An aircraft wing 101 or tail arrangement (figure 8) is provided comprising an aircraft wing tip portion T or tail fin (T, figure 8), and one or more outlets 102- 116 for the delivery of anti-icing fluid to a surface of the aircraft wing tip portion or tail fin. The anti-icing system may also be applicable to folding wing tips.
Aircraft wing or tail arrangement
2025-04-09
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |