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1. 发明申请

US20100162567A1 MOUNTING DEVICE FOR AN AIRCRAFT 有权
标题翻译：安装飞机装置
公开(公告)号：US20100162567A1
公开(公告)日：2010-07-01
申请号：US11556125
申请日：2006-11-02
申请人： Brad L. Kirkwood , Paul S. Gregg , Gerry D. Miller , Jeff D. Will , David W. Evans
发明人： Brad L. Kirkwood , Paul S. Gregg , Gerry D. Miller , Jeff D. Will , David W. Evans
IPC分类号： B21D53/88 , B23Q1/00
CPC分类号： B64C3/28 , B64F5/10 , Y10T29/49622 , Y10T29/53991
摘要： The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.
摘要翻译：本发明涉及飞机中的安装装置。在本发明的一个方面，公开了一种组装安装装置的金属固定件的方法。在本发明的另一方面，公开了一种安装装置。在本发明的另一方面，公开了一种用于在飞行器中安装和使用安装装置的方法。

2. 发明申请

US20080105661A1 METHOD AND APPARATUS TO CONSTRUCT METAL SECUREMENT MEMBER FOR AN AIRCRAFT 有权
标题翻译：构建飞机金属保护部件的方法和装置
公开(公告)号：US20080105661A1
公开(公告)日：2008-05-08
申请号：US11556099
申请日：2006-11-02
申请人： Brad L. Kirkwood , Paul S. Gregg , Gerry D. Miller , Jeff D. Will , David W. Evans
发明人： Brad L. Kirkwood , Paul S. Gregg , Gerry D. Miller , Jeff D. Will , David W. Evans
IPC分类号： B23K26/00
CPC分类号： B64F5/0009 , B23K3/087 , B23K31/00 , B64C3/185 , B64F5/10 , Y10T403/4605
摘要： The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.
摘要翻译：本发明涉及飞机中的安装装置。在本发明的一个方面，公开了一种组装安装装置的金属固定件的方法。在本发明的另一方面，公开了一种安装装置。在本发明的另一方面，公开了一种用于在飞行器中安装和使用安装装置的方法。

3. 发明授权

US09016551B2 Method and apparatus to construct metal securement member for an aircraft 有权
标题翻译：构建飞机金属固定件的方法和装置
公开(公告)号：US09016551B2
公开(公告)日：2015-04-28
申请号：US11556099
申请日：2006-11-02
申请人： Brad L. Kirkwood , Paul S. Gregg , Gerry D. Miller , Jeff D. Will , David W. Evans
发明人： Brad L. Kirkwood , Paul S. Gregg , Gerry D. Miller , Jeff D. Will , David W. Evans
IPC分类号： B23K1/20 , B23K3/00 , B23K31/00 , B64C3/18
CPC分类号： B64F5/0009 , B23K3/087 , B23K31/00 , B64C3/185 , B64F5/10 , Y10T403/4605
摘要： The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.
摘要翻译：本发明涉及飞机中的安装装置。在本发明的一个方面，公开了一种组装安装装置的金属固定件的方法。在本发明的另一方面，公开了一种安装装置。在本发明的另一方面，公开了一种用于在飞行器中安装和使用安装装置的方法。

4. 发明授权

US07810757B2 Mounting device for an aircraft 有权
标题翻译：飞机安装装置
公开(公告)号：US07810757B2
公开(公告)日：2010-10-12
申请号：US11556125
申请日：2006-11-02
申请人： Brad L Kirkwood , Paul S. Gregg , Gerald D. Miller , Jeff D. Will , David W. Evans
发明人： Brad L Kirkwood , Paul S. Gregg , Gerald D. Miller , Jeff D. Will , David W. Evans
IPC分类号： B64C3/26
CPC分类号： B64C3/28 , B64F5/10 , Y10T29/49622 , Y10T29/53991
摘要： The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.
摘要翻译：本发明涉及飞机中的安装装置。在本发明的一个方面，公开了一种组装安装装置的金属固定件的方法。在本发明的另一方面，公开了一种安装装置。在本发明的另一方面，公开了一种在飞行器中安装和使用安装装置的方法。

5. 发明授权

US5534354A Multiple density sandwich structures 失效
标题翻译：多密度三明治结构
公开(公告)号：US5534354A
公开(公告)日：1996-07-09
申请号：US474336
申请日：1995-06-07
申请人： Paul S. Gregg , Matthew G. Kistner , Jeff D. Will
发明人： Paul S. Gregg , Matthew G. Kistner , Jeff D. Will
IPC分类号： B21D26/055 , B23K26/20 , B64C1/00 , B64C3/20 , B64C27/473 , E04C2/32 , B32B3/28 , B32B15/00
CPC分类号： B64C1/06 , B21D26/055 , B23K26/244 , B23K26/26 , B23K26/28 , B64C1/08 , B64C27/473 , B64C3/20 , E04C2/322 , B64C2001/0072 , B64C2001/0081 , B64C2027/4736 , Y02T50/433 , Y10S72/709 , Y10T29/49339 , Y10T428/1234 , Y10T428/12347 , Y10T428/12639 , Y10T428/12806
摘要： A method to superplastic form sandwich structures is provided. A series of worksheets are joined together at selected locations through the use of partial penetration welding. The worksheets are subsequently superplastic formed in order to form a sandwich structure. The method allows a different number of worksheets to be used at different points throughout the sandwich structure. This results in a sandwich structure with a different internal reinforcement at different locations in the sandwich structure. In the preferred embodiment, a wing is fabricated from a series of worksheets partial penetration welded together using a laser. The worksheets are superplastic formed to producing a wing with a different internal reinforcement at two or more locations in the wing. The wing includes a pair of double thickness skins that define a major portion of aerodynamically smooth outer surface of the airfoil. Each skin is formed from at least two sheets of superplastically formed material that are joined by diffusion bonding. The internal reinforcement extends between the surface's interior surfaces of the skins and are welded to the skins by wave welds. The webs of the internal reinforcement extend between the skins diagonally and each web is formed of a single sheet of superplastically formed material.
摘要翻译：提供了一种超塑性夹层结构的方法。一系列工作表通过部分穿透焊接在选定的位置连接在一起。工件表随后被形成为超塑性以形成夹层结构。该方法允许在整个夹层结构中的不同点使用不同数量的工作表。这导致在夹层结构中在不同位置处具有不同内部加强件的夹层结构。在优选实施例中，翼由使用激光部分穿透焊接在一起的一系列工作表制成。工作表是超塑性的，用于在翼中的两个或更多个位置处产生具有不同内部加强件的翼。机翼包括一对双层厚皮，其限定了翼型的空气动力学平滑的外表面的主要部分。每个皮肤由通过扩散粘合连接的至少两片超塑性材料形成。内部加强件在表面的表面的内表面之间延伸并且通过波纹焊接到表皮上。内部加强筋的腹板在对角线之间延伸，每个腹板由单层超塑性材料形成。

6. 发明授权

US07642481B2 Apparatus and method for forming corrugated members 有权
标题翻译：用于形成波纹构件的装置和方法
公开(公告)号：US07642481B2
公开(公告)日：2010-01-05
申请号：US11464650
申请日：2006-08-15
申请人： Max U. Kismarton , Paul S. Gregg , Jeff D. Will
发明人： Max U. Kismarton , Paul S. Gregg , Jeff D. Will
IPC分类号： B23K26/20 , B21D47/01
CPC分类号： B21D13/02 , Y10T29/49634
摘要： An apparatus and method for forming a stringer are provided. The stringer generally includes a web having a desired corrugated configuration and first and second flanges welded to opposite edges of the web. The apparatus includes a support structure, a strongback that is supported by the support structure, and a plurality of dies that are adjustable relative to the strongback. The strongback defines a corrugated contour surface corresponding to the desired corrugated configuration of the web. The dies define corresponding forming surfaces and are configured to be advanced toward the strongback to thereby form the web to the desired corrugated configuration between the contour surface of the strongback and the forming surfaces of the dies. Further, the apparatus can receive the flanges of the stringer in a predetermined configuration with the web so that the flanges can be welded to the web while the web is supported by the strongback and dies in the desired corrugated configuration.
摘要翻译：提供了一种用于形成纵梁的装置和方法。纵梁通常包括具有期望的波纹构造的腹板和焊接到腹板的相对边缘的第一和第二凸缘。该装置包括支撑结构，由支撑结构支撑的强力支撑件，以及可相对于强力可调节的多个模具。强力定义对应于网的期望的波纹构造的波纹轮廓表面。模具限定相应的成形表面，并且被构造成朝向强力推进，从而在强力的轮廓表面和模具的成形表面之间形成所需的波纹状结构。此外，该装置可以以带有网的预定构造接收纵梁的凸缘，使得凸缘可以被焊接到腹板上，同时腹板被强力支撑并且以期望的波纹结构模具。

7. 发明授权

US5330092A Multiple density sandwich structures and method of fabrication 失效
标题翻译：多密度夹层结构及其制造方法
公开(公告)号：US5330092A
公开(公告)日：1994-07-19
申请号：US809304
申请日：1991-12-17
申请人： Paul S. Gregg , Matthew G. Kistner , Jeff D. Will
发明人： Paul S. Gregg , Matthew G. Kistner , Jeff D. Will
IPC分类号： B21D26/055 , B23K26/20 , B64C1/00 , B64C3/20 , B64C27/473 , E04C2/32 , B23K28/02
CPC分类号： B64C1/06 , B21D26/055 , B23K26/244 , B23K26/26 , B23K26/28 , B64C1/08 , B64C27/473 , B64C3/20 , E04C2/322 , B64C2001/0072 , B64C2001/0081 , B64C2027/4736 , Y02T50/433 , Y10S72/709 , Y10T29/49339 , Y10T428/1234 , Y10T428/12347 , Y10T428/12639 , Y10T428/12806
摘要： A method to superplastic form sandwich structures is provided. A series of worksheets are joined together at selected locations through the use of partial penetration welding. The worksheets are subsequently superplastic formed in order to form a sandwich structure. The method allows a different number of worksheets to be used at different points throughout the sandwich structure. This results in a sandwich structure with a different internal reinforcement at different locations in the sandwich structure. In the preferred embodiment, a wing is fabricated from a series of worksheets partial penetration welded together using a laser. The worksheets are superplastic formed to producing a wing with a different internal reinforcement at two or more locations in the wing.
摘要翻译：提供了一种超塑性夹层结构的方法。一系列工作表通过部分穿透焊接在选定的位置连接在一起。工件表随后被形成为超塑性以形成夹层结构。该方法允许在整个夹层结构中的不同点使用不同数量的工作表。这导致在夹层结构中在不同位置处具有不同内部加强件的夹层结构。在优选实施例中，翼由使用激光部分穿透焊接在一起的一系列工作表制成。工作表是超塑性的，用于在翼中的两个或更多个位置处产生具有不同内部加强件的翼。

8. 发明授权

US07818945B2 Composite structural member having an undulating web and method for forming same 有权
标题翻译：具有起伏网的复合结构件及其形成方法
公开(公告)号：US07818945B2
公开(公告)日：2010-10-26
申请号：US11541620
申请日：2006-09-29
申请人： Paul S. Gregg , Max U. Kismarton , Jeff D. Will
发明人： Paul S. Gregg , Max U. Kismarton , Jeff D. Will
IPC分类号： E04C3/00
CPC分类号： B64C1/064 , B29C65/48 , B29C65/483 , B29C65/4835 , B29C65/5057 , B29C65/56 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/742 , B29D99/0007 , B29K2105/06 , B29K2305/00 , B29K2307/00 , B29L2031/003 , B29L2031/3076 , B64C1/065 , B64C3/182 , B64C2001/0072 , E04C3/07 , E04C3/29 , E04C2003/0452 , Y02T50/43 , B29K2307/04
摘要： Composite structural members and methods for forming the same are disclosed. In one embodiment, a composite structural member includes a central structural portion that extends in a first direction and having a first flange portion and a second flange portion that are spaced apart in a second direction perpendicular to the first direction by a web portion, the web portion further including a periodic or a non-periodic undulation extending in the first direction. A first reinforced polymer-based substrate is fixedly coupled to the first flange portion, and a second reinforced polymer-based substrate is fixedly coupled to the second flange portion.
摘要翻译：公开了复合结构件及其形成方法。在一个实施例中，复合结构构件包括中心结构部分，该中心结构部分在第一方向上延伸并且具有第一凸缘部分和第二凸缘部分，所述第一凸缘部分和第二凸缘部分通过腹板部分沿垂直于第一方向的第二方向间隔开，部分还包括在第一方向上延伸的周期性或非周期性波动。第一增强的基于聚合物的基底固定地联接到第一凸缘部分，并且第二增强的基于聚合物的基底固定地联接到第二凸缘部分。

9. 发明申请

US20080040926A1 Apparatus and Method for Forming Corrugated Members 有权
标题翻译：用于形成波纹构件的装置和方法
公开(公告)号：US20080040926A1
公开(公告)日：2008-02-21
申请号：US11464650
申请日：2006-08-15
申请人： Max U. Kismarton , Paul S. Gregg , Jeff D. Will
发明人： Max U. Kismarton , Paul S. Gregg , Jeff D. Will
IPC分类号： B21D47/01
CPC分类号： B21D13/02 , Y10T29/49634
摘要： An apparatus and method for forming a stringer are provided. The stringer generally includes a web having a desired corrugated configuration and first and second flanges welded to opposite edges of the web. The apparatus includes a support structure, a strongback that is supported by the support structure, and a plurality of dies that are adjustable relative to the strongback. The strongback defines a corrugated contour surface corresponding to the desired corrugated configuration of the web. The dies define corresponding forming surfaces and are configured to be advanced toward the strongback to thereby form the web to the desired corrugated configuration between the contour surface of the strongback and the forming surfaces of the dies. Further, the apparatus can receive the flanges of the stringer in a predetermined configuration with the web so that the flanges can be welded to the web while the web is supported by the strongback and dies in the desired corrugated configuration.
摘要翻译：提供了一种用于形成纵梁的装置和方法。纵梁通常包括具有期望的波纹构造的腹板和焊接到腹板的相对边缘的第一和第二凸缘。该装置包括支撑结构，由支撑结构支撑的强力支撑件，以及可相对于强力可调节的多个模具。强力定义对应于网的期望的波纹构造的波纹轮廓表面。模具限定相应的成形表面，并且被构造成朝向强力推进，从而在强力的轮廓表面和模具的成形表面之间形成所需的波纹状结构。此外，该装置可以以带有网的预定构造接收纵梁的凸缘，使得凸缘可以被焊接到腹板上，同时腹板被强力支撑并且以期望的波纹结构模具。

10. 发明授权

US5451472A Multiple density sandwich structures and method of fabrication 失效
标题翻译：多密度夹层结构及其制造方法
公开(公告)号：US5451472A
公开(公告)日：1995-09-19
申请号：US195998
申请日：1994-02-14
申请人： Paul S. Gregg , Matthew G. Kistner , Jeff D. Will
发明人： Paul S. Gregg , Matthew G. Kistner , Jeff D. Will
IPC分类号： B21D26/055 , B23K26/20 , B64C1/00 , B64C3/20 , B64C27/473 , E04C2/32 , B32B3/28 , B32B15/00
CPC分类号： B64C1/06 , B21D26/055 , B23K26/244 , B23K26/26 , B23K26/28 , B64C1/08 , B64C27/473 , B64C3/20 , E04C2/322 , B64C2001/0072 , B64C2001/0081 , B64C2027/4736 , Y02T50/433 , Y10S72/709 , Y10T29/49339 , Y10T428/1234 , Y10T428/12347 , Y10T428/12639 , Y10T428/12806
摘要： A method to superplastic form sandwich structures is provided. A series of worksheets are joined together at selected locations through the use of partial penetration welding. The worksheets are subsequently superplastic formed in order to form a sandwich structure. The method allows a different number of worksheets to be used at different points throughout the sandwich structure. This results in a sandwich structure with a different internal reinforcement at different locations in the sandwich structure. In the preferred embodiment, a wing is fabricated from a series of worksheets partial penetration welded together using a laser. The worksheets are superplastic formed to producing a wing with a different internal reinforcement at two or more locations in the wing.
摘要翻译：提供了一种超塑性夹层结构的方法。一系列工作表通过部分穿透焊接在选定的位置连接在一起。工件表随后被形成为超塑性以形成夹层结构。该方法允许在整个夹层结构中的不同点使用不同数量的工作表。这导致在夹层结构中在不同位置处具有不同内部加强件的夹层结构。在优选实施例中，翼由使用激光部分穿透焊接在一起的一系列工作表制成。工作表是超塑性的，用于在翼中的两个或更多个位置处产生具有不同内部加强件的翼。

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