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United States Patent 6,420,677
Emer ,   et al. July 16, 2002

Laser machining cooling holes in gas turbine components

Abstract

The present invention provides a method of laser machining a cooling hole in a hollow gas turbine component, the cooling hole including a circular cross section metering hole and a diffuser with an opening which extends from a shape locus in the metering hole to a trapezoidal cross section opening by firing a series of laser pulses at an acute angle at the outer surface of the component toward the shape locus to create the diffuser opening, with the laser pulses penetrating the component outer surface up to but not substantially beyond the shape locus, then firing the laser through the shape locus and the inner surface of the component to create the metering hole having a circular cross section. Alternatively, the initial laser pulses are fired to create the central portion of the diffuser opening, then firing the laser to create the metering hole, followed by firing the laser along the peripheral portion of the diffuser opening.


Inventors: Emer; George (Cresskill, NJ); Wos; Frank (Landing, NJ); Romin; Dmitriy (Brooklyn, NY)
Assignee: Chromalloy Gas Turbine Corporation (Orangeburg, NY)
Appl. No.: 741727
Filed: December 20, 2000

Current U.S. Class: 219/121.71; 219/121.72; 219/121.67; 219/121.7; 219/121.68
Intern'l Class: B23K 026/00
Field of Search: 219/121.71,121.72,121.67,121.7,121.68


References Cited

U.S. Patent Documents
4737613Apr., 1988Frye219/121.
4762464Aug., 1988Vertz et al.416/97.
5223692Jun., 1993Lozier et al.219/121.
5609779Mar., 1997Crow et al.219/121.
5683600Nov., 1997Kelley et al.219/121.
5739502Apr., 1998Anderson et al.219/121.
5837964Nov., 1998Emer et al.219/121.
6307175Oct., 2001Blochinger et al.219/121.
Foreign Patent Documents
0365195Mar., 1996EP.
0748469Oct., 1997EP.

Primary Examiner: Elve; M. Alexandra
Attorney, Agent or Firm: Bittman; Mitchell D.

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