Time-varying non-linear clamping method with high flexibility

The invention provides a time-varying non-linear clamping method with high flexibility. A processing region or processing characteristics can be changed, and the positions and the number of positioning points present dynamic changes along with the changes of a milling region or milling characteristi...

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Bibliographische Detailangaben
Hauptverfasser:	XU MING, PENG YU, XIANG BINGFEI, ZHU XIAOJUN, ZHOU ZAOWEN, MENG ZHILING, WANG JIANJUN, XIONG YONG, LI XIANG, HUANG HONGBIN, HUANG JING
Format:	Patent
Sprache:	eng
Schlagworte:	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 PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention provides a time-varying non-linear clamping method with high flexibility. A processing region or processing characteristics can be changed, and the positions and the number of positioning points present dynamic changes along with the changes of a milling region or milling characteristics. In order to realize the purpose of accurate quick automatic positioning and steady clamping of a wainscot workpiece, the invention provides a flexible solution method, so that accurate manufacture and integrated processing under the condition of clamping at a time can be realized, a processing benchmark does not need to be exchanged, the processing accuracy is ensured, and the processing deformation of a wainscot can be effectively controlled.