专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20200002010A1 COMPOSITE AEROSTRUCTURE WITH INTEGRATED HEATING ELEMENT 审中-公开
公开(公告)号：US20200002010A1
公开(公告)日：2020-01-02
申请号：US16564108
申请日：2019-09-09
申请人： TRIUMPH AEROSTRUCTURES, LLC.
发明人： Kyle B. Hardman , Mark A. Calder , Ian C. Derx
IPC分类号： B64D15/12 , H05B3/14 , H05B3/28 , B29C70/88 , B64D15/22
摘要： A heated composite structure and a method for forming a heated composite structure. The structure includes carbon fibers embedded within a thermoplastic matrix. The carbon fibers are connected with first and second electrodes that are configured to be connected with an electric source such that applying current to the electrodes causes current to flow through the embedded carbon fibers to provide resistive heating sufficient to heat the composite structure to impede formation of ice on the composite structure.

2. 发明申请

US20190322375A1 COMPOSITE AEROSTRUCTURE WITH INTEGRATED HEATING ELEMENT 审中-公开
公开(公告)号：US20190322375A1
公开(公告)日：2019-10-24
申请号：US16393519
申请日：2019-04-24
申请人： TRIUMPH AEROSTRUCTURES, LLC.
发明人： Kyle B. Hardman , Mark A. Calder , Ian C. Derx
IPC分类号： B64D15/12 , B64D15/22 , B29C70/88 , H05B3/14 , H05B3/28
摘要： A heated composite structure and a method for forming a heated composite structure. The structure includes carbon fibers embedded within a thermoplastic matrix. The carbon fibers are connected with first and second electrodes that are configured to be connected with an electric source such that applying current to the electrodes causes current to flow through the embedded carbon fibers to provide resistive heating sufficient to heat the composite structure to impede formation of ice on the composite structure.

3. 发明授权

US09254539B2 Manufacturing system 有权
标题翻译：制造系统
公开(公告)号：US09254539B2
公开(公告)日：2016-02-09
申请号：US14691254
申请日：2015-04-20
申请人： Triumph Aerostructures, LLC
发明人： Laszlo Ferenczi , Gary Pekar
IPC分类号： B23P21/00 , B64F5/00
CPC分类号： B23P21/004 , B23P2700/01 , B64F5/10 , Y10T29/534
摘要： A manufacturing system is provided comprising a plurality of work stations having one or more tools for processing a work item, at least one carrier for moving a work item among the plurality of work stations, and a platform for connecting the plurality of work stations. In a further embodiment, at least one of the plurality of work stations is not on a line with the other work stations and may include a lift machine for raising and/or lowering the at least one carrier and the work item. The platform also may preferably comprise at least one rotator for changing the direction of movement of the at least one carrier on the platform. The system also may preferably comprise at least one conveyer for transporting the at least one carrier to the platform.
摘要翻译：提供一种制造系统，包括具有用于处理工件的一个或多个工具的多个工作站，用于移动多个工作站中的工件的至少一个承载件和用于连接多个工作站的平台。在另一个实施例中，多个工作站中的至少一个工作站不与其他工作站在一条直线上，并且可以包括用于升高和/或降低至少一个承载件和工件的升降机。平台还可以优选地包括至少一个用于改变平台上的至少一个托架的移动方向的旋转器。该系统还可以优选地包括用于将至少一个载体运送到平台的至少一个输送器。

4. 发明申请

US20150224614A1 MANUFACTURING SYSTEM 有权
标题翻译：制造系统
公开(公告)号：US20150224614A1
公开(公告)日：2015-08-13
申请号：US14691254
申请日：2015-04-20
申请人： Triumph Aerostructures, LLC
发明人： Laszlo Ferenczi , Gary Pekar
IPC分类号： B23P21/00 , B64F5/00
CPC分类号： B23P21/004 , B23P2700/01 , B64F5/10 , Y10T29/534
摘要： A manufacturing system is provided comprising a plurality of work stations having one or more tools for processing a work item, at least one carrier for moving a work item among the plurality of work stations, and a platform for connecting the plurality of work stations. In a further embodiment, at least one of the plurality of work stations is not on a line with the other work stations and may include a lift machine for raising and/or lowering the at least one carrier and the work item. The platform also may preferably comprise at least one rotator for changing the direction of movement of the at least one carrier on the platform. The system also may preferably comprise at least one conveyer for transporting the at least one carrier to the platform.
摘要翻译：提供一种制造系统，包括具有用于处理工件的一个或多个工具的多个工作站，用于移动多个工作站中的工件的至少一个承载件和用于连接多个工作站的平台。在另一个实施例中，多个工作站中的至少一个工作站不与其他工作站在一条直线上，并且可以包括用于升高和/或降低至少一个承载件和工件的升降机。平台还可以优选地包括至少一个用于改变平台上的至少一个托架的移动方向的旋转器。该系统还可以优选地包括用于将至少一个载体运送到平台的至少一个输送器。

5. 发明申请

US20190337261A1 THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE 审中-公开
公开(公告)号：US20190337261A1
公开(公告)日：2019-11-07
申请号：US16402780
申请日：2019-05-03
申请人： TRIUMPH AEROSTRUCTURES, LLC.
发明人： Mark A. Calder , John F. Ellis , William David Dennison , Martin A. Wimmer , Earl L. Stone, III
IPC分类号： B32B5/26 , B64C3/20 , B32B3/30 , B32B5/02 , B32B37/06 , B64C3/26 , B64C3/18
摘要： A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.

6. 发明申请

US20160121536A1 Dynamically Engineered Radius Extruding Device and Methods of Using the Same 审中-公开
标题翻译：动力工程半径挤压装置及其使用方法
公开(公告)号：US20160121536A1
公开(公告)日：2016-05-05
申请号：US14930716
申请日：2015-11-03
申请人： Triumph Aerostructures, LLC
发明人： Ian Conrad Derx , John Ellis
IPC分类号： B29C47/12 , B29C47/00
CPC分类号： B29C48/30 , B29C48/0021 , B29C48/12 , B29C48/2528 , B29C48/2562 , B29C48/2566 , B29C48/301 , B29C48/302 , B29K2105/06 , B29K2105/253
摘要： Devices and methods for shaping and extruding void filling materials are provided.
摘要翻译：提供了用于成形和挤出空隙填充材料的装置和方法。

7. 发明申请

US20200001569A1 THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE 审中-公开
公开(公告)号：US20200001569A1
公开(公告)日：2020-01-02
申请号：US16557107
申请日：2019-08-30
申请人： TRIUMPH AEROSTRUCTURES, LLC.
发明人： Mark A. Calder , John F. Ellis , William David Dennison , Martin A. Wimmer , Earl L. Stone, III
IPC分类号： B32B5/26 , B32B3/30 , B32B37/06 , B64C3/26 , B64C3/20 , B32B5/02 , B64C3/18
摘要： A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.

8. 发明申请

US20180345346A1 METHOD FOR FORMING A METAL BEAM OR STRINGER 审中-公开
公开(公告)号：US20180345346A1
公开(公告)日：2018-12-06
申请号：US16055915
申请日：2018-08-06
申请人： Triumph Aerostructures, LLC
发明人： Harold M. Brewer, JR. , Steven McDonough , Charles Phy , David Rose , Brian Travis , Keith Willhite
IPC分类号： B21D5/04 , B21D7/03 , B21D7/00 , B21D53/92
CPC分类号： B21D5/04 , B21D7/00 , B21D7/03 , B21D53/92
摘要： A method for forming a metal beam may comprise: clamping first and second portions of the metal beam in a substantially fixed and in a position whereat the metal beam is rotatable about three axes; applying a net bending force to the clamped second portion of the metal beam at a predetermined angle; sensing twisting of the second portion of the metal beam resulting from the net bending force; and modulating the angle at which the net force is applied to reduce the twisting of the metal beam. As a result, the net bending force is moved toward the shear center and toward being along the principal axis of the metal beam.

9. 发明授权

US10052670B2 Stringer forming device and methods of using the same 有权
公开(公告)号：US10052670B2
公开(公告)日：2018-08-21
申请号：US14851498
申请日：2015-09-11
申请人： Triumph Aerostructures, LLC
发明人： Harold M. Brewer, Jr. , Steven McDonough , Charles Phy , David Rose , Brian Travis , Keith Willhite
IPC分类号： B21D7/00 , B21D5/04 , B21D7/03 , B21D53/92
CPC分类号： B21D5/04 , B21D7/00 , B21D7/03 , B21D53/92
摘要： An apparatus for bending metal beams and methods of using the same are provided herein.

10. 发明授权

US11440288B2 Thermoplastic aerostructure with localized ply isolation and method for forming aerostructure 有权
公开(公告)号：US11440288B2
公开(公告)日：2022-09-13
申请号：US16557107
申请日：2019-08-30
申请人： TRIUMPH AEROSTRUCTURES, LLC.
发明人： Mark A. Calder , John F. Ellis , William David Dennison , Martin A. Wimmer , Earl L. Stone, III
IPC分类号： B32B3/00 , B32B5/00 , B32B37/00 , B29C65/00 , B64C3/00 , B32B5/26 , B64C3/20 , B32B3/30 , B32B5/02 , B64C3/26 , B64C3/18 , B32B37/06 , B29C65/02 , B29C65/18 , B29C65/30 , B29C65/32
摘要： A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式