SYSTEMS AND METHODS TO VERIFY MAIN ROTOR SWASHPLATE POSITIONING

A device (100, 200) to verify main rotor swashplate (300) positioning includes an inner surface (112, 212) of a first section (110, 210) and a gradient surface (150, 250) of a second section (120, 220). The gradient surface (150, 250) of the second section (120, 220) may have a plurality of graduati...

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Bibliographische Detailangaben
Hauptverfasser:	LINTON, Bradley D, HAUGEBERG, Chad R
Format:	Patent
Sprache:	eng ; fre ; ger
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 PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A device (100, 200) to verify main rotor swashplate (300) positioning includes an inner surface (112, 212) of a first section (110, 210) and a gradient surface (150, 250) of a second section (120, 220). The gradient surface (150, 250) of the second section (120, 220) may have a plurality of graduation indications (151, 251). In one implementation, the inner surface (112, 212) of the first section (110, 210) at least partially defines a travel arc (107) that is parallel to and concentric with the inner surface (112, 212). In such an implementation, the device (100, 200) may be configured to move along the travel arc (107) as it rotates about a collective sleeve (510) to contact a swashplate lug (322).