Method for producing profiled parts by grinding and a turbomachine blade produced thereby

• US 5,330,326 A
• Filed: 01/29/1993
• Issued: 07/19/1994
• Est. Priority Date: 05/04/1987
• Status: Expired due to Fees

• Current Assignee: Ulrich Kuehne
• Original Assignee: Ulrich Kuehne
• Inventors: Meyer, Klaus, Heine, Karlheinz, Rueschmann, Klaus, Kuehne, Ulrich
• Primary Examiner(s): Rose, Robert A.
• Application Number:
  US08/011,217
• Time in Patent Office: 536 Days
• Field of Search: 51/281 R, 51/327, 51/144, 29/889.2, 29/889, 416/223 R, 416/248
• US Class Current: 416/248
• CPC Class Codes: B24B 19/14 for grinding turbine blades, propeller blades or the like using grinding belts B24B21/16
• CPC Class Codes: B24B 49/00 Measuring or gauging equipment for controlling the feed movement of the grinding tool or work; Arrangements of indicating or measuring equipment, e.g. for indicating the start of the grinding operation B24B33/06, B24B37/005 take precedence; if applicable to other machine tools, B23Q15/00 - B23Q17/00 take precedence
• CPC Class Codes: F05B 2200/31 odd
• CPC Class Codes: Y10T 29/49316 Impeller making

Abstract

A method for producing a profiled part from a blank, wherein the cross-sectional profile of the part to be produced differs in some portions both quantitatively and qualitatively from the cross-sectional profile of the blank, so that different amounts of material must be removed between a starting profile of the blank and a desired final profile of the part includes pre-shaping and finish-grinding the part to be produced in one chucking position with at least one profiled grinding wheel. The blank is translated and rotated relative to the at least one profiled grinding wheel during the pre-shaping step for giving the blank approximately a desired profile. The finish-grinding step is performed at least partially after the pre-shaping step for smoothing surfaces and producing the final profile to accurate dimensions. A turbomachine blade, an intermediate product for the turbomachine blade and a method of manufacturing the interim product are also provided.

Claims

1. Intermediate product for a turbomachine blade, comprising:

a) an elongated metal block having an original cross section and a length of from 5 to 30% greater than the length of the blade to be produced;

b) a suction side contour, a root contour and a top contour of the blade at least partly ground into said metal block, and remaining pieces having the original cross section of the metal block protruding from both said root and said top contours; and

c) said root contour and said top contour having lengthwise dimensions slightly exceeding actual dimensions to be produced.

2. Intermediate product according to claim 1, wherein said elongated metal block has an approximately rectangular cross-section.

3. Intermediate product according to claim 1, wherein said length of said elongated metal block is approximately 20% greater than the length of the blade to be produced.

4. Intermediate product according to claim 1, wherein said lengthwise dimensions of said root contour and said top contour exceed the actual dimensions to be produced by at least the cutting width of a saw or cutting device.

5. Intermediate product according to claim 1, wherein said metal block is formed of steel.

6. Intermediate product according to claim 5, wherein said remaining pieces have a length projecting from said root and top contours by at least 2 mm.

7. Intermediate product according to claim 5, wherein said root and top contours exceed the actual dimensions to be produced by between 0.5 and 4 mm.

8. Intermediate product according to claim 5, wherein said root and top contours exceed the actual dimensions to be produced by approximately 3 mm.

9. Intermediate product according to claim 5, wherein the leading and trailing edges have a connecting plane therebetween, and including a pressure side contour preground at least as far as said connecting plane.

10. Intermediate product according to claim 1, wherein said elongated metal block has a parallelogram cross-section.