Aircraft nacelles having adjustable chines are described. An example apparatus includes a multi-segment chine coupled to a nacelle. The multi-segment chine includes a first segment oriented along a fore-aft direction. The first segment is translatable relative to the nacelle along the fore-aft direction. The multi-segment chine further includes a second segment oriented along the fore-aft direction. The second segment is substantially coplanar with the first segment.
AIRCRAFT NACELLES HAVING ADJUSTABLE CHINES
2020-11-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |