Method of positioning a hollow workpiece

Patent metadata

Field	Value
Publication number	US-11135686-B2
Application number	US-201816015916-A
Country	US
Kind code	B2
Filing date	Jun 22, 2018
Priority date	Jun 23, 2017
Publication date	Oct 5, 2021
Grant date	Oct 5, 2021

Abstract

A method is for positioning a hollow workpiece obtained by casting and that enables the workpiece obtained in this way to be machined in accurate manner. The workpiece is obtained by a casting method involving a mold and a sacrificial core inserted inside the mold and serving to form at least one cavity in the workpiece. The workpiece includes surfaces of a first type defined during casting by the surfaces of the mold, and surfaces of a second type defined during casting by the surfaces of the core. A frame of reference for positioning the workpiece is constructed that includes at least three reference points (P1-P3) belonging to surfaces of the second type of the workpiece.

First claim

The invention claimed is:

1. A positioning method for positioning a hollow workpiece on tooling, the positioning method comprising:
obtaining said workpiece by a casting method involving a mold and a sacrificial core inserted inside the mold and serving to form at least one cavity in said workpiece, wherein said workpiece comprises surfaces of a first type defined during casting by surfaces of the mold, and surfaces of a second type defined during casting by surfaces of the core;
after the obtaining said workpiece, constructing a positioning frame of reference for positioning the workpiece on said tooling, said constructing said positioning frame of reference including identifying at least three reference points to place setting members of the tooling on, each of the at least three reference points belonging to the surfaces of the second type of the workpiece;
the method further comprising, after the constructing said positioning frame of reference, putting the workpiece on said tooling, said tooling having as many of said setting members as there are said reference points in the positioning frame of reference, the putting the workpiece on the tooling including directly contacting a respective setting member of the tooling on each of the reference points of the positioning frame of reference of the workpiece.

2. The positioning method according to claim 1 , wherein the positioning frame of reference comprises at least five reference points belonging to the surfaces of the second type of the workpiece.

3. The positioning method according to claim 1 , wherein the positioning frame of reference does not have any reference point belonging to the surfaces of the first type of the workpiece.

4. The positioning method according to claim 1 , wherein each of the reference points of the positioning frame of reference is situated on a surface that is locally plane.

5. The positioning method according to claim 1 , wherein all of the reference points of the frame of reference are situated on final surfaces of the workpiece.

6. The positioning method according to claim 1 , wherein the core defines a wall of the workpiece having at least two faces that are the surfaces of the second type.

7. The positioning method according to claim 6 , wherein a thickness of said wall is less than 1 mm.

8. The positioning method according to claim 1 , wherein the workpiece is a turbine engine blade or vane.

9. A method of machining a hollow workpiece obtained by casting, the method comprising:
performing the positioning method according to claim 1 , wherein said tooling is drilling tooling; and
drilling a hole in an inside wall of the workpiece having at least two faces that are the surfaces of the second type.

10. The positioning method according to claim 1 , wherein the positioning frame of reference comprises six reference points belonging to the surfaces of the second type of the workpiece.

11. The positioning method according to claim 1 , wherein the tooling is configured to cut the workpiece.

12. The positioning method according to claim 1 , wherein at least one of the reference points is positioned at a bottom of a notch formed in a top end of a pressure side wall of the workpiece.

13. The positioning method according to claim 12 , wherein one of the reference points is positioned at a rear edge of the pressure side wall of the workpiece.

14. The positioning method according to claim 1 , wherein all of the reference points where the setting members are placed on the workpiece are separate from a location where the tooling cuts or drills the workpiece.

15. The method according to claim 9 , wherein the putting the workpiece on said tooling occurs before the drilling the hole begins.

Assignees

• Safran Aircraft Engines

Inventors

• Vollebregt Matthieu Jean Luc
• Guerard Coralie Cinthia
• Huchin Patrick Emilien Paul Emile
• Tami Lizuzu Joseph Toussaint

Classifications

• B22C9/043

  Removing the consumable pattern · CPC title

• F05D2230/68

  using auxiliary equipment for lifting or holding · CPC title

• B22C9/064

  Locating means for cores · CPC title

• F05D2240/30

  Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor · CPC title

• F05D2230/21

  by casting · CPC title