Tool and method for mounting pulsating pressure sensor on aircraft skin

The invention provides a tool and method for installing a pulsating pressure sensor on an aircraft skin, and the tool comprises an installation block, the right side of the installation block is sleeved with a limiting ring in an engaged manner, one side of the limiting ring is provided with a wire...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LYU ANBO, GAO TIANSHENG, HUO XINCHEN, WANG DI, WU PENG
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The invention provides a tool and method for installing a pulsating pressure sensor on an aircraft skin, and the tool comprises an installation block, the right side of the installation block is sleeved with a limiting ring in an engaged manner, one side of the limiting ring is provided with a wire arrangement groove, the limiting ring is sleeved with a pressing ring, the right side surface of the pressing ring is provided with an outer double-faced adhesive tape ring, and the two sides of the pressing ring are provided with guide rods. The left end of the guide rod is connected with a pressing plate, the guide rod is sleeved with a pressure spring, the pressure spring is located between the installation block and the pressing plate, a sliding rod penetrates through the middle of the pressing plate and the middle of the installation block, a pressing head is fixed to the outer end of the sliding rod, a connecting plate is installed on the sliding rod, and the sliding rod is sleeved with a reset spring. The re