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    COMPLIANT PANEL FOR AIRCRAFT
    1.
    发明申请
    COMPLIANT PANEL FOR AIRCRAFT 有权
    用于飞机的合规面板

    公开(公告)号：US20080149769A1

    公开(公告)日：2008-06-26

    申请号：US12042629

    申请日：2008-03-05

    申请人： William J. Koch ,  Donald P. Matheson ,  Barney B. Anderson ,  Jeffrey R. Swada

    发明人： William J. Koch ,  Donald P. Matheson ,  Barney B. Anderson ,  Jeffrey R. Swada

    IPC分类号： B64C1/12

    CPC分类号： B64C1/10 ,  B64C1/062 ,  B64C1/12

    摘要： A pressurized bulkhead or panel for an aircraft includes an energy absorbing skin that deforms in response to an object strike that imparts at least a threshold amount of impact energy to the skin. The skin may be configured as a dome or a lofted panel that is essentially free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristics of the skin. The skin may be formed from a monolithic one-piece material, such as metal of composites, and may include various integrally formed reinforcing features.

    摘要翻译： 用于飞行器的加压隔板或面板包括能量吸收皮肤，其响应于向皮肤施加至少阈值量的冲击能量的物体撞击而变形。 皮肤可以被配置为基本上没有刚性加强件和不可变形的加强件的圆顶或顶部面板，否则会妨碍皮肤的柔性特性。 皮肤可以由单片整体材料形成，例如复合材料的金属，并且可以包括各种整体形成的增强特征。

    Compliant panel for aircraft
    2.
    发明授权
    Compliant panel for aircraft 有权
    飞机合规板

    公开(公告)号：US07997529B2

    公开(公告)日：2011-08-16

    申请号：US12042629

    申请日：2008-03-05

    申请人： William J. Koch ,  Donald P. Matheson ,  Barney B. Anderson ,  Jeffrey R. Swada

    发明人： William J. Koch ,  Donald P. Matheson ,  Barney B. Anderson ,  Jeffrey R. Swada

    IPC分类号： B64C7/00

    CPC分类号： B64C1/10 ,  B64C1/062 ,  B64C1/12

    摘要： A pressurized bulkhead or panel for an aircraft includes an energy absorbing skin that deforms in response to an object strike that imparts at least a threshold amount of impact energy to the skin. The skin may be configured as a dome or a lofted panel that is essentially free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristics of the skin. The skin may be formed from a monolithic one-piece material, such as metal of composites, and may include various integrally formed reinforcing features.

    摘要翻译： 用于飞行器的加压隔板或面板包括能量吸收皮肤，其响应于向皮肤施加至少阈值量的冲击能量的物体撞击而变形。 皮肤可以被配置为基本上没有刚性加强件和不可变形的加强件的圆顶或顶部面板，否则会妨碍皮肤的柔性特性。 皮肤可以由单片整体材料形成，例如复合材料的金属，并且可以包括各种整体形成的增强特征。

    COMPLIANT CROWN PANEL FOR AN AIRCRAFT
    3.
    发明申请
    COMPLIANT CROWN PANEL FOR AN AIRCRAFT 有权
    合适的CROWN面板

    公开(公告)号：US20130087657A9

    公开(公告)日：2013-04-11

    申请号：US12965451

    申请日：2010-12-10

    申请人： William J. Koch ,  Donald P. Matheson

    发明人： William J. Koch ,  Donald P. Matheson

    IPC分类号： B64C1/10 ,  C23F1/04 ,  B32B37/02 ,  B64D45/00 ,  B64C1/14

    CPC分类号： B64C1/10 ,  B64C1/36 ,  Y10T156/10

    摘要： An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign objects, such as birds. The dome is intentionally designed to deform in response to a foreign object strike that imparts at least a threshold amount of impact energy to the bulkhead. The dome is free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristic of the dome. Practical embodiments of the bulkhead utilize fewer parts, are less heavy, and are less expensive than traditional bulkheads that utilize rigid stiffeners. The crown panel has similar compliant characteristics. The crown panel is designed to simultaneously deform and deflect in response to foreign object impacts such as birds and hail. The crown panel is formed from a monolithic one-piece material, such as aluminum, and various reinforcing features are integrally formed in the material.

    摘要翻译： 这里描述了飞机前进压舱壁和飞机冠面板。 前向压力舱壁包括可塑性和可变形的穹顶，其构造成捕获诸如鸟类的异物。 圆顶被有意地设计成响应于向舱壁施加至少一个阈值量的冲击能量的异物撞击而变形。 圆顶没有刚性加强件和不可变形的加强件，否则会妨碍圆顶的柔性特性。 隔板的实际实施例使用更少的部件，更不重，并且比使用刚性加强件的传统舱壁便宜。 冠面板具有类似的柔顺特性。 冠面板设计成可以响应诸如鸟和冰雹等异物影响而同时变形和偏转。 冠面板由诸如铝的单片整体材料形成，并且在该材料中一体地形成各种增强特征。

    COMPLIANT CROWN PANEL FOR AN AIRCRAFT
    4.
    发明申请
    COMPLIANT CROWN PANEL FOR AN AIRCRAFT 有权
    合适的CROWN面板

    公开(公告)号：US20110101164A1

    公开(公告)日：2011-05-05

    申请号：US12965451

    申请日：2010-12-10

    申请人： William J. Koch ,  Donald P. Matheson

    发明人： William J. Koch ,  Donald P. Matheson

    IPC分类号： B64C1/10 ,  B64D45/00 ,  B64C1/14 ,  B32B37/02 ,  C23F1/04

    CPC分类号： B64C1/10 ,  B64C1/36 ,  Y10T156/10

    摘要： An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign objects, such as birds. The dome is intentionally designed to deform in response to a foreign object strike that imparts at least a threshold amount of impact energy to the bulkhead. The dome is free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristic of the dome. Practical embodiments of the bulkhead utilize fewer parts, are less heavy, and are less expensive than traditional bulkheads that utilize rigid stiffeners. The crown panel has similar compliant characteristics. The crown panel is designed to simultaneously deform and deflect in response to foreign object impacts such as birds and hail. The crown panel is formed from a monolithic one-piece material, such as aluminum, and various reinforcing features are integrally formed in the material.

    摘要翻译： 这里描述了飞机前进压舱壁和飞机冠面板。 前向压力舱壁包括可塑性和可变形的穹顶，其配置成“捕获”诸如鸟类的异物。 圆顶被有意地设计成响应于向舱壁施加至少一个阈值量的冲击能量的异物撞击而变形。 圆顶没有刚性加强件和不可变形的加强件，否则会妨碍圆顶的柔性特性。 隔板的实际实施例使用更少的部件，更不重，并且比使用刚性加强件的传统舱壁便宜。 冠面板具有类似的柔顺特性。 冠面板设计成可以响应诸如鸟和冰雹等异物影响而同时变形和偏转。 冠面板由诸如铝的单片整体材料形成，并且在该材料中一体地形成各种增强特征。

    Compliant crown panel for an aircraft
    5.
    发明授权
    Compliant crown panel for an aircraft 有权
    符合飞机的皇冠面板

    公开(公告)号：US08434716B2

    公开(公告)日：2013-05-07

    申请号：US12965451

    申请日：2010-12-10

    申请人： William J. Koch ,  Donald P. Matheson

    发明人： William J. Koch ,  Donald P. Matheson

    IPC分类号： B64C1/14

    CPC分类号： B64C1/10 ,  B64C1/36 ,  Y10T156/10

    摘要： An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign objects, such as birds. The dome is intentionally designed to deform in response to a foreign object strike that imparts at least a threshold amount of impact energy to the bulkhead. The dome is free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristic of the dome. Practical embodiments of the bulkhead utilize fewer parts, are less heavy, and are less expensive than traditional bulkheads that utilize rigid stiffeners. The crown panel has similar compliant characteristics. The crown panel is designed to simultaneously deform and deflect in response to foreign object impacts such as birds and hail. The crown panel is formed from a monolithic one-piece material, such as aluminum, and various reinforcing features are integrally formed in the material.

    摘要翻译： 这里描述了飞机前进压舱壁和飞机冠面板。 前向压力舱壁包括可塑性和可变形的穹顶，其配置成“捕获”诸如鸟类的异物。 圆顶被有意地设计成响应于向舱壁施加至少一个阈值量的冲击能量的异物撞击而变形。 圆顶没有刚性加强件和不可变形的加强件，否则会妨碍圆顶的柔性特性。 隔板的实际实施例使用更少的部件，更不重，并且比使用刚性加强件的传统舱壁便宜。 冠面板具有类似的柔顺特性。 冠面板设计成可以响应诸如鸟和冰雹等异物影响而同时变形和偏转。 冠面板由诸如铝的单片整体材料形成，并且在该材料中一体地形成各种增强特征。

    Compliant crown panel for an aircraft
    6.
    发明授权
    Compliant crown panel for an aircraft 有权
    符合飞机的皇冠面板

    公开(公告)号：US08398021B2

    公开(公告)日：2013-03-19

    申请号：US11682818

    申请日：2007-03-06

    申请人： William J. Koch ,  Donald P. Matheson

    发明人： William J. Koch ,  Donald P. Matheson

    IPC分类号： B64C1/12

    CPC分类号： B64C1/10 ,  B64C1/36 ,  Y10T156/10

    摘要： An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign objects, such as birds. The dome is intentionally designed to deform in response to a foreign object strike that imparts at least a threshold amount of impact energy to the bulkhead. The dome is free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristic of the dome. Practical embodiments of the bulkhead utilize fewer parts, are less heavy, and are less expensive than traditional bulkheads that utilize rigid stiffeners. The crown panel has similar compliant characteristics. The crown panel is designed to simultaneously deform and deflect in response to foreign object impacts such as birds and hail. The crown panel is formed from a monolithic one-piece material, such as aluminum, and various reinforcing features are integrally formed in the material.

    摘要翻译： 这里描述了飞机前进压舱壁和飞机冠面板。 前向压力舱壁包括可塑性和可变形的穹顶，其构造成捕获诸如鸟类的异物。 圆顶被有意地设计成响应于向舱壁施加至少一个阈值量的冲击能量的异物撞击而变形。 圆顶没有刚性加强件和不可变形的加强件，否则会妨碍圆顶的柔性特性。 隔板的实际实施例使用更少的部件，更不重，并且比使用刚性加强件的传统舱壁便宜。 冠面板具有类似的柔顺特性。 冠面板设计成可以响应诸如鸟和冰雹等异物影响而同时变形和偏转。 冠面板由诸如铝的单片整体材料形成，并且在该材料中一体地形成各种增强特征。