公开(公告)号：US08876039B2

公开(公告)日：2014-11-04

申请号：US13462422

申请日：2012-05-02

Applicant: Jacob G. Lubenow ,  Andrew S. McComas ,  Jeremy A. Zanzig ,  Jeffrey A. Gerhart ,  Alan R. Klug ,  Jonathan P. Clark

Inventor： Jacob G. Lubenow ,  Andrew S. McComas ,  Jeremy A. Zanzig ,  Jeffrey A. Gerhart ,  Alan R. Klug ,  Jonathan P. Clark

IPC: B64C3/56

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/102

Abstract: A folding wing for an aircraft comprises first and second inboard wing sections, and first and second outboard wing sections. The first and second inboard wing sections rotate about a centerline hinge, and a centerline spring applies force to the first and second inboard wing sections to rotate the first and second inboard wing sections from a stowed position to a deployed position. At least one of the first and second inboard wing sections translates along the axis of rotation of the first and second inboard wing sections as they move from the stowed to the deployed positions. The first and second outboard wing sections rotate between the stowed and the deployed positions about first and second outboard hinges.

Abstract translation: 用于飞机的折翼包括第一和第二内侧翼部，以及第一和第二外侧翼部。 第一和第二内侧翼部围绕中心线铰链旋转，并且中心线弹簧对第一和第二内侧翼部施加力，以将第一和第二内侧翼部从收起位置旋转到展开位置。 第一和第二内侧翼部分中的至少一个在它们从收起的位置移动到展开位置时沿着第一和第二内侧翼部的旋转轴线平移。 第一和第二外侧翼部分围绕第一和第二外侧铰链在收起和展开位置之间旋转。

公开(公告)号：US20120280080A1

公开(公告)日：2012-11-08

申请号：US13462422

申请日：2012-05-02

Applicant: Jacob G. LUBENOW ,  Andrew S. McComas ,  Jeremy A. Zanzig ,  Jeffrey A. Gerhart ,  Alan R. Klug ,  Jonathan P. Clark

Inventor： Jacob G. LUBENOW ,  Andrew S. McComas ,  Jeremy A. Zanzig ,  Jeffrey A. Gerhart ,  Alan R. Klug ,  Jonathan P. Clark

IPC: B64C3/56

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/102

Abstract: A folding wing for an aircraft comprises first and second inboard wing sections, and first and second outboard wing sections. The first and second inboard wing sections rotate about a centerline hinge, and a centerline spring applies force to the first and second inboard wing sections to rotate the first and second inboard wing sections from a stowed position to a deployed position. At least one of the first and second inboard wing sections translates along the axis of rotation of the first and second inboard wing sections as they move from the stowed to the deployed positions. The first and second outboard wing sections rotate between the stowed and the deployed positions about first and second outboard hinges.

Abstract translation: 用于飞机的折翼包括第一和第二内侧翼部，以及第一和第二外侧翼部。 第一和第二内侧翼部围绕中心线铰链旋转，并且中心线弹簧对第一和第二内侧翼部施加力，以将第一和第二内侧翼部从收起位置旋转到展开位置。 第一和第二内侧翼部分中的至少一个在它们从收起的位置移动到展开位置时沿着第一和第二内侧翼部的旋转轴线平移。 第一和第二外侧翼部分围绕第一和第二外侧铰链在收起和展开位置之间旋转。