Force loading device, static heat experiment testing system and static heat experiment testing method

The invention provides a force loading device and a static heat experiment test system and method.The force loading device comprises an adapter, one end of the adapter is provided with a first groove, the bottom center of the first groove is provided with a second groove, the bottom edge of the firs...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	LIU PUCHEN, SUN YONG, ZHANG YUNBO, XING FEI, MA LUJUN
Format:	Patent
Sprache:	chi ; 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 INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention provides a force loading device and a static heat experiment test system and method.The force loading device comprises an adapter, one end of the adapter is provided with a first groove, the bottom center of the first groove is provided with a second groove, the bottom edge of the first groove is provided with a third groove, the side wall of the adapter is provided with a liquid inlet hole and a liquid outlet hole, the liquid inlet hole is communicated with the bottom of the second groove, and the liquid outlet hole is communicated with the bottom of the third groove; the liquid outlet hole is communicated with the bottom of the third groove; one end of the liquid cooling outer pipe is matched and communicated with the first groove; the liquid-cooling inner pipe is arranged in the liquid-cooling outer pipe, and one end of the liquid-cooling inner pipe is matched and communicated with the second groove; one end of the force loading pipe is matched and communicated with the liquid cooling outer p