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31. 发明授权

US2986247A Heat insulation 失效
标题翻译：绝热
公开(公告)号：US2986247A
公开(公告)日：1961-05-30
申请号：US58607256
申请日：1956-05-21
申请人： BELL AEROSPACE CORP
发明人： ARTHUR SCHNITT , DE LORENZI EZIO P
IPC分类号： B64C1/38
CPC分类号： B64C1/38

32. 发明申请

US20180362135A1 PANEL FOR A VEHICLE AND METHOD OF MANUFACTURING A PANEL 审中-公开
公开(公告)号：US20180362135A1
公开(公告)日：2018-12-20
申请号：US15628092
申请日：2017-06-20
申请人： THE BOEING COMPANY
发明人： Marc STOROZUK
IPC分类号： B64C1/12 , B64C1/06 , B64C1/38
CPC分类号： B64C1/12 , B64C1/061 , B64C1/069 , B64C1/38 , B64C2001/0045 , B64C2001/0072
摘要： A panel for a vehicle and a method for manufacturing the panel are provided. One panel has two sides forming a corner having a profile that is substantially non-orthogonal and a substructure is provided having a protrusion extending from a body of the substructure towards a surface of the panel. The protrusion has a profile extending along an edge thereof that substantially matches the profile of the corner of the panel such that the protrusion and the corner of the panel form a gap therebetween when the panel is mounted to the substructure

33. 发明授权

US09994301B2 Virtual aerodynamic surface systems 有权
公开(公告)号：US09994301B2
公开(公告)日：2018-06-12
申请号：US14083077
申请日：2013-11-18
申请人： ROHR, INC.
发明人： Teresa M. Kruckenberg , Vijay V. Pujar , Robert L. Braden
IPC分类号： B64C1/00 , B64C1/38 , B64C21/00 , B64C23/00
CPC分类号： B64C1/38 , B64C21/00 , B64C23/005 , B64C2220/00 , B64C2230/02 , Y02T50/166
摘要： A method of generating a pressure wave proximate an airflow surface and altering airflow to promote a localized lowering of skin friction over the airflow surface is described herein. A series of pressure waves may be configured to create a virtual riblet to control turbulent vortices in a boundary layer adjacent to the airflow surface creating a virtual riblet. The pressure waves may be configured to prevent disruption of the flow of air relative to at least one of a step or a gap associated with the airflow surface. The pressure wave generating system may be comprised of at least one of a thermoacoustic material, a piezoelectric material and a semiconductor material, and a microelectric circuit.

34. 发明授权

US09856011B2 Method for the joining of wings or control surfaces to an airplane fuselage 有权
公开(公告)号：US09856011B2
公开(公告)日：2018-01-02
申请号：US14819792
申请日：2015-08-06
申请人： The Boeing Company
发明人： Richard P. Topf , Jonathan D. Embler , Thomas R. Pinney
IPC分类号： B64C1/06 , B64C1/38 , B64C1/26 , B64C9/02 , B64C30/00
CPC分类号： B64C1/38 , B64C1/26 , B64C9/02 , B64C30/00 , Y02T50/44
摘要： Methods of joining a first aerostructure part with a second aerostructure part are disclosed, for example, methods of joining an airplane wing or control surface to an airplane fuselage or joining fins to a rocket body. The method comprises aligning a plurality of connection elements in a linear array within the second aerostructure part, wherein the connection elements comprise a plurality of flexible connection elements and at least one rigid connection element, and attaching the first aerostructure part to the second aerostructure part at a plurality of connection points with the plurality of connection elements. The second aerostructure part expands linearly at a greater rate when exposed to heat than the first aerostructure part resulting in a difference in linear distance between the first aerostructure part and the second aerostructure part and the flexible connection elements are configured to flex to accommodate for this linear distance difference.

35. 发明申请

US20160207606A1 AIRCRAFT AND FUSELAGE COOLING STRUCTURE 审中-公开
标题翻译：飞机和熔炉冷却结构
公开(公告)号：US20160207606A1
公开(公告)日：2016-07-21
申请号：US14962748
申请日：2015-12-08
申请人： MITSUBISHI AIRCRAFT CORPORATION
发明人： Nobuhide HARA , Osamu YAMADA
IPC分类号： B64C1/38 , B64C7/00 , B64C1/06
CPC分类号： B64C1/38 , B64C7/00 , B64D13/00 , Y02T50/56
摘要： Under constraints on the space and the weight of an aircraft, the present invention aims to protect structural members from a heat generation part. An aircraft includes: a fuselage; an air conditioning pack installed on the outside of a lower part of the fuselage; a fairing covering the air conditioning pack; an outer heat insulation material disposed in a region of the fuselage, which corresponds to the air conditioning pack, from the outside of the fuselage; and an inner heat insulation material disposed around the region on the inside of the fuselage.
摘要翻译：在对飞机的空间和重量的限制下，本发明旨在保护结构构件免受发热部分的影响。飞机包括：机身; 安装在机身下部外侧的空调组件; 整流罩覆盖空调包装; 设置在机身的与机身外侧对应的机身的区域的外部隔热材料; 以及设置在机身内侧的区域周围的内部隔热材料。

36. 发明申请

US20160169256A1 METHOD AND ASSEMBLY FOR ATTACHING COMPONENTS 审中-公开
标题翻译：连接组件的方法和装配
公开(公告)号：US20160169256A1
公开(公告)日：2016-06-16
申请号：US15041522
申请日：2016-02-11
申请人： United Technologies Corporation
发明人： Wendell V. Twelves , Kathleen E. Sinnamon
IPC分类号： F16B5/02 , B64C1/06 , B64F5/00
CPC分类号： F16B5/0241 , B64C1/06 , B64C1/38 , B64C9/02 , B64F5/00 , Y10T29/49826 , Y10T403/21 , Y10T403/217
摘要： An exemplary method of adjustably mounting a first component to a second component includes, among other things, securing the first component to the second component with a linking member, and selectively adjusting the temperature of a variable portion of the linking member to change a size of the linking member.
摘要翻译：将第一部件可调节地安装到第二部件的示例性方法包括除其他之外，通过连接部件将第一部件固定到第二部件，并且选择性地调节连接部件的可变部分的温度以改变连接部件的尺寸连接构件。

37. 发明授权

US09283711B1 Hybrid ablative thermal protection systems and associated methods 有权
标题翻译：混合烧蚀热保护系统及相关方法
公开(公告)号：US09283711B1
公开(公告)日：2016-03-15
申请号：US12550793
申请日：2009-08-31
申请人： Bryan Clark Brewer , Patrick Jacob Mobers
发明人： Bryan Clark Brewer , Patrick Jacob Mobers
IPC分类号： B29C65/48
CPC分类号： B64G1/58 , B29C65/4835 , B64C1/38 , B64G1/62
摘要： A method of forming a thermal protection system for high speed aircraft is described. The method includes mechanically working an uncured ablator material into a first surface of a felt layer such that the ablator material penetrates a distance into a thickness of the felt layer thereby forming an region that has a mixture of felt and ablator material, adding additional uncured ablator material to the worked ablator material, and curing the combined ablator material.
摘要翻译：描述了形成用于高速飞行器的热保护系统的方法。该方法包括将未固化的消融器材料机械加工到毡层的第一表面中，使得消融器材料穿过一定距离进入毡层的厚度，从而形成具有毡和烧结材料混合物的区域，添加另外未固化的烧烤器材料到工作的消融器材料，并固化组合的消融器材料。

38. 发明授权

US08960601B2 Aircraft cooling duct 有权
标题翻译：飞机冷却管道
公开(公告)号：US08960601B2
公开(公告)日：2015-02-24
申请号：US12093157
申请日：2006-11-07
申请人： Victor John Willdig , Kim Sharp
发明人： Victor John Willdig , Kim Sharp
IPC分类号： B64C1/38
CPC分类号： B64C1/38 , B64C1/12 , B64C3/26 , B64C3/36 , B64C13/50 , B64D13/006
摘要： An aircraft structure, for example a wing, includes a section of skin, for example a lower wing panel, the panel defining an external (lower) surface that in use is on the exterior of the aircraft and an internal (upper) surface opposite the external surface, and a duct comprising a section of duct for transporting cooling fluid, for example air, between the internal and external surfaces of the panel from a first location in the panel to a second location that is spaced apart from the first location in a direction substantially parallel to the external surface of the panel. The cooling air cools an electronic hydrostatic actuator (EHA 4b) in the wing 2.
摘要翻译：飞机结构，例如机翼，包括皮肤部分，例如下翼板，所述面板限定在使用中在飞机外部的外部（下）表面，以及与飞机相对的内部（上）表面外表面和管道，其包括用于将面板的内表面和外表面之间的冷却流体（例如空气）从面板中的第一位置传送到与第一位置间隔开的第二位置的管道方向基本上平行于面板的外表面。冷却空气冷却机翼2中的电子静液压致动器（EHA 4b）。

39. 发明申请

US20140332631A1 AMORPHOUS METAL RIBLETS 有权
标题翻译：非晶金属蛋白
公开(公告)号：US20140332631A1
公开(公告)日：2014-11-13
申请号：US14070183
申请日：2013-11-01
申请人： The Boeing Company
发明人： Diane C. Rawlings , Stephen Christensen
IPC分类号： B64C21/10 , B32B15/08 , B32B3/30 , F15D1/00 , B64C1/38
CPC分类号： B64C21/10 , B32B3/08 , B32B3/30 , B32B7/12 , B32B15/08 , B32B15/20 , B32B25/08 , B32B27/283 , B32B27/288 , B32B27/34 , B32B27/38 , B32B27/40 , B32B2250/02 , B32B2307/416 , B32B2307/50 , B32B2307/702 , B32B2605/18 , B64C1/38 , B64C2230/26 , F15D1/0035 , F15D1/004 , Y02T50/166 , Y10T428/24355 , Y10T428/24612
摘要： An array of aerodynamic riblets is created by a plurality of high stiffness tips with a layer supporting the tips in predetermined spaced relation and adhering the tips to a vehicle surface.
摘要翻译：空气动力肋的阵列由多个高刚度尖端产生，其具有以预定的间隔关系支撑尖端的层并且将尖端附接到车辆表面。

40. 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。

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