Laminate composite wing structures

The application discloses laminate composite wing structures. A wing may include a wing skin, a laminate composite first stringer, a rib, and at least one fastener. A majority of the first stringer may be characterized by a stacked plurality of generally planar plies of reinforcement material struct...

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Bibliographic Details
Main Authors DOWNEY TYLER W, SAMPEDRO-THOMPSON WILLIAM M, CHOY WENDELL C K, ROACHE RYAN CHRISTOPHER, CHARLES JORDAN, GAMBLE MICHAEL JOHN, SANTINI GREGORY M, WATKINS JESSICA L
Format Patent
LanguageChinese
English
Published 27.07.2016
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The application discloses laminate composite wing structures. A wing may include a wing skin, a laminate composite first stringer, a rib, and at least one fastener. A majority of the first stringer may be characterized by a stacked plurality of generally planar plies of reinforcement material structurally joined as a stack to an interior surface of the wing skin and extending generally parallel to the interior surface and a span-wise direction of the wing along a substantial portion of the interior surface. The first stringer may have a generally solid trapezoidal cross section when viewed in a plane that is generally perpendicular to the span-wise direction. The rib may be positioned adjacent the interior surface, and may extend generally perpendicular to the span-wise direction. The trapezoidal cross section may be interfaced with the rib flange. The fastener may extend through the wing skin, the trapezoidal cross section, and the rib flange. 本申请公开了层压复合材料机翼结构。种机翼可包括：机翼蒙皮、层压复合材料的第桁条、翼肋和至少个紧固件。第桁条的大部分具有层叠的多个大
Bibliography:Application Number: CN201511031003