Device and method for regulating aircraft control surfaces

This describes an aircraft control surface regulating device, comprising an elongated structural body formed of a base positioned at a first end and fixed to the structure of the aircraft and a regulation assembly arranged at a second end and positioned next to the control surfaces, the regulation a...

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Bibliographische Detailangaben
Hauptverfasser:	Cruz, Marcos Roberto, Bastos Telles Nunes, Luis Augusto, Candia De Miranda, Pedro, Almendanha, Juliano Batista, Ramos, Débora Saraiva, Rodrigues De Oliveira, Adir, Costa Dos Santos, Gilberto Silva, Pinto, Maurilio Augusto
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES 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 HELICOPTERS MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	This describes an aircraft control surface regulating device, comprising an elongated structural body formed of a base positioned at a first end and fixed to the structure of the aircraft and a regulation assembly arranged at a second end and positioned next to the control surfaces, the regulation assembly comprising at least one dial indicator positionable between a first measuring position and a second positioning position and at least one reference ruler arranged adjacent to at least one dial indicator and positionable between an initial position and a final position.A method is also described for regulating aircraft control surfaces, comprising the steps of:(i) fixing a regulating device on an extrados coating of the wing of the aircraft, said regulating device comprising a regulation assembly formed of at least one dial indicator and at least one reference ruler;(ii) measuring the dial indicator in a first measuring position determining a zero position of the indicator and positioning the reference ruler in an initial position determining a zero position of the ruler;(iii) positioning the reference ruler in a final position and positioning the dial indicator in second positioning position to perform the positioning of the control surface regulated in relation to the wing of the aircraft.