An aircraft sensor includes a housing (12), a strut (14) connected to and extending from a top of the housing (12), and a probe (16) extending from the strut (14). The strut (14) includes a flange (18) extending radially outward from a bottom portion of the strut (14) and a body (20) extending from a top of the flange (18). The strut (14) also includes a bore (24) extending into the strut body (20) and having a closed end positioned in the body (20). The strut (14) also includes a vent shaft (28) fluidly connected to the bore (24) and including an outlet.
AIRCRAFT SENSOR WITH VENTED BORES IN A STRUT
FLUGZEUGSENSOR MIT BELÜFTETEN BOHRUNGEN IN EINER STREBE
CAPTEUR D'AVION AVEC DES ORIFICES VENTILÉS DANS UNE ENTRETOISE
02.04.2025
Patent
Elektronische Ressource
Englisch
IPC: | G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G01K MEASURING TEMPERATURE , Messen der Temperatur |