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1. 发明授权

US08274024B2 Control surface assemblies with torque tube base 有权
标题翻译：带扭矩管底座的控制面组件
公开(公告)号：US08274024B2
公开(公告)日：2012-09-25
申请号：US13018406
申请日：2011-01-31
申请人： Jeffery D. Russom , Lawrence R. White , James Greenwood
发明人： Jeffery D. Russom , Lawrence R. White , James Greenwood
IPC分类号： F42B15/01 , B64C1/26
CPC分类号： F42B10/04 , B64C1/26 , B64C5/00 , B64C5/06 , B64C9/02 , Y02T50/44
摘要： Control surface assemblies have a torque tube base. In one embodiment, a method includes moving an aerospace vehicle through a medium; and moving at least a portion of a control surface assembly to generate a force for controlling the vehicle.
摘要翻译：控制面组件有一个扭矩管底座。在一个实施例中，一种方法包括使航空航天车辆移动通过介质; 以及移动控制表面组件的至少一部分以产生用于控制车辆的力。

2. 发明申请

US20080302918A1 CONTROL SURFACE ASSEMBLIES WITH TORQUE TUBE BASE 审中-公开
标题翻译：带扭矩管座的控制面组件
公开(公告)号：US20080302918A1
公开(公告)日：2008-12-11
申请号：US12038319
申请日：2008-02-27
申请人： Jeffery D. Russom , Lawrence R. White , James Greenwood
发明人： Jeffery D. Russom , Lawrence R. White , James Greenwood
IPC分类号： B64C3/58
CPC分类号： F42B10/04 , B64C1/26 , B64C5/00 , B64C5/06 , B64C9/02 , Y02T50/44
摘要： Control surface assemblies having a torque tube base are disclosed. In one embodiment, a method includes providing a control surface assembly including: providing a control surface portion having a pair of longitudinal surfaces, providing a hollow base portion coupled to the control surface portion, the base portion including an elongated curved wall, and an elongated base plate disposed crosswise to the pair of the longitudinal surfaces having at least one aperture disposed therein, and a plurality of attachment flanges extending laterally outwardly beyond the longitudinal surfaces; coupling the attachment flanges to a supporting structure of a vehicle such that the control surface portion projects outwardly from the supporting structure; moving the vehicle through a medium; and moving at least a portion of the control surface assembly to generate a force on the vehicle.
摘要翻译：公开了具有扭矩管底座的控制表面组件。在一个实施例中，一种方法包括提供控制表面组件，其包括：提供具有一对纵向表面的控制表面部分，提供联接到所述控制表面部分的中空基部，所述基部包括细长弯曲壁，以及细长基板与所述一对纵向表面交叉设置，所述纵向表面具有设置在其中的至少一个孔，以及多个附接凸缘，其横向向外延伸超过所述纵向表面; 将附接凸缘联接到车辆的支撑结构，使得控制表面部分从支撑结构向外突出; 将车辆移动通过介质; 以及移动所述控制表面组件的至少一部分以在所述车辆上产生力。

3. 发明授权

US07410120B2 Control surface assemblies with torque tube base 有权
标题翻译：带扭矩管底座的控制面组件
公开(公告)号：US07410120B2
公开(公告)日：2008-08-12
申请号：US11043918
申请日：2005-01-21
申请人： Jeffery D. Russom , Lawrence R. White , James Greenwood
发明人： Jeffery D. Russom , Lawrence R. White , James Greenwood
IPC分类号： B64C1/26 , B64C5/06 , B64C5/02
CPC分类号： F42B10/04 , B64C1/26 , B64C5/00 , B64C5/06 , B64C9/02 , Y02T50/44
摘要： Control surface assemblies having a torque tube base are disclosed. In one embodiment, a control surface assembly includes a control surface portion and a base portion. The base portion has a hollow, shell-like base portion coupled to a first end portion of the control surface portion, and is adapted to be coupled to a supporting structure such that the control surface portion projects outwardly from the supporting structure. In one aspect, the base portion includes an elongated, closed section portion adapted to be coupled to the supporting structure. In a further aspect, the base portion includes an elongated, closed section portion adapted to be coupled to the supporting structure, and a pair of tapered end portions formed at opposing ends of the closed section portion.
摘要翻译：公开了具有扭矩管底座的控制表面组件。在一个实施例中，控制表面组件包括控制表面部分和基部部分。底座部分具有联接到控制表面部分的第一端部的中空的壳状基部，并且适于联接到支撑结构，使得控制表面部分从支撑结构向外突出。在一个方面，基部包括适于联接到支撑结构的细长的闭合部分部分。在另一方面，基部包括适于联接到支撑结构的细长的闭合部分部分和形成在闭合部分部分的相对端部处的一对锥形端部部分。

4. 发明申请

US20110210200A1 CONTROL SURFACE ASSEMBLIES WITH TORQUE TUBE BASE 有权
标题翻译：带扭矩管座的控制面组件
公开(公告)号：US20110210200A1
公开(公告)日：2011-09-01
申请号：US13018406
申请日：2011-01-31
申请人： Jeffery D. Russom , Lawrence R. White , James Greenwood
发明人： Jeffery D. Russom , Lawrence R. White , James Greenwood
IPC分类号： B64C19/00
CPC分类号： F42B10/04 , B64C1/26 , B64C5/00 , B64C5/06 , B64C9/02 , Y02T50/44
摘要： Control surface assemblies have a torque tube base. In one embodiment, a method includes moving an aerospace vehicle through a medium; and moving at least a portion of a control surface assembly to generate a force for controlling the vehicle.
摘要翻译：控制面组件有一个扭矩管底座。在一个实施例中，一种方法包括使航空航天车辆移动通过介质; 以及移动控制表面组件的至少一部分以产生用于控制车辆的力。

5. 发明授权

US5797239A Titanium reinforced structural panel having a predetermined shape 失效
标题翻译：具有预定形状的钛增强结构板
公开(公告)号：US5797239A
公开(公告)日：1998-08-25
申请号：US782228
申请日：1997-01-13
申请人： Mark A. Zaccone , Jeffery D. Russom
发明人： Mark A. Zaccone , Jeffery D. Russom
IPC分类号： B21D26/055 , B23K20/02 , E04C2/34
CPC分类号： B21D26/055 , B23K20/023 , B23K2203/14
摘要： A method of fabricating a structural panel having a predetermined shape in which an inflatable envelope assembly is formed from at least a pair of superplastically formed and diffusion bonded metallic core sheets. The inflatable envelope assembly can be disposed between first and second metallic face sheets which are generally superplastically formed into the predetermined shape prior to being assembled. Thereafter, the assembled face sheets and the inflatable envelope assembly can be superplastically formed and diffusion bonded to form an integral structure, such as structural panel having a compound curvature. Alternatively, the inflatable envelope assembly can be disposed between a pair of reinforced titanium composite sheets. The reinforced titanium composite sheets can also be joined to adjacent face sheets, such as by welding or diffusion bonding, such that an integral structural panel having the predetermined shape can be readily fabricated. The reinforced titanium composite sheets have a flow stress greater than the inflatable envelope assembly and the face sheets to provide increased strength and stiffness for the resulting structural panel. The structural panel can also have a variety of predetermined shapes, such as predetermined complex shapes including shapes having a predetermined compound curvature. The resulting structural panel, such as a wing, wing tip or fan blade, is also generally smooth so as to eliminate mold line defects which adversely affect the aerodynamic performance of the structural panel.
摘要翻译：一种制造具有预定形状的结构板的方法，其中由至少一对超塑性和扩散结合的金属芯片形成可膨胀的外壳组件。可充气封套组件可以设置在第一和第二金属面板之间，在组装之前通常超塑性地形成预定形状。此后，组装的面板和可膨胀的外壳组件可以被超塑性地形成并且扩散接合以形成整体结构，例如具有复合曲率的结构面板。或者，可充气封套组件可以设置在一对增强的钛复合片之间。增强的钛复合片也可以通过焊接或扩散接合而接合到相邻的面片，使得可以容易地制造具有预定形状的整体式结构面板。增强的钛复合片材具有大于可充气封套组件和面板的流动应力，以为所得到的结构板提供增加的强度和刚度。结构面板还可以具有各种预定形状，例如包括具有预定复合曲率的形状的预定复杂形状。所得到的结构板，例如机翼，翼尖或风扇叶片，也通常是平滑的，以便消除不利地影响结构板的空气动力性能的模具线缺陷。

6. 发明授权

US5687900A Structural panel having a predetermined shape and an associated method for superplastically forming and diffusion bonding the structural panel 失效
标题翻译：具有预定形状的结构板和用于超塑性地形成和扩散结合结构板的相关方法
公开(公告)号：US5687900A
公开(公告)日：1997-11-18
申请号：US411477
申请日：1995-03-28
申请人： Mark A. Zaccone , Jeffery D. Russom
发明人： Mark A. Zaccone , Jeffery D. Russom
IPC分类号： B21D26/055 , B23K20/02 , B23K20/00 , B23K101/02
CPC分类号： B21D26/055 , B23K20/023 , B23K2203/14
摘要： A method of fabricating a structural panel having a predetermined shape features forming an inflatable envelope assembly from at least a pair of superplastically formed and diffusion bonded metallic core sheets. The inflatable envelope assembly can be disposed between first and second metallic face sheets which are generally superplastically formed into the predetermined shape prior to being assembled. Thereafter, the assembled face sheets and the inflatable envelope assembly can be superplastically formed and diffusion bonded to form an integral structure, such as structural panel having a compound curvature. Alternatively, the inflatable envelope assembly can be disposed between a pair of reinforced titanium composite sheets. The reinforced titanium composite sheets can also be joined to adjacent face sheets, such as by welding or diffusion bonding, such that an integral structural panel having the predetermined shape can be readily fabricated. The reinforced titanium composite sheets have a flow stress greater than the inflatable envelope assembly and the face sheets to provide increased strength and stiffness for the resulting structural panel.
摘要翻译：制造具有预定形状的结构板的方法特征在于，形成了至少一对超塑性和扩散粘合的金属芯片的可充气外壳组件。可充气封套组件可以设置在第一和第二金属面板之间，在组装之前通常超塑性地形成预定形状。此后，组装的面板和可膨胀的外壳组件可以被超塑性地形成并且扩散接合以形成整体结构，例如具有复合曲率的结构面板。或者，可充气封套组件可以设置在一对增强的钛复合片之间。增强的钛复合片也可以通过焊接或扩散接合而接合到相邻的面片，使得可以容易地制造具有预定形状的整体式结构面板。增强的钛复合片材具有大于可充气封套组件和面板的流动应力，以为所得到的结构板提供增加的强度和刚度。

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