Title:
VIRTUAL TURBOMACHINE BLADE CONTACT GAP INSPECTION
Document Type and Number:
Japanese Patent JP2017078401
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a computer system and computerized method for virtually inspecting contact gaps of a blade stage of a turbomachine.SOLUTION: The system may include a digitizing device 130 for obtaining a three-dimensional model 132 of a shroud 134 of each blade of the blade stage. A computer system may include at least one module configured to perform the following steps: extracting a geometric location data of a hard face plane of each shroud from the three-dimensional model; generating a three-dimensional virtual rendering of the shrouds of the blade stage on the basis of the geometric location data and known dimensions of the blade stage, the three-dimensional virtual rendering including a rendering of contact gaps between adjacent shrouds; and inspecting the blade stage using the three-dimensional virtual rendering.SELECTED DRAWING: Figure 1
Inventors:
JACOB ANDREW SALM
JAMES RYAN CONNOR
JEFFREY DAVID ERNO
JAMES RYAN CONNOR
JEFFREY DAVID ERNO
Application Number:
JP2016151636A
Publication Date:
April 27, 2017
Filing Date:
August 02, 2016
Export Citation:
Assignee:
GENERAL ELECTRIC CO GE
International Classes:
F01D25/00; F01D5/14; F02C7/00; G06F17/50; G06T19/00
Domestic Patent References:
JPH04218708A | 1992-08-10 | |||
JP2009115091A | 2009-05-28 | |||
JP2006048583A | 2006-02-16 |
Foreign References:
US20140003948A1 | 2014-01-02 | |||
KR20080069306A | 2008-07-28 | |||
US20090123268A1 | 2009-05-14 | |||
WO2014008088A1 | 2014-01-09 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka