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. 发明授权

US09272769B2 Joint for composite wings 有权
标题翻译：复合翼的接头
公开(公告)号：US09272769B2
公开(公告)日：2016-03-01
申请号：US13675809
申请日：2012-11-13
申请人： The Boeing Company
发明人： Chun-Liang Lin , Ryan M Mahn , Karl B Lee
IPC分类号： B64C3/26 , B64F5/00 , B64C1/26
CPC分类号： B64C3/26 , B64C1/26 , B64F5/00 , Y10T29/49622
摘要： A wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or co-cured with a wing skin. The webbing and cap of the stringer may be trimmed to expose a noodle and base flange. The noodle and base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.
摘要翻译：包括T形弦和用于连接内侧翼板组件和外侧翼板组件的拼接板的翼接头。翼板组件包括与机翼皮肤共同粘合或共同固化的纵梁。可以修剪桁条的织带和帽子以暴露面条和底部法兰。面条和底座法兰接口与T型底架和机翼皮肤接合拼接板。暴露的面条可能与修剪后的桁条的底部法兰不冲洗。 T弦的底部可以包括用于容纳非齐平面的凹槽，使得T形弦和基底凸缘之间不存在间隙。或者，垫片可以用于补偿非冲洗面条或基底法兰，并且腹板可以包括牺牲层，允许基底法兰和腹板与面条齐平。

2. 发明授权

US08857765B2 Method and apparatus for attaching an aircraft fuselage frame to a wing box 有权
标题翻译：将飞机机身框架连接到翼盒的方法和装置
公开(公告)号：US08857765B2
公开(公告)日：2014-10-14
申请号：US13652975
申请日：2012-10-16
申请人： The Boeing Company
发明人： Grant Brian Thomas , Chun-Liang Lin , Francis E. Andrews , Wendell C. K. Choy
IPC分类号： B64C1/00
CPC分类号： B64C1/26 , Y10T29/49622
摘要： The present disclosure is generally directed to an aircraft body including a fuselage skin on an outboard member of the aircraft body and a wing box extending through a member of the aircraft body. The wing box being enclosed and capable of being pressurized is fixedly attached at an outer surface to at least one pair of an attachment member and an attachment link member that is fixedly attached to the aircraft body.
摘要翻译：本公开总体上涉及飞机主体，其包括在飞行器主体的外侧构件上的机身皮肤和延伸穿过飞行器主体的构件的翼盒。被封闭并能够被加压的翼盒在外表面固定地附接到固定地连接到飞行器主体的至少一对附接构件和连接构件。

3. 发明申请

US20140131518A1 JOINT FOR COMPOSITE WINGS 有权
标题翻译：复合网络联合
公开(公告)号：US20140131518A1
公开(公告)日：2014-05-15
申请号：US13675809
申请日：2012-11-13
申请人： The Boeing Company
发明人： Chun-Liang Lin , Ryan M. Mahn , Karl B. Lee
IPC分类号： B64C3/26 , B64F5/00
CPC分类号： B64C3/26 , B64C1/26 , B64F5/00 , Y10T29/49622
摘要： A wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or co-cured with a wing skin. The webbing and cap of the stringer may be trimmed to expose a noodle and base flange. The noodle and base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.
摘要翻译：包括T形弦和用于连接内侧翼板组件和外侧翼板组件的拼接板的翼接头。翼板组件包括与机翼皮肤共同粘合或共同固化的纵梁。可以修剪桁条的织带和帽子以暴露面条和底部法兰。面条和底座法兰接口与T型底架和机翼皮肤接合拼接板。暴露的面条可能与修剪后的桁条的底部法兰不冲洗。 T弦的底部可以包括用于容纳非齐平面的凹槽，使得T形弦和基底凸缘之间不存在间隙。或者，垫片可以用于补偿非冲洗面条或基底法兰，并且腹板可以包括牺牲层，允许基底法兰和腹板与面条齐平。

4. 发明申请

US20140103162A1 Method And Apparatus For Attaching An Aircraft Fuselage Frame To A Wing Box 有权
标题翻译：将飞机机身框架连接到机箱的方法和装置
公开(公告)号：US20140103162A1
公开(公告)日：2014-04-17
申请号：US13652975
申请日：2012-10-16
申请人： THE BOEING COMPANY
发明人： Grant Brian Thomas , Chun-Liang Lin , Francis E. Andrews , Wendell C.K. Choy
IPC分类号： B64C1/26 , B64F5/00 , B64D37/04
CPC分类号： B64C1/26 , Y10T29/49622
摘要： The present disclosure is generally directed to an aircraft body including a fuselage skin on an outboard member of the aircraft body and a wing box extending through a member of the aircraft body. The wing box being enclosed and capable of being pressurized is fixedly attached at an outer surface to at least one pair of an attachment member and an attachment link member that is fixedly attached to the aircraft body.
摘要翻译：本公开总体上涉及飞机主体，其包括在飞行器主体的外侧构件上的机身皮肤和延伸穿过飞行器主体的构件的翼盒。被封闭并能够被加压的翼盒在外表面固定地附接到固定地连接到飞行器主体的至少一对附接构件和连接构件。

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