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    • 5. 发明授权
    • Wing skin and method of manufacture thereof
    • 翼皮及其制造方法
    • US07195203B2
    • 2007-03-27
    • US10509149
    • 2003-03-25
    • Mark LivingstoneDarren CrewStephen Bell
    • Mark LivingstoneDarren CrewStephen Bell
    • B64C1/00
    • B64C3/26B64F5/00
    • A simplified structure for a wing skin and wing box wherein the internal surface (2) of an aircraft wing skin panel (1) in the wing box includes a multiplicity of strips (3), each strip being associated with a stringer. The strips (3) have different gradients in the span-wise direction S, which is the direction in which the strips extend. The surface of each strip is, in the chord-wise direction C, parallel to the external surface (5). At a junction, at which a rib meets a stringer, the interior surface (2) has an area (4a) that is parallel to the exterior surface (5), such that the rib and stringer at that junction may be simply attached to the wing skin panel (1).
    • 机翼皮肤和翼盒的简化结构,其中翼盒中的飞机机翼皮肤面板(1)的内表面(2)包括多个条带(3),每个条带与桁条相关联。 带(3)在跨度方向S上具有不同的梯度,这是带延伸的方向。 每个条带的表面在弦方向C上平行于外表面(5)。 在肋条与桁条相交的连接部处,内表面(2)具有平行于外表面(5)的区域(4a),使得该结处的肋条和桁条可以简单地附接到 翼面板(1)。
    • 6. 发明申请
    • Wing skin and method of manufacture thereof
    • 翼皮及其制造方法
    • US20050224652A1
    • 2005-10-13
    • US10509149
    • 2003-03-25
    • Mark LivingstoneDarren CrewStephen Bell
    • Mark LivingstoneDarren CrewStephen Bell
    • B64C3/26B64F5/00B64C1/00
    • B64C3/26B64F5/00
    • The internal surface (2) of an aircraft wing skin panel (1) in the wing box comprises a multiplicity of strips (3), each strip being associated with a stringer. The strips (3) have different gradients in the span-wise direction S, which is the direction in which the strips extend. The surface of each strip is, in the chord-wise direction C, parallel to the external surface (5). At a junction, at which a rib meets a stringer, the interior surface (2) has an area (4a) that is parallel to the exterior surface (5), such that the rib and stringer at that junction may be simply attached to the wing skin panel (1). Manufacture and design of wing skins and wing boxes may be greatly simplified by means of defining the interior surface with such strips.
    • 机翼箱中的飞机机翼皮肤面板(1)的内表面(2)包括多个条带(3),每个条带与桁条相关联。 带(3)在跨度方向S上具有不同的梯度,这是带延伸的方向。 每个条带的表面在弦方向C上平行于外表面(5)。 在肋条与桁条相交的连接部处,内表面(2)具有平行于外表面(5)的区域(4a),使得该结处的肋条和桁条可以简单地附接到 翼面板(1)。 通过用这样的条限定内表面,可以大大简化机翼表皮和翼盒的制造和设计。