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公开(公告)号：US09535022B1
公开(公告)日：2017-01-03
申请号：US13944571
申请日：2013-07-17
申请人： The Boeing Company
IPC分类号： G01N27/00
CPC分类号： G01N27/00 , B64F5/60 , G01N22/04 , G01N27/223
摘要： A system for detecting moisture characteristics of a material of a complex structure while the material is in situ or forms part of the complex structure. The system includes at least one moisture detection sensor positioned proximate the material of the complex structure while the material is in situ. The system also includes a controller in data receiving communication with the moisture detection sensor.
摘要翻译： 一种用于在材料就地或形成复杂结构的一部分时检测复合结构材料的水分特性的系统。 该系统包括至少一个位于复合结构材料附近的水分检测传感器，同时材料在原位。 该系统还包括与湿度检测传感器进行数据接收通信的控制器。
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公开(公告)号：US20150273761A1
公开(公告)日：2015-10-01
申请号：US14736148
申请日：2015-06-10
申请人： The Boeing Company
CPC分类号： B29C66/91221 , B23K26/0006 , B23K26/032 , B23K26/082 , B23K26/352 , B23K2101/34 , B23K2103/16 , B23K2103/38 , B23K2103/42 , B29C66/91411 , B29C73/10 , B29C73/34 , B29C2035/0838 , B29L2031/3076
摘要： A machine and process for a heating system for a composite patch comprising a light beam and a controller. The controller is configured to command the light beam to heat the resin in the composite patch to a desired level for curing while avoiding overheating a fiber in the composite patch.
摘要翻译： 一种用于复合贴片加热系统的机器和方法，包括光束和控制器。 控制器被配置为命令光束将复合贴片中的树脂加热到所需的固化水平，同时避免复合贴片中的纤维过热。
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公开(公告)号：US11047745B2
公开(公告)日：2021-06-29
申请号：US14966878
申请日：2015-12-11
申请人： The Boeing Company
摘要： According to an embodiment, a heat detection system includes a graphene conductor, a housing containing the graphene conductor; and, a signal wire connected in electrical communication with the graphene conductor, the signal wire having a length that extends from the housing.
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公开(公告)号：US09995288B2
公开(公告)日：2018-06-12
申请号：US15009223
申请日：2016-01-28
申请人： The Boeing Company
IPC分类号： F03G7/06 , B64C13/30 , F16G1/20 , G05D23/275
CPC分类号： F03G7/065 , B64C13/30 , F16G1/20 , G05D23/27535
摘要： Described herein is a motor comprising a first rotatable member and an anchor, spaced apart from the first rotatable member. The motor also comprises a belt, in tension about the first rotatable member and the anchor. The belt is co-rotatably engaged with the first rotatable member. Further, the belt is made from a shape-memory alloy. Additionally, the motor comprises a thermal regulation device, positioned between spaced-apart first and second portions of the belt. The thermal regulation device is also configured to concurrently cool the first portion of the belt to contract the first portion of the belt and heat the second portion of the belt to expand the second portion of the belt. Concurrent contraction and expansion of the first and second portions of the belt cause rotation of the belt.
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5.发明申请METHODS AND SYSTEMS FOR DETERMINING OPTICAL PROPERTIES FOR LIGHT TRANSMITTED MEDIUMS 审中-公开用于确定光传输介质的光学性质的方法和系统公开(公告)号：US20150362402A1
公开(公告)日：2015-12-17
申请号：US14301686
申请日：2014-06-11
申请人： THE BOEING COMPANY
CPC分类号： G01M11/0228 , G01B11/0625 , G01J3/28 , G01J3/42 , G01M11/005 , G01N21/55 , G01N21/59
摘要： Methods and systems for determining optical properties for light transmitted mediums are provided. One method includes acquiring one or more measured values indicative of a reflectance for a material, acquiring one or more measured values indicative of a transmittance for the material, and determining a set of calculated values for an index of refraction coefficient and an extinction coefficient from the one or more measured values indicative of reflectance and transmittance, respectively. The method includes identifying a calculated value from the set of calculated values for the index of refraction coefficient and a calculated value from the set of calculated values for the extinction coefficient that are within a threshold determined by the difference between the one or more measured values indicative of the reflectance or transmittance and a predicted reflectance or transmittance, respectively. The method includes determining a reflectance and transmittance for the material using the calculated values.
摘要翻译： 提供了用于确定光透射介质光学特性的方法和系统。 一种方法包括获取指示材料的反射率的一个或多个测量值，获取表示材料的透射率的一个或多个测量值，以及确定来自所述材料的折射系数和消光系数的计算值的集合 分别表示反射率和透射率的一个或多个测量值。 该方法包括从针对折射系数的计算值的集合中识别计算值，以及从消光系数的计算值的集合中计算出的值在由一个或多个测量值之间的差确定的阈值内 的反射率或透射率以及预测的反射率或透射率。 该方法包括使用所计算的值确定材料的反射率和透射率。
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公开(公告)号：US10160163B2
公开(公告)日：2018-12-25
申请号：US14736148
申请日：2015-06-10
申请人： The Boeing Company
IPC分类号： B29C65/00 , B23K26/00 , B23K26/03 , B29C73/10 , B29C73/34 , B23K26/082 , B29L31/30 , B29C35/08 , B23K101/34 , B23K103/16 , B23K103/00
摘要： A machine and process for a heating system for a composite patch comprising a light beam and a controller. The controller is configured to command the light beam to heat the resin in the composite patch to a desired level for curing while avoiding overheating a fiber in the composite patch.
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公开(公告)号：US20180321134A1
公开(公告)日：2018-11-08
申请号：US15585096
申请日：2017-05-02
申请人： The Boeing Company
摘要： A bondline characteristic determination system comprises a plurality of graphene sensors and a plurality of graphene lines. The plurality of graphene sensors is positioned within a bondline of a composite structure. The plurality of graphene sensors is formed of graphene doped with a noble gas. The plurality of graphene lines electrically connects the plurality of graphene sensors external to the composite structure.
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公开(公告)号：US20180288832A1
公开(公告)日：2018-10-04
申请号：US15477289
申请日：2017-04-03
申请人： The Boeing Company
摘要： An electronic dimmable window is heated by a graphene heating element formed on a transparent panel aligned with and proximal to the electronic dimmable window. The heating element is controlled by a thermostatic control circuit printed on the transparent panel.
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公开(公告)号：US20170167925A1
公开(公告)日：2017-06-15
申请号：US14966878
申请日：2015-12-11
申请人： The Boeing Company
CPC分类号： G01K7/24 , G01K1/08 , G01K3/005 , G01K2211/00
摘要： According to an embodiment, a heat detection system includes a graphene conductor, a housing containing the graphene conductor; and, a signal wire connected in electrical communication with the graphene conductor, the signal wire having a length that extends from the housing.
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10.发明授权公开(公告)号：US09664183B2
公开(公告)日：2017-05-30
申请号：US14593106
申请日：2015-01-09
申请人： THE BOEING COMPANY
发明人： Sahrudine Apdalhaliem , Moushumi Shome , Kimberly D. Meredith , Waeil M. Ashmawi , Morteza Safai , Frederick T. Calkins
摘要： Aspects of the present disclosure generally relate to an SMA actuator that includes a cooling device disposed within a torque tube. In one aspect, the cooling device includes a sliding sleeve, an expandable sleeve, and plurality of cooling fins coupled to the expandable sleeve. Axial movement of the sliding sleeve relative to the expandable sleeve facilitates radial expansion of the expandable sleeve and urges the cooling fins into contact with the torque tube. The cooling fins function as heat sinks when in contact with the torque tube to facilitate the removal of heat from the torque tube to increase the cooling rate of the torque tube. During heating of the torque tube, the cooling fins may be spaced apart from the torque tube to reduce the thermal mass that is heated, thus increasing the heating rate of the torque tube.
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