A FLEXIBLE KINEMATICS ELEMENT WITH INPUT-OUTPUT LINEARIZATION

The present embodiments relate to a rotorcraft 100, and, more particularly, to an apparatus for transmitting a mechanical control signal in a rotorcraft 100 from a point of introduction to a point of application. The apparatus may include a flexible kinematics element 200, 405, a control signal tran...

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Bibliographische Detailangaben
Hauptverfasser:	Schmid, Emanuel, Steger, Justus, Schweighöfer, Peter
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BEARINGS BLASTING COSMONAUTICS ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The present embodiments relate to a rotorcraft 100, and, more particularly, to an apparatus for transmitting a mechanical control signal in a rotorcraft 100 from a point of introduction to a point of application. The apparatus may include a flexible kinematics element 200, 405, a control signal transmitter 406, 407, 408, and an interface element 430 that is coupled between a linear control signal conveyor 201 of the flexible kinematics element 200, 405 and the control signal transmitter 406, 407, 408. The interface element 430 may linearize a motion associated with the mechanical control signal at the input and/or output interface of the linear control signal conveyor 201 of the flexible kinematics element 200, 405.