inspeÇço radiogrÁfica digital de alta velocidade para fuselagens de aeronaves

A system (10) and method for radiographic inspection of aircraft fuselage (12)s includes a radiation source (28) preferably located inside of the fuselage (12) and a radiation detector (32) preferably located outside of the fuselage (12). A source positioning system (30) is provided for moving the r...

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Bibliographische Detailangaben
Hauptverfasser:	THOMAS JAMES BATZINGER, DENNIS MICHAEL WALSH, GREGORY ALAN MOHR, CLIFFORD BUENO, KENNETH GORDON HERD
Format:	Patent
Sprache:	por
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	A system (10) and method for radiographic inspection of aircraft fuselage (12)s includes a radiation source (28) preferably located inside of the fuselage (12) and a radiation detector (32) preferably located outside of the fuselage (12). A source positioning system (30) is provided for moving the radiation source (28) longitudinally with respect to the fuselage (12), and a detector positioning system (34) is provided for positioning the radiation detector (32) in longitudinal alignment with the radiation source (28). The detector positioning system (34) also moves the radiation detector (32) circumferentially with respect to the fuselage (12). In operation, the radiation detector (32) is moved over the fuselage (12) in a circumferential direction while the radiation source (28) illuminates an adjacent region of the fuselage (12) with radiation.