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1. 发明授权

US11472431B1 Visual warning assembly 有权
公开(公告)号：US11472431B1
公开(公告)日：2022-10-18
申请号：US17165709
申请日：2021-02-02
申请人： David Mark Stewart
发明人： David Mark Stewart
IPC分类号： G08B21/00 , B60W50/14 , H04W4/46 , B62J50/22
摘要： A visual warning assembly, configured to make a warning from one vehicle to another vehicle. The visual warning assembly has a case with a front face joined to a base and an antenna. A channel display window, a channel selector button, a power button, a green lighted button, a yellow lighted button and a red lighted button, arranged on the front face. A mounting ball is magnetically joined to the base. A microcontroller is electrically coupled to the green lighted button, the yellow lighted button, and the red lighted button. The microcontroller is programmed with instructions to: receive a communication from a second visual warning assembly. Then, engage one member of a lighted button set consisting of the red button, the yellow button, and the green button creating an indicating light. Finally, receiving a signal from a user making the indicating light an activated button.

2. 发明申请

US20110233338A1 JOINT 审中-公开
标题翻译：联合
公开(公告)号：US20110233338A1
公开(公告)日：2011-09-29
申请号：US13037404
申请日：2011-03-01
申请人： David Mark STEWART
发明人： David Mark STEWART
IPC分类号： B64C3/00 , B64C1/00 , B23P11/00 , B23P17/00
CPC分类号： B64C3/28 , Y10T29/49771 , Y10T29/49826
摘要： A joint between an aircraft wing box cover and a leading/trailing edge structure, the cover and the structure having flush aerodynamic outer surfaces, wherein the structure has an integrally formed land that extends over an inner surface of the cover, and the land of the structure is fastened to the cover. Also a method of forming the joint.
摘要翻译：飞机翼盒盖与前缘/后缘结构之间的接头，盖和结构具有冲洗的空气动力学外表面，其中该结构具有在盖的内表面上延伸的整体形成的平台，结构固定在盖上。也是形成接头的方法。

3. 发明申请

US20110186690A1 BRIDGING SEAL 有权
标题翻译：桥接密封
公开(公告)号：US20110186690A1
公开(公告)日：2011-08-04
申请号：US13018537
申请日：2011-02-01
申请人： David Mark STEWART
发明人： David Mark STEWART
IPC分类号： B64C3/50 , B64C1/38 , B23P17/00
CPC分类号： B23P17/00 , B64C1/38 , B64C3/50 , B64C7/00 , B64C9/02 , Y10T29/49622
摘要： A bridging seal comprising a stack of two or more layers of elastomer, the bridging seal having a first edge and a second edge opposite the first edge, adjacent layers being attached to each other at the first and second edges, wherein adjacent layers of the bridging seal have opposing surfaces and a substantial portion of the opposing surfaces is unbonded. The bridging seal may be used to seal a gap between two aerodynamic surfaces on an aircraft.
摘要翻译：桥接密封件包括两层或更多层弹性体的叠层，所述桥接密封件具有第一边缘和与所述第一边缘相对的第二边缘，相邻层在所述第一边缘和第二边缘处彼此附接，其中所述桥接密封件具有相对的表面，并且相对表面的大部分是未粘合的。桥接密封件可用于密封飞机上的两个空气动力学表面之间的间隙。

4. 发明授权

US07748661B2 Aircraft structure and a fastener for use therewith 失效
标题翻译：飞机结构和与其一起使用的紧固件
公开(公告)号：US07748661B2
公开(公告)日：2010-07-06
申请号：US11613807
申请日：2006-12-20
申请人： Andrew James Harris , David Mark Stewart
发明人： Andrew James Harris , David Mark Stewart
IPC分类号： B64C1/12
CPC分类号： B64C1/12 , F16B19/00
摘要： An aircraft structure, for example a wing (20), includes a structural skeleton having structural elements (for example, spars (60) and ribs (70)) enclosed within a skin (200). A fastener (110a,b) is fastened to the skeleton and wholly within the skin (200). The fastener (110a,b) fastens to the structure (20) a bracket (120) for carrying stores (80). The fastener (110a,b) includes a body (300) defining an internal bore (230). The body (300) includes an internal threaded region (330), within the internal bore (230), for fastening the bracket (120) to the aircraft structure (20).
摘要翻译：飞机结构，例如翼（20），包括具有封闭在皮肤（200）内的结构元件（例如，翼梁（60）和肋（70））的结构骨架。紧固件（110a，b）被紧固到骨架上并且完全在皮肤（200）内。紧固件（110a，b）紧固到结构（20）上用于携带存储（80）的托架（120）。紧固件（110a，b）包括限定内孔（230）的主体（300）。主体（300）包括在内孔（230）内的内螺纹区域（330），用于将支架（120）紧固到飞机结构（20）。

5. 发明授权

US08376278B2 Cover trailing edge profile 有权
标题翻译：盖后缘轮廓
公开(公告)号：US08376278B2
公开(公告)日：2013-02-19
申请号：US12897988
申请日：2010-10-05
申请人： David Mark Stewart
发明人： David Mark Stewart
IPC分类号： B64C3/00
CPC分类号： B64C3/26 , B64C3/28 , Y10T29/49826
摘要： An aircraft wing assembly, comprising a front spar, a rear spar, and upper and lower wing covers extending between the front and rear spars, wherein the upper and/or lower wing cover overhangs the rear spar and has a non-linear trailing edge profile forming an array of tabs and cut-outs. Also, a method of assembling the aircraft wing.
摘要翻译：一种飞机机翼组件，包括前翼梁，后翼梁以及在前后翼梁之间延伸的上下翼翼盖，其中上翼和/或下翼盖悬挂在后翼梁上，并且具有非线性后缘轮廓形成一系列标签和切口。另外，组装飞机机翼的方法。

6. 发明授权

US08876051B2 Bridging seal 有权
标题翻译：桥接密封
公开(公告)号：US08876051B2
公开(公告)日：2014-11-04
申请号：US13018537
申请日：2011-02-01
申请人： David Mark Stewart
发明人： David Mark Stewart
IPC分类号： B64C9/02 , B64C7/00 , B64C3/50 , B64C1/38 , B23P17/00
CPC分类号： B23P17/00 , B64C1/38 , B64C3/50 , B64C7/00 , B64C9/02 , Y10T29/49622
摘要： A bridging seal comprising a stack of two or more layers of elastomer, the bridging seal having a first edge and a second edge opposite the first edge, adjacent layers being attached to each other at the first and second edges, wherein adjacent layers of the bridging seal have opposing surfaces and a substantial portion of the opposing surfaces is unbonded. The bridging seal may be used to seal a gap between two aerodynamic surfaces on an aircraft.
摘要翻译：桥接密封件包括两层或更多层弹性体的叠层，所述桥接密封件具有第一边缘和与所述第一边缘相对的第二边缘，相邻层在所述第一边缘和第二边缘处彼此附接，其中所述桥接密封件具有相对的表面，并且相对表面的大部分是未粘合的。桥接密封件可用于密封飞机上的两个空气动力学表面之间的间隙。

7. 发明申请

US20110095133A1 COVER TRAILING EDGE PROFILE 有权
标题翻译：盖子拖车边缘剖面
公开(公告)号：US20110095133A1
公开(公告)日：2011-04-28
申请号：US12897988
申请日：2010-10-05
申请人： David Mark STEWART
发明人： David Mark STEWART
IPC分类号： B64C3/10 , B64C3/18 , B23P11/00
CPC分类号： B64C3/26 , B64C3/28 , Y10T29/49826
摘要： An aircraft wing assembly, comprising a front spar, a rear spar, and upper and lower wing covers extending between the front and rear spars, wherein the upper and/or lower wing cover overhangs the rear spar and has a non-linear trailing edge profile forming an array of tabs and cut-outs. Also, a method of assembling the aircraft wing.
摘要翻译：一种飞机机翼组件，包括前翼梁，后翼梁以及在前后翼梁之间延伸的上下翼翼盖，其中上翼和/或下翼盖悬挂在后翼梁上，并且具有非线性后缘轮廓形成一系列标签和切口。另外，组装飞机机翼的方法。

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