-
公开(公告)号：US20150306859A1
公开(公告)日：2015-10-29
申请号：US14795209
申请日：2015-07-09
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Mark A. Negley , Marc J. Piehl , Kay Y. Blohowiak , Alan E. Landmann , Richard H. Bossi , Robert L. Carlsen , Gregory Alan Foltz , Geoffrey A. Butler , Liam S. Cavanaugh Pingree , Stephen G. Moore , John Mark Gardner , Robert A. Anderson
CPC classification number: B32B37/144 , B29C73/10 , B32B3/06 , B32B7/12 , B32B15/00 , B32B15/08 , B32B19/02 , B32B27/00 , B32B2250/42 , B32B2260/021 , B32B2305/08 , B32B2307/202 , B32B2307/204 , B32B2307/54 , B32B2307/558 , B32B2311/00 , B32B2398/00 , B32B2405/00 , B32B2605/18 , Y10T29/49208 , Y10T29/49885 , Y10T156/10 , Y10T428/24752 , Y10T428/31678
Abstract: A method of forming a molybdenum composite hybrid laminate is disclosed. The method includes treating a surface of each of a plurality of molybdenum foil layers. The method further includes interweaving the surface treated molybdenum foil layers with a plurality of composite material layers. The method further includes bonding with an adhesive layer each of the surface treated molybdenum foil layers to adjacent composite material layers to form a molybdenum composite hybrid laminate having improved yield strength.
Abstract translation: 公开了一种形成钼复合混合层压板的方法。 该方法包括处理多个钼箔层中的每一个的表面。 该方法还包括用多个复合材料层交织经表面处理的钼箔层。 该方法还包括将每个表面处理的钼箔层的粘合剂层粘合到相邻的复合材料层，以形成具有改进的屈服强度的钼复合混合层合物。
-
公开(公告)号：US12247136B2
公开(公告)日：2025-03-11
申请号：US17450201
申请日：2021-10-07
Applicant: The Boeing Company
Inventor： Bart Stevens , Kay Y. Blohowiak , Christopher Garnier
IPC: C09D5/14 , A01N25/10 , A01N59/16 , A01P1/00 , C09D5/22 , C09D7/45 , C09D183/06 , C09D183/08
Abstract: An antimicrobial coating composition is disclosed. The antimicrobial coating composition also includes a polymer having a plurality of alkene units and a plurality of macroCTA polymer units. The composition also includes one or more reactive silanes, one or more wetting agents, and one or more solvents. A method for applying an antimicrobial coating composition is disclosed. The method for applying an antimicrobial coating composition may include contacting a polymer, one or more wetting agents, one or more solvents, and one or more reactive silanes with one another to prepare an antimicrobial coating composition, homogenizing the antimicrobial coating composition, applying the antimicrobial coating composition to a substrate, and allowing the antimicrobial coating composition to dry at ambient conditions.
-
23.发明申请公开(公告)号：US20200307157A1
公开(公告)日：2020-10-01
申请号：US16365431
申请日：2019-03-26
Applicant: The Boeing Company
Inventor： Kay Y. Blohowiak , Denise A. Blohowiak , James M. Kestner
Abstract: There is provided a laminated hybrid metallized polymer film for erosion protection of a composite structure. The laminated hybrid metallized polymer film includes a metal foil layer, a laminating adhesive layer underlying the metal foil layer, and a polymer film layer underlying the laminating adhesive layer. The polymer film layer is laminated to the metal foil layer with the laminating adhesive layer coupled between the metal foil layer and the polymer film layer. The laminated hybrid metallized polymer film further includes an adhesive layer underlying the polymer film layer. The adhesive layer adheres the polymer film layer to a substrate surface of the composite structure. The metal foil layer, the laminating adhesive layer, the polymer film layer, and the adhesive layer form the laminated hybrid metallized polymer film for application over and to the substrate surface of the composite structure.
-
24.发明授权公开(公告)号：US10265923B2
公开(公告)日：2019-04-23
申请号：US15465029
申请日：2017-03-21
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , John B. Moser , Brett I. Lyons , Moushumi Shome , Kay Y. Blohowiak
Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.
-
Patent Agency Ranking
公开(公告)号：US10016792B2
公开(公告)日：2018-07-10
申请号：US15293349
申请日：2016-10-14
Applicant: The Boeing Company
Inventor： Ashley C. Tracey , Anthony M. Westren , Kay Y. Blohowiak , Mark R. Brei , Tyler Jacob Zimmerman , Richard C. Barclay , Tara Kovacs Baker , Yuliya Shafranyuk
IPC: B08B7/00
CPC classification number: B08B7/0042 , B29C33/3835
Abstract: Provided are methods for cleaning processing tools from residue using laser ablation. Also provided are processing tools comprising non-metal base portions and protective optical layers that cover and shield these base portions from laser ablation. For example, a protective optical layer may reflect a laser beam used for ablating the tool. Methods of forming these protective optical layers on non-metal base portions are also provided. In some embodiments, this protective optical layer is the outermost layer exposed to the environment. Alternatively, the protective optical layer may be covered by a release layer. The release layer may be retained or removed during laser ablation. In some embodiments, light emitted by a processing tool during laser ablation is analyzed to determine performance of its protective optical layer. This feedback may be used to control the laser ablation such as to control orientation of the laser beam relative to the processing tool.
-
公开(公告)号：US09776705B2
公开(公告)日：2017-10-03
申请号：US14446187
申请日：2014-07-29
Applicant: The Boeing Company
Inventor： Matthew Anthony Dilligan , Frederick T. Calkins , Tyler Jacob Zimmerman , James Henry Mabe , Kay Y. Blohowiak
CPC classification number: B64C3/48 , B64C9/02 , B64C9/16 , B64C13/50 , B64C2003/445 , F03G7/065 , Y02T50/14 , Y02T50/32
Abstract: A shape memory structure includes a plurality of bases directly attached to a composite structure and arranged along a first line at a first edge of the composite structure. A plurality of buckle-shaped shape memory structures are attached to corresponding ones of the plurality of bases, such that first ends of the plurality of buckle-shaped shape memory structures are raised relative to the composite structure. Second ends of the plurality of buckle-shaped shape memory structures are directly attached to the composite structure along a second line at a second edge of the composite structure, the second edge being opposite the first edge. When activated, the shape memory structure changes from a buckled shape to an original shape to cause the composite structure to assume a deployed shape; when deactivated, the shape memory structure to resumes a buckled shape and the composite structure an undeployed shape.
-
27.发明申请公开(公告)号：US20160229519A1
公开(公告)日：2016-08-11
申请号：US14446187
申请日：2014-07-29
Applicant: The Boeing Company
Inventor： Matthew Anthony Dilligan , Frederick T. Calkins , Tyler Jacob Zimmerman , James Henry Mabe , Kay Y. Blohowiak
CPC classification number: B64C3/48 , B64C9/02 , B64C9/16 , B64C13/50 , B64C2003/445 , F03G7/065 , Y02T50/14 , Y02T50/32
Abstract: Method and apparatus for controlling a shape of a composite structure. A shape memory structure associated with the composite structure is activated. The shape memory structure changes from a buckled shape to an original shape and causes the composite structure to change from an undeployed shape to a deployed shape. The shape memory structure is deactivated. The shape memory structure changes from the original shape to the buckled shape in response to a load from the composite structure and causes the composite structure to change from the deployed shape to the undeployed shape.
Abstract translation: 用于控制复合结构的形状的方法和装置。 与复合结构相关联的形状记忆结构被激活。 形状记忆结构从弯曲形状变为原始形状，并且使得复合结构从未部署形状变化为展开形状。 形状记忆结构被禁用。 形状记忆结构响应于来自复合结构的载荷而从原始形状变化到弯曲形状，并且使得复合结构从展开形状变化到未部署形状。
-
公开(公告)号：US08962753B2
公开(公告)日：2015-02-24
申请号：US14206363
申请日：2014-03-12
Applicant: The Boeing Company
Inventor： Kjersta L. Larson-Smith , Kay Y. Blohowiak , Jill E. Seebergh , Michael R. Sirkis , Vasan S. Sundaram
IPC: C08L83/04 , C09D5/00 , C08G77/04 , C08G77/14 , C09D183/04 , C09D183/06 , C08K5/5419 , C07F7/18 , C08K5/54
CPC classification number: C09D5/00 , C07F7/1804 , C08G77/04 , C08G77/14 , C08K5/54 , C08K5/5419 , C09D183/04 , C09D183/06 , Y10T428/31612 , Y10T428/31663
Abstract: A hybrid coating composition including an organosilane component, a metal alkoxide component and a surfactant component, with the metal alkoxide component present in the composition at a molar ratio of about 75:1 with respect to the surfactant component. The hybrid coating composition once cured on a transparent substrate has an initial clarity greater than 98. Transparent members are also disclosed that include a transparent substrate having the hybrid coating composition cured on a first major surface thereof.
Abstract translation: 相对于表面活性剂组分，包含有机硅烷组分，金属醇盐组分和表面活性剂组分的混合涂料组合物，其中金属醇盐组分以约75:1的摩尔比存在于组合物中。 一旦在透明基材上固化的混合涂料组合物的初始透明度大于98.还公开了透明构件，其包括在其第一主表面上固化的混合涂料组合物的透明基材。
-
公开(公告)号：US20140193645A1
公开(公告)日：2014-07-10
申请号：US14206363
申请日：2014-03-12
Applicant: The Boeing Company
Inventor： Kjersta L. Larson-Smith , Kay Y. Blohowiak , Jill E. Seebergh , Michael R. Sirkis , Vasan S. Sundaram
IPC: C09D5/00
CPC classification number: C09D5/00 , C07F7/1804 , C08G77/04 , C08G77/14 , C08K5/54 , C08K5/5419 , C09D183/04 , C09D183/06 , Y10T428/31612 , Y10T428/31663
Abstract: A hybrid coating composition including an organosilane component, a metal alkoxide component and a surfactant component, with the metal alkoxide component present in the composition at a molar ratio of about 75:1 with respect to the surfactant component. The hybrid coating composition once cured on a transparent substrate has an initial clarity greater than 98. Transparent members are also disclosed that include a transparent substrate having the hybrid coating composition cured on a first major surface thereof.
Abstract translation: 相对于表面活性剂组分，包含有机硅烷组分，金属醇盐组分和表面活性剂组分的混合涂料组合物，其中金属醇盐组分以约75:1的摩尔比存在于组合物中。 一旦在透明基材上固化的混合涂料组合物的初始透明度大于98.还公开了透明构件，其包括在其第一主表面上固化的混合涂料组合物的透明基材。
-
-
-
-
-
-
-
-
Search Results
29
records
(took 0.023 seconds)
