Stringers and aircraft skin structures and related methods are disclosed. An example apparatus includes a skin structure and a support. The support includes a first surface, a second surface opposite the first surface, and a tapered edge extending from the first surface. The example apparatus includes a first material disposed between a first portion of the support and a first portion of the skin structure to couple the second surface of the support to the skin structure and a second material disposed between a second portion of the support and a second portion of the skin structure. The second material is different than the first material. The second portion of the support includes at least a portion of the tapered edge.
STRINGERS FOR AIRCRAFT SKIN STRUCTURES AND RELATED METHODS
2021-03-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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