, or a protuberance that, in each case, has a shape complementary to at least a portion of the at least one complex surface.

13. A method of assembling together a first core and a second core in order to make a non-permanent model configured for use in lost wax molding to form a part having a first cavity and a second cavity corresponding respectively to the first core and to the second core, wherein the first and second cores are assembled together with a first spacer, the first spacer being arranged between the first and second cores, wherein the first spacer includes a first spacer element arranged between the first and second cores and configured to maintain the position of the first spacer relative to the first and second cores, and wherein the first spacer element includes a first housing configured to receive the second core.

14. The method according to claim 13 , wherein the first spacer element is arranged between the first core and the second core so as to present at least a first point of contact with the first core.

15. A method of assembling together a first core and a second core in order to make a non-permanent model configured for use in lost wax molding to form a part having a first cavity and a second cavity corresponding respectively to the first core and to the second core, wherein the first and second cores are assembled together with a first spacer, the first spacer being arranged between the first and second cores, wherein the method further includes a step of assembling a third core and a second spacer with the first and second cores, the second spacer being arranged between the first and third cores, and wherein the second spacer has a second spacer element, the first and second spacer elements being configured to be assembled together in an out-of-part zone.

16. The method according to claim 15 , wherein the first and second spacer elements are configured for being assembled together by complementary shapes.

17. The method according to claim 15 , wherein the first and second spacer elements are configured so as to be fixed relative to each other in at least one direction.

18. The method according to claim 15 , wherein the first and second spacer elements are fixed to each other.

19. The method according to claim 15 , wherein the second spacer element includes a second housing configured to receive the third core.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 15, 2019
From: ROLLINGER, ADRIEN BERNARD VINCENT; VOLLEBREGT, MATHIEU JEAN LUC; TAMI LIZUZU, JOSEPH TOUSSAINT; HERB, VINCENT MARC; GUERCHE, DIDIER MAURICE MARCEAU; BOHLI, RAMZI
To: SAFRAN; SAFRAN AIRCRAFT ENGINES
Reel/Frame 048342/0659 →
Priority Claims (1)
FR 16 57229 · Jul 27, 2016 · national
Continuity (1)
Related Publication 20190160524A1 · May 30, 2019