WING AND WING DESIGN METHOD
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United States of America Patent
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Issued Date -
Sep 24, 2020
app pub date -
Sep 10, 2018
filing date -
Oct 10, 2017
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Abstract
A wing used for an aircraft includes a configuration member formed of a composite material. The configuration member is divided into a plurality of regions along a surface thereof. The plurality of regions include a first region formed of the composite material of a high strength type, and a second region formed of the composite material of a high elasticity type having higher rigidity than the high strength type. The first region includes any region closest to a wing end side out of the plurality of regions, and the second region includes a region closest to the wing end side and a trailing edge side out of the plurality of regions.
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