System and method for positioning error compensation during manufacturing of complex-shaped gas turbine engine parts
AssigneePratt & Whitney Canada Corp.
InventorsYuwen LI, Amr ELFIZY
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AssigneePratt & Whitney Canada Corp.
InventorsYuwen LI, Amr ELFIZY
Estimating the term…
A system and method for error compensation in positioning a complex-shaped gas turbine engine part during manufacturing thereof with a machine. Theoretical measurements for a plurality of control points on the part are first retrieved. Actual measurements for the control points are then acquired in a coordinate system of the machine. If an error between the actual and theoretical measurements is beyond a tolerance, a transformation matrix is computed. The transformation matrix represents a transformation to be applied to the coordinate system to adjust a pose thereof for compensating the error. The transformation matrix may be computed and applied to the coordinate system iteratively until the actual measurements are brought within tolerance. A machining program may then be generated for manufacturing the part accordingly.
A method for positioning error compensation during manufacturing of a complex-shaped gas turbine engine part with a machine, the method comprising:
A system for positioning error compensation during manufacturing of a complex-shaped gas turbine engine part with a machine, the system comprising:
A system for positioning error compensation during manufacturing of a complex-shaped gas turbine engine part with a machine, the system comprising:
Dependencies are inferred from the claim text.