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公开(公告)号：US20070102963A1
公开(公告)日：2007-05-10
申请号：US11164120
申请日：2005-11-10
IPC分类号： B62D25/20
CPC分类号： B62D21/155
摘要： An underbody crash device for a vehicle. The underbody crash device comprises a pillar member attached to the vehicle. The vehicle has a primary load path for absorbing crash energy in a collision. The pillar member is movable to a deployed position for supporting the vehicle directly on the ground and positioning the primary load path to increase crash energy absorbed therein.
摘要翻译： 用于车辆的底部碰撞装置。 底体碰撞装置包括附接到车辆的柱构件。 车辆具有用于在碰撞中吸收碰撞能量的主要负载路径。 支柱构件可移动到展开位置，用于将车辆直接支撑在地面上并且定位主负载路径以增加其中吸收的碰撞能量。
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公开(公告)号：US07237828B2
公开(公告)日：2007-07-03
申请号：US11164120
申请日：2005-11-10
IPC分类号： B60T7/12
CPC分类号： B62D21/155
摘要： An underbody crash device for a vehicle. The underbody crash device comprises a pillar member attached to the vehicle. The vehicle has a primary load path for absorbing crash energy in a collision. The pillar member is movable to a deployed position for supporting the vehicle directly on the ground and positioning the primary load path to increase crash energy absorbed therein.
摘要翻译： 用于车辆的底部碰撞装置。 底体碰撞装置包括附接到车辆的柱构件。 车辆具有用于在碰撞中吸收碰撞能量的主要负载路径。 支柱构件可移动到展开位置，用于将车辆直接支撑在地面上并且定位主负载路径以增加其中吸收的碰撞能量。
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公开(公告)号：US07284788B1
公开(公告)日：2007-10-23
申请号：US11163300
申请日：2005-10-13
申请人： Saeed Barbat , Gregory Frederick , Li Chai , Phillip Przybylo , Xiaowei Li
发明人： Saeed Barbat , Gregory Frederick , Li Chai , Phillip Przybylo , Xiaowei Li
IPC分类号： B06R19/02
摘要： An energy-absorbing underrun protection system for a vehicle. The energy-absorbing underrun protection system is comprised of a deformable construction adapted for deforming along a longitudinal axis to absorb crash energy. This deformable construction has a torque arm member extending substantially perpendicularly therefrom for receiving an impact load offset from the longitudinal axis and bending the deformable construction toward the impact load.
摘要翻译： 一种用于车辆的能量吸收欠载保护系统。 能量吸收防钻撞保护系统包括可变形结构，其适于沿着纵向轴线变形以吸收碰撞能量。 该可变形结构具有大致垂直延伸的扭矩臂构件，用于接收从纵向轴线偏移的冲击载荷并将可变形构造朝向冲击载荷弯曲。
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4.发明申请AUTOMOTIVE VEHICLE FRONT ARCHITECTURE WITH A PARTIALLY ROTATABLE STRUCTURAL LINK 有权具有部分可旋转结构链接的汽车车身结构公开(公告)号：US20070040414A1
公开(公告)日：2007-02-22
申请号：US11161830
申请日：2005-08-18
申请人： Gregory Frederick , Phillip Przybylo , Li Chai , Xiaowei Li
发明人： Gregory Frederick , Phillip Przybylo , Li Chai , Xiaowei Li
IPC分类号： B62D25/08
CPC分类号： B62D21/152
摘要： An automotive vehicle front structure includes upper and lower siderails and a structural link extending from the upper and lower siderails, with the structural link having a pivotable connection to the upper siderail and a rigid connection to the lower siderail, such that energy absorption provided by the structure may be tailored by varying the character of the joint between the structural link and the upper siderail.
摘要翻译： 机动车辆前部结构包括上部和下部挡板以及从上部和下部挡板延伸的结构连杆，结构连杆具有与上部侧板的可枢转连接，并且与下部侧杆形成刚性连接，使得由 结构可以通过改变结构连杆和上侧甲板之间的关节的特性来定制。
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公开(公告)号：US20060138093A1
公开(公告)日：2006-06-29
申请号：US11060937
申请日：2005-02-18
CPC分类号： B23K26/206 , B23K9/00 , B23K9/044 , B23K10/00 , B23K15/00 , B23K20/002 , B23K20/021 , B23K26/32 , B23K26/342 , B23K26/60 , B23K2101/001 , B23K2103/18 , B23K2103/26 , B23P6/007 , C22F1/10 , F01D5/005 , F05D2230/232 , F05D2230/30
摘要： A method of repairing a metallic component, such as a superalloy turbine blade or turbine nozzle, includes the step of preparing the component by stripping the protective coatings from the component. The component is then pre-conditioned for welding by a first hot isostatic process. Once the conditioning sequence is complete, the component is welded using any of a number of welding techniques and by adding weld fillers to the weld area. After the welding step, the component is sealed by a second hot isostatic process treatment performed at conditions similar to the first hot isostatic process. The component is finally prepared for re-entry into service.
摘要翻译： 修复诸如超级合金涡轮机叶片或涡轮喷嘴的金属部件的方法包括通过从组件剥离保护涂层来制备组件的步骤。 然后通过第一个热等静压过程对该部件进行预处理以进行焊接。 一旦调理顺序完成，使用多种焊接技术焊接组件，并通过在焊接区域添加焊接填料。 在焊接步骤之后，通过在类似于第一热等静压工艺的条件下进行的第二次热等静压处理来密封部件。 该组件终于准备重新投入使用。
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公开(公告)号：US06364971B1
公开(公告)日：2002-04-02
申请号：US09487931
申请日：2000-01-20
申请人： Artie Gene Peterson, Jr. , David Wayne Gandy , Gregory Frederick , Jan T. Stover , Ramaswamy Viswanathan
发明人： Artie Gene Peterson, Jr. , David Wayne Gandy , Gregory Frederick , Jan T. Stover , Ramaswamy Viswanathan
IPC分类号： B23K2634
CPC分类号： B23K26/206 , B23K9/00 , B23K9/044 , B23K10/00 , B23K15/00 , B23K20/002 , B23K20/021 , B23K26/32 , B23K26/342 , B23K26/60 , B23K2101/001 , B23K2103/18 , B23K2103/26 , B23P6/007 , C22F1/10 , F01D5/005 , F05D2230/232 , F05D2230/30
摘要： A method of repairing a metallic member, such as a superalloy turbine blade, includes the step of preparing the blade by stripping the protective coatings from the blade. The blade is then pre-conditioned for welding by a first hot isostatic process. Once the blade conditioning sequence is complete, the blade is welded using a laser welding technique and by adding weld fillers to the weld area. After the welding step, the blade is sealed by a second hot isostatic process treatment performed at conditions similar to the first hot isostatic process. The blade is finally prepared for re-entry into service.
摘要翻译： 修复诸如超级合金涡轮机叶片的金属构件的方法包括通过从刀片剥离保护涂层来制备刀片的步骤。 然后通过第一个热等静压过程对刀片进行预处理以进行焊接。 一旦刀片调理顺序完成，刀片将使用激光焊接技术进行焊接，并通过在焊接区域添加焊接填料。 在焊接步骤之后，通过在与第一热等静压过程类似的条件下进行的第二次热等静压处理来对刀片进行密封。 刀片最终准备重新投入使用。
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7.发明申请公开(公告)号：US20060086776A1
公开(公告)日：2006-04-27
申请号：US10972247
申请日：2004-10-22
IPC分类号： B23K31/00
CPC分类号： B23K20/021 , B23K2101/001 , F01D5/005 , F05D2230/80
摘要： Accordingly, the present invention provides a method for joining metallic members, which can be used to join component sub-assemblies. Further, the present invention provides a method for repairing a component by replacing a damaged portion and re-inserting a replacement section. In general, the present invention provides in one embodiment a method for joining metallic members comprising: preparing a surface of a first metallic member, thereby providing an oxide-free surface; preparing a surface of a second metallic member, thereby providing an oxide-free surface; applying pressure to the first and second metallic members, thereby forcing the surface of the first metallic member and the surface of the second metallic member together and forming a joint area; sealing an outer edge of the joint area; and subjecting the members to a hot isostatic process operation.
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公开(公告)号：US20050126664A1
公开(公告)日：2005-06-16
申请号：US10704240
申请日：2003-11-07
CPC分类号： B23K26/206 , B23K9/00 , B23K9/044 , B23K10/00 , B23K15/00 , B23K20/002 , B23K20/021 , B23K26/32 , B23K26/342 , B23K26/60 , B23K2101/001 , B23K2103/18 , B23K2103/26 , B23P6/007 , C22F1/10 , F01D5/005 , F05D2230/232 , F05D2230/30
摘要： A method of repairing a metallic component, such as a superalloy turbine blade or turbine nozzle, includes the step of preparing the component by stripping the protective coatings from the component. The component is then pre-conditioned for welding by a first hot isostatic process. Once the conditioning sequence is complete, the component is welded using any of a number of welding techniques and by adding weld fillers to the weld area. After the welding step, the component is sealed by a second hot isostatic process treatment performed at conditions similar to the first hot isostatic process. The component is finally prepared for re-entry into service.
摘要翻译： 修复诸如超级合金涡轮机叶片或涡轮喷嘴的金属部件的方法包括通过从组件剥离保护涂层来制备组件的步骤。 然后通过第一个热等静压过程对该部件进行预处理以进行焊接。 一旦调理顺序完成，使用多种焊接技术焊接组件，并通过在焊接区域添加焊接填料。 在焊接步骤之后，通过在类似于第一热等静压工艺的条件下进行的第二次热等静压处理来密封部件。 该组件终于准备重新投入使用。
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