Loading of aircraft landing gear

A method of loading a landing gear in an aircraft comprises accessing an ideal path specifying movement of the landing gear from a starting location to an expected mounting location on the aircraft; determining a difference between the expected mounting location and an actual mounting location on th...

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Bibliographische Detailangaben
Hauptverfasser:	DesJardien Matthew R, Van Horne Brian, Kremenich Allan M, Al Aqrabawi Zeyad A, Nelson Blair P
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION CALCULATING COMPUTING CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS COUNTING DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTRIC DIGITAL DATA PROCESSING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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Beschreibung
Zusammenfassung:	A method of loading a landing gear in an aircraft comprises accessing an ideal path specifying movement of the landing gear from a starting location to an expected mounting location on the aircraft; determining a difference between the expected mounting location and an actual mounting location on the aircraft; modifying the ideal path to move the expected mounting location to the actual mounting location; and moving the landing gear along the modified path.