Method for forming shaped passages

• US 5,418,345 A
• Filed: 02/28/1994
• Issued: 05/23/1995
• Est. Priority Date: 02/28/1994
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Adamski, Edward G.
• Primary Examiner(s): Evans, Geoffrey S.
• Application Number:
  US08/203,071
• Time in Patent Office: 449 Days
• Field of Search: 204/129.55, 204/224 M, 29/564, 29/56.5, 29/56.6, 29/33 P, 219/69.17, 219/69.2, 219/69.16, 219/121.7, 219/121.71, 219/121.82, 364/474.34, 364/474.35, 364/474.36, 364/474.04, 364/474.08, 408/1 R, 408/13
• US Class Current: 219/69.17
• CPC Class Codes: B23H 11/003 Mounting of workpieces, e.g. working-tables
• CPC Class Codes: B23H 9/10 Working turbine blades or nozzles
• CPC Class Codes: B23K 26/384 of specially shaped holes
• CPC Class Codes: Y10T 29/5136 Separate tool stations for selective or successive operation on work

Abstract

A two step operation passage forming process includes steps to minize tolerance build up between the operations. The method includes a step of determining a spatial error between the coordinate systems of the two operations. In a particular embodiment, the step of determining the spatial error includes forming an indexing hole in a template at a particular location using the first operation, aligning the apparatus of the second operation with the indexing hole, and measuring the spatial error between the actual position of the indexing hole and a translated position. The determined spatial error may then be used as an offset in the second operation to account for tolerance differences between the two operations.

Claims

1. A method to form a plurality of passages in an article, each of the plurality of passages having a first portion and a second portion in flow communication, the first portion formed by a first passage forming means having a first coordinate system, the second portion formed by a second passage forming means having a second coordinate system, each of the plurality of passages having a predetermined spatial position defining a position P1_p within the first coordinate system, a position P2_p within the second coordinate system, and wherein the plurality of passages define a spatial envelope, the method including the steps of:

forming an indexing hole in a plate, the indexing hole being formed by the first passage forming means and at a position P1_i within the first coordinate system, the position P1_i being within the spatial envelope of the plurality of passages;

placing the plate within the second passage forming means and aligning the second passage forming means with the indexing hole;

determining the spatial error E_p between the actual position P2_i of the indexing hole relative to a position P2_i,t, wherein P2_i,t corresponds to a translation of the coordinate P1_i from the first coordinate system into the second coordinate system;

forming the first portions at the positions P1_p using the first passage forming means; and

forming the second portions at positions P2_c using the second passage forming means, wherein the positions P2_c correspond to positions P2_p +E_p.

2. The method according to claim 1, wherein the first passage forming means is laser apparatus and the second passage forming means is an electric discharge machining apparatus, wherein the step of forming the first portions includes laser drilling the first portions, and wherein the step of forming the second portions includes electric discharge machining the second portions.

3. The method according to claim 1, wherein the first passage forming means is electric discharge machining apparatus and the second passage forming means is an electric discharge machining apparatus, wherein the step of forming the first portions includes electric discharge machining the first portions, and wherein the step of forming the second portions includes electric discharge machining the second portions.

4. The method according to claim 1, wherein the plurality of passages define multiple envelopes, and wherein the step of forming an index hole includes forming a plurality of index holes, at least one within each spatial envelope.

5. The method according to claim 1, wherein the step of forming the indexing hole includes selecting a position for the indexing hole that corresponds to the position of one of the plurality of passages.

6. The method according to claim 1, wherein the second passage forming means includes an electrical circuit extending between the second passage forming means and the template, the electrical circuit having a power source and a signaling device, wherein the step of determining the spatial error E_p includes performing a continuity test to determine accurate location of index hole within second coordinate system.

7. The method according to claim 1, wherein the second passage forming means is an electric discharge machining apparatus and includes an electrode having an extension sized to fit within the indexing hole, and wherein the step of determining the spatial error E_p includes a step of inserting the extension within the indexing hole such that the extension does not touch the surface of the indexing hole.

8. The method according to claim 1, wherein the article is a turbine component and the passages are cooling passages, and wherein the step of forming the first portion includes a step of forming a cooling passage within the turbine component.

9. The method according to claim 8, wherein the turbine component includes an airfoil portion, and wherein the step of forming a first portion includes the step of forming a cooling passage that extends through the airfoil portion.

10. The method according to claim 8, wherein the turbine component includes a platform, and wherein the step of forming a first portion includes the step of forming a cooling passage that extends through the platform.

11. The method according to claim 1, wherein the passages are shaped passages having a metering section and a diffusing section, wherein the step of forming the first portion includes a step of forming the metering section, and wherein the step of forming the second section includes the step of forming the diffusing section.

12. The method according to claim 8, wherein the cooling passages are shaped passages having a metering section and a diffusing section, wherein the step of forming the first portion includes a step of forming the metering section, and wherein the step of forming the second section includes the step of forming the diffusing section.

13. The method according to claim 6, wherein the plurality of passages have a planar position with a range of values and an angle with a range of values relative to a predetermined reference, and wherein the step of forming an indexing hole includes selecting a passage having an angle that is the median of the range of values of the angle.

14. The method according to claim 6, wherein the plurality of passages have a planar position with a range of values and an angle with a range of values relative to a predetermined reference, and wherein the step of forming an indexing hole includes selecting a passage having a planar position that is the median of the range of planar positions.