US5047966A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Airfoil measurement method
Assignee: TURBINE ENGINE COMPONENTS TECHNOLOGIES Corp
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Filing: 1989-05-22
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Granted: 1991-09-10
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Expires: 2009-05-22
Abstract
Abstract A coordinate measuring machine is used to extract data points from an airfoil surface. The machine is controlled to move a probe to desired points by a generic program applicable to any airfoil and a nominal data file specific to the type of airfoil being measured containing coordinates of desired data points, surface normal vectors and optional machine control instructions arranged in the order of usage. The program reads the data file and predicts the location of corresponding data points on the surface from the file data and deviation information available from already-sampled data points on the blade. An analysis program accepts the data points, mathematically reconstructs portions of the airfoil and measures dimensions from those portions. The dimensions are compared to tolerances read from another file specific to the airfoil type.
Inventors
- 👤 Kevin H. Crow
- 👤 Melvin L. Morris
- 👤 William F. Derouchie
- 👤 Dan W. Prevost
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 08:12
CPC Classifications
G; G05; G05B; G05B19/00; G05B19/02; G05B19/18; G05B19/401; G05B2219/00; G05B2219/30; G05B2219/37; G05B2219/37193; G05B2219/37205; G05B2219/37441
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
200 words
The method of measuring an airfoil comprising the steps of: activating a control program for controlling the movement of a measuring machine probe, supplying nominal coordinates of the airfoil to be measured to the control program, moving the probe to the nominal coordinates under program control, acquiring data points on the airfoil corresponding to the nominal coordinates, measuring the airfoil by mathematically reconstructing at least certain portions of the airfoil by interpolation utilizing the data points and determining dimensions from the certain portions, and wherein the control program further compensates for deviations between the nominal and actual coordinate points for movement of the probe and acquisition of data points by the further steps of: determining the length of a nominal chord from the nominal coordinates, for each airfoil section, acquiring data points sufficient to define an actual airfoil chord and calculating the difference of length between the actual airfoil chord and the nominal chord, predicting the position of other data points to be measured from the nominal coordinates and the calculated difference of length, and substituting the predicted data points for the nominal coordinates for the movement of the probe, whereby the efficiency and accuracy of probe movement is enhanced.
Claim 2
Independent Claim
200 words
The method of measuring an airfoil comprising the steps of: activating a control program for controlling the movement of a measuring machine probe, supplying nominal coordinates of the airfoil to be measured to the control program, moving the probe to the nominal coordinates under program control, acquiring data points on the airfoil corresponding to the nominal coordinates, measuring the airfoil by mathematically reconstructing at least certain portions of the airfoil by interpolation utilizing the data points and determining dimensions from the certain portions, and wherein the control program further compensates for deviations between the nominal and actual coordinate points for movement of the probe and acquisition of data points by the further steps of: determining the length of a nominal chord from the nominal coordinates, for each airfoil section, acquiring data points sufficient to define an actual airfoil chord and calculating the difference of length between the actual airfoil chord and the nominal chord, predicting the position of other data points to be measured from the nominal coordinates and the calculated difference of length, and substituting the predicted data points for the nominal coordinates for the movement of the probe, whereby the efficiency and accuracy of probe movement is enhanced.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-09-09 | 1995-03-11 | 1995-09-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-09-09 | 1999-03-11 | 1999-09-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-09-09 | 2003-03-11 | 2003-09-10 | $7700.00 | Window Closed / Lapsed |