Thermal anti-ice bypass systems for use with aircraft
Abstract:
Thermal anti-icing systems are disclosed. An example anti-icing system includes a housing defining an inner recess, a first support fitting, a second support fitting spaced away from the first support fitting. The housing is positioned between the first support fitting and the second support fitting. The first support fitting, the second support fitting and an outer wall of the housing define a heating chamber that is fluidly separated from the inner recess.
Public/Granted literature
Information query
Patent Agency Ranking
0/0