The present invention is a self-disengaging pitot tube cover having a split cylinder configuration and an internal release mechanism, which is triggered by a temperature sensitive mechanism upon detecting a predetermined temperature so that the pitot tube cover separates and is released from the pitot tube at a predetermined temperature.
System for ensuring failsafe operation of pitot tube covers for multiple types of pitot tubes
2024-04-09
Patent
Electronic Resource
English
IPC: | G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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