An assembly for an aircraft propulsion system includes a first lip segment and a second lip segment. The first lip segment includes a first lip skin, a first mount and a first electric heater. The first mount is disposed at a first side of the first lip segment and connected to the first lip skin. The first electric heater is disposed at the first side of the first lip segment and integrated with the first lip skin. The second lip segment includes a second lip skin, a second mount and a second electric heater. The second mount is disposed at a second side of the second lip segment and connected to the second lip skin. The second mount is removably attached to the first mount. The second electric heater is disposed at the second side of the second lip segment and integrated with the second lip skin.
SEGMENTED NACELLE INLET LIP WITH ELECTRIC THERMAL ANTI-ICING SYSTEM
07.11.2024
Patent
Elektronische Ressource
Englisch
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