Static pressure hole airtight clamp assembly

A static pressure hole airtight clamp assembly used for connecting a static pressure hole and airtight testing equipment comprises a base comprising a hollow shell, the first end of the base covers the static pressure hole, and the second end opposite to the first end is connected with a supporting...

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Bibliographische Detailangaben
Hauptverfasser:	XU BIN, ZHAO XINRAN, YUAN WENDUO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING CYLINDERS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HAND TOOLS HEATING LIGHTING MANIPULATORS MEASURING MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICS PISTONS PORTABLE POWER-DRIVEN TOOLS SEALINGS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR THERMAL INSULATION IN GENERAL TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A static pressure hole airtight clamp assembly used for connecting a static pressure hole and airtight testing equipment comprises a base comprising a hollow shell, the first end of the base covers the static pressure hole, and the second end opposite to the first end is connected with a supporting column device; a strut device connected at a first end thereof to the base, and connected at a second end thereof, opposite the first end, to an air tightness test device; the connecting rod is transversely connected to the supporting column device and can move along the supporting column device; the length of the connecting rod is adjustable; two ends of the connecting rod are connected with fixing pieces; the fixing piece comprises a rod part, and the rod part is connected to the connecting rod; the connecting part comprises a first connector part and a second connector part, the first connector part is combined to the rod part, the second connector part is fixed to the aircraft, and the first connector part and