FIELD: aviation.
SUBSTANCE: system of protection of load bearing composite elements contains external and internal skins, intermediate layer of protective filler. Between external and internal skins a primary protective layer is provisioned, which contacts the external surface of the protected airframe load bearing element - ribs of a netlike framework made of unidirectional composite material which is located between internal and external skins.
EFFECT: ensuring long-term durability of netlike frameworks at minimum weight costs with allowance for the requirements of shock durability and resistance to degradation of properties under the action of climatic factors.
2 dwg
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Authors
Dates
2015-08-10—Published
2014-06-27—Filed