LOCKPIN CONNECTION AND METHOD

An actuator arrangement includes an actuator screwshaft (420) configured to receive a female connector (220), a lockpin (200) having a male connector (210) that is connected to the female connector (200). When the actuator screwshaft (420) is rotated, in use, the lockpin (200) is configured to move...

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Bibliographische Detailangaben
Hauptverfasser:	TIMMS, Mark David, BUTRIMAVICIUS, Karolis, SMITH, Paul
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ENGINEERING ELEMENTS AND UNITS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An actuator arrangement includes an actuator screwshaft (420) configured to receive a female connector (220), a lockpin (200) having a male connector (210) that is connected to the female connector (200). When the actuator screwshaft (420) is rotated, in use, the lockpin (200) is configured to move from a first position to a second position.