IP Library › Granted Patent US 8,309,875
Granted Patent B2
US 8,309,875 · App. 12/611,434 · Granted Nov 13, 2012

Apparatus and method for making bores in an edge of a turbine blade

Assignee: Siemens Aktiengesellschaft
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Quick Facts
Patent No.
US 8,309,875
App. No.
12/611,434
Granted
Nov 13, 2012
Kind
B2
Abstract

An apparatus for making bores in a turbine blade edge is provided. The apparatus includes a drilling device and a guide for the drilling device. The guide includes a bearing element with a gap which is delimited by bearing faces and has the shape of a turbine blade edge. Further, the apparatus includes two guide modules which lie opposite one another and are brought to bear with a side face of the turbine blade and which together form a tension device for fixing the guide on the turbine blade. Furthermore, a method for making bores in a turbine blade edge using such an apparatus is provided.

Claims (38)

1. An apparatus for making bores in an edge of a turbine blade, comprising:

a drilling device with a rotating electrode as a drilling tool; and

a guide for the drilling device,

wherein the guide includes

a bearing element, a gap being formed in the bearing element, the gap being delimited by bearing faces and having a contour corresponding to a shape of a turbine blade edge to be machined, and

at least two guide modules lying opposite one another,

wherein the guide modules together form a tension device for fixing the guide on the turbine blade, and

wherein the bearing element of the guide includes a clearance for leading through the rotating electrode.

2. The apparatus as claimed in claim 1 , wherein the guide modules, when forming the tension device for fixing the guide on the turbine blade, bear with a side face of the turbine blade.

3. The apparatus as claimed in claim 1 , wherein the gap in the bearing element is delimited by two bearing prisms.

4. The apparatus as claimed in claim 1 , wherein at least a region of the guide in which the clearance is formed comprises an electrically insulating material.

5. The apparatus as claimed in claim 1 , wherein the clearance is arranged in line with the gap.

6. The apparatus as claimed in claim 4 , wherein the clearance is arranged in line with the gap.

7. The apparatus as claimed in claim 1 , wherein at least one of the guide modules has a cylindrical locating element.

8. The apparatus as claimed in claim 3 , wherein at least one of the guide modules has a cylindrical locating element.

9. The apparatus as claimed in claim 4 , wherein at least one of the guide modules has a cylindrical locating element.

10. The apparatus as claimed in claim 7 , wherein the locating element is fixed and held displaceably on the guide module.

11. The apparatus as claimed in claim 8 , wherein the locating element is fixed and held displaceably on the guide module.

12. The apparatus as claimed in claim 9 , wherein the locating element is fixed and held displaceably on the guide module.

13. The apparatus as claimed in claim 1 , wherein the bearing element is connected releasably and exchangeably to the guide.

14. A method for making bores in a turbine blade edge, comprising:

providing an apparatus, comprising:

a drilling device with a rotating electrode as a drilling tool; and

a guide for the drilling device,

wherein the guide includes

a bearing element, a gap being formed in the bearing element, the gap being delimited by bearing faces and having a contour corresponding to a shape of a turbine blade edge to be machined, and

at least two guide modules lying opposite one another,

wherein the guide modules together form a tension device for fixing the guide on the turbine blade, and

wherein the bearing element of the guide includes a clearance for leading through the rotating electrode;

placing the apparatus onto the turbine blade such that the turbine blade edge to be machined is arranged in a region of the gap of the bearing element,

mounting the turbine blade between the guide modules; and

making bores in the turbine blade edge by the drilling device.

15. The method as claimed in claim 14 , wherein the turbine blade is mounted with tension between the guide modules.

16. The method as claimed in claim 14 , wherein the gap in the bearing element is delimited by two bearing prisms.

17. The method as claimed in claim 14 , wherein at least a region of the guide in which the clearance is formed comprises an electrically insulating material.

18. The method as claimed in claim 14 , wherein the clearance is arranged in line with the gap.

19. The method as claimed in claim 14 , wherein at least one of the guide modules has a cylindrical locating element.

20. The method as claimed in claim 19 , wherein the locating element is fixed and held displaceably on the guide module.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 3, 2009
From: BERGER, INGO; DUNKEL, UWE; RAUE, STEFFI
To: SIEMENS AKTIENGESELLSCHAFT
Reel/Frame 023462/0798 →
Priority Claims (1)
EP 08019280 · Nov 4, 2008 · regional
Continuity (1)
Related Publication 20100108644A1 · May 6, 2010