An aircraft sensor includes a housing, a strut connected to and extending from a top of the housing, and a probe extending from the strut. The strut includes a flange extending radially outward from a bottom portion of the strut and a body extending from a top of the flange. The strut also includes a bore extending into the strut body and having a closed end positioned in the body. The strut also includes a vent shaft fluidly connected to the bore and including an outlet.
AIRCRAFT SENSOR WITH VENTED BORES IN A STRUT
27.03.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |