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1. 发明授权

US08714485B2 Method of fabricating a hat stringer 有权
标题翻译：制作帽子的方法
公开(公告)号：US08714485B2
公开(公告)日：2014-05-06
申请号：US12638977
申请日：2009-12-15
申请人： Donald P. Matheson , Kenneth L. Brook
发明人： Donald P. Matheson , Kenneth L. Brook
IPC分类号： B64C1/00 , B64C3/00 , B64C5/00
CPC分类号： B64C1/064 , B29C70/00 , B29D99/0014 , B32B3/02 , B32B5/26 , B32B7/045 , B32B7/08 , B32B2260/021 , B32B2260/023 , B32B2260/046 , B32B2262/106 , B32B2605/18 , B32B2607/00 , B64C3/182 , B64C3/26 , Y10T29/49622 , Y10T428/2457 , Y10T428/24612 , Y10T428/31511
摘要： A structure may comprise a skin member and a hat stringer. The hat stringer may include a base portion and first and second webs extending outwardly from the base portion. Each one of the first and second webs may be comprised of a wrap laminate having wrap plies and a cover laminate having cover plies. The first and second webs may be interconnected by a cap. The hat stringer and skin member may be co-cured.
摘要翻译：结构可以包括皮肤构件和帽子纵梁。帽子纵梁可以包括基部和从基部向外延伸的第一和第二腹板。第一和第二纤维网中的每一个可以由具有包裹层的包裹层压材料和具有覆盖层的盖层压板构成。第一和第二纤维网可以通过盖相互连接。帽子绷带和皮肤构件可以被共同固化。

2. 发明申请

US20110139932A1 HIGH PULLOFF CAPABILITY HAT STRINGER 有权
标题翻译：高弹力能力帽
公开(公告)号：US20110139932A1
公开(公告)日：2011-06-16
申请号：US12638977
申请日：2009-12-15
申请人： Donald P. Matheson , Kenneth L. Brook
发明人： Donald P. Matheson , Kenneth L. Brook
IPC分类号： B64C1/12 , B32B37/02 , B21D53/88
CPC分类号： B64C1/064 , B29C70/00 , B29D99/0014 , B32B3/02 , B32B5/26 , B32B7/045 , B32B7/08 , B32B2260/021 , B32B2260/023 , B32B2260/046 , B32B2262/106 , B32B2605/18 , B32B2607/00 , B64C3/182 , B64C3/26 , Y10T29/49622 , Y10T428/2457 , Y10T428/24612 , Y10T428/31511
摘要： A structure may comprise a skin member and a hat stringer. The hat stringer may include a base portion and first and second webs extending outwardly from the base portion. Each one of the first and second webs may be comprised of a wrap laminate having wrap plies and a cover laminate having cover plies. The first and second webs may be interconnected by a cap. The hat stringer and skin member may be co-cured.
摘要翻译：结构可以包括皮肤构件和帽子纵梁。帽子纵梁可以包括基部和从基部向外延伸的第一和第二腹板。第一和第二纤维网中的每一个可以由具有包裹层的包裹层压材料和具有覆盖层的盖层压板构成。第一和第二纤维网可以通过盖相互连接。帽子绷带和皮肤构件可以被共同固化。

3. 发明申请

US20130087657A9 COMPLIANT CROWN PANEL FOR AN AIRCRAFT 有权
标题翻译：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。

4. 发明申请

US20080149769A1 COMPLIANT PANEL FOR AIRCRAFT 有权
标题翻译：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。

5. 发明授权

US07997529B2 Compliant panel for aircraft 有权
标题翻译：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。

6. 发明申请

US20110101164A1 COMPLIANT CROWN PANEL FOR AN AIRCRAFT 有权
标题翻译：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。

7. 发明授权

US08548544B2 System, method and article for controlling the dispensing of insulin 有权
公开(公告)号：US08548544B2
公开(公告)日：2013-10-01
申请号：US12305582
申请日：2007-06-19
申请人： Robert C. Kircher, Jr. , Richard S. Mauseth , Jason N. Bishop , Donald P. Matheson , Suray Bhatia , Jeff A. Bilmes
发明人： Robert C. Kircher, Jr. , Richard S. Mauseth , Jason N. Bishop , Donald P. Matheson , Suray Bhatia , Jeff A. Bilmes
IPC分类号： A61B5/00
CPC分类号： A61M5/1723 , A61B5/14532 , A61M2230/005 , A61M2230/201 , G06F19/00 , G06F19/3456 , G06F19/3468 , G06N5/048 , G16H50/50
摘要： A system and method for automatically adjusting parameters for predicting blood glucose levels and/or controlling the dispensing of insulin. In one embodiment, the system is a stand-alone system. In one embodiment, the system is part of a system for controlling the dispensing of insulin.

8. 发明申请

US20100292634A1 SYSTEM, METHOD AND ARTICLE FOR CONTROLLING THE DISPENSING OF INSULIN 有权
标题翻译：用于控制胰岛素分配的系统，方法和文章
公开(公告)号：US20100292634A1
公开(公告)日：2010-11-18
申请号：US12305582
申请日：2007-06-19
申请人： Robert C. Kircher, JR. , Richard S. Mauseth , Jason N. Bishop , Donald P. Matheson , Suray Bhatia , Jeff A. Bilmes
发明人： Robert C. Kircher, JR. , Richard S. Mauseth , Jason N. Bishop , Donald P. Matheson , Suray Bhatia , Jeff A. Bilmes
IPC分类号： A61M37/00
CPC分类号： A61M5/1723 , A61B5/14532 , A61M2230/005 , A61M2230/201 , G06F19/00 , G06F19/3456 , G06F19/3468 , G06N5/048 , G16H50/50
摘要： A system and method for automatically adjusting parameters for predicting blood glucose levels and/or controlling the dispensing of insulin. In one embodiment, the system is a stand-alone system. In one embodiment, the system is part of a system for controlling the dispensing of insulin.
摘要翻译：一种用于自动调节用于预测血糖水平和/或控制胰岛素分配的参数的系统和方法。在一个实施例中，系统是独立系统。在一个实施例中，系统是用于控制胰岛素分配的系统的一部分。

9. 发明授权

US08434716B2 Compliant crown panel for an aircraft 有权
标题翻译：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。

10. 发明授权

US08398021B2 Compliant crown panel for an aircraft 有权
标题翻译：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。

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