NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Control apparatusAlthough the method and apparatus of the present invention can be utilized to apply either a uniform or a nonuniform covering of material over many different workpieces, the apparatus (20) is advantageously utilized to apply a thermal barrier covering (64) to an airfoil (22) which is used in a turbine engine. The airfoil is held by a gripper assembly (86) while a spray gun (24) is effective to apply the covering over the airfoil. When a portion of the covering has been applied, a sensor (28) is utilized to detect the thickness of the covering. A control apparatus (32) compares the thickness of the covering of material which has been applied with the desired thickness and is subsequently effective to regulate the operation of the spray gun to adaptively apply a covering of a desired thickness with an accuracy of at least plus or minus 0.0015 inches (1.5 mils) despite unanticipated process variations.
Document ID
20080004209
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Derkacs, Thomas
Fetheroff, Charles W.
Matay, Istvan M.
Toth, Istvan J.
Date Acquired
August 24, 2013
Publication Date
November 9, 1982
Subject Category
Chemistry And Materials (General)
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-238213
Patent Number: US-PATENT-4,358,471
Funding Number(s)
CONTRACT_GRANT: NAS3-20112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,358,471
Patent Application
US-PATENT-APPL-SN-238213
No Preview Available