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71. 发明授权

US4834829A Vacuum ring for producing laminated glass 失效
标题翻译：用于生产夹层玻璃的真空环
公开(公告)号：US4834829A
公开(公告)日：1989-05-30
申请号：US138321
申请日：1987-12-28
申请人： Charles E. Ash , Siegfried H. Herliczek , David R. Jenkins
发明人： Charles E. Ash , Siegfried H. Herliczek , David R. Jenkins
IPC分类号： B32B17/10 , B32B43/00 , B60J10/02
CPC分类号： B32B43/00 , B32B17/10045 , B32B17/10834 , B60J10/70
摘要： A vaccum ring is coupled to a vacuum source and utilized to de-air a laminated glass assembly while it is positioned within a pressurized and heated autoclave unit. The vacuum ring has a channel for receiving the edge of the glass assembly and is fabricated to minimize the extrusion of the laminating material during the autoclave operation. The walls of the channel each have a single longitudinally extending groove approximately centered between the edges of the wall, and the floor of the channel includes a single longitudinally extending groove positioned to be adjacent the edge of a laceration shield layer of the glass assembly. All three grooves interconnect with the vacuum source. The channel generally conforms to the outer edge of the glass assembly with or without applied vacuum of pressure, and the provision of grooved walls greatly enhances the sealing of the ring to the glass.
摘要翻译：真空环耦合到真空源并用于在层压玻璃组件定位在加压和加热的高压釜单元内时将其去空气。真空环具有用于接收玻璃组件的边缘的通道，并且被制造成使得在高压釜操作期间层压材料的挤出最小化。通道的壁各自具有大致居中在壁的边缘之间的单个纵向延伸的槽，并且通道的底部包括一个单独的纵向延伸的凹槽，其定位成邻近玻璃组件的撕裂屏蔽层的边缘。所有三个凹槽与真空源互连。通道通常符合玻璃组件的外边缘，有或没有施加压力的真空，并且提供带槽的壁大大地增强了环对玻璃的密封。

72. 发明授权

US3649283A Process for applying photoresist 失效
标题翻译：适用于光电子的方法
公开(公告)号：US3649283A
公开(公告)日：1972-03-14
申请号：US3649283D
申请日：1969-10-29
申请人： SHIPLEY CO
发明人： CHRISTENSEN CARL W , ISAACSON CALVIN M
IPC分类号： B32B27/00 , B32B43/00 , G03C1/72 , G03C1/74 , G03C11/12 , G03F7/09 , G03F7/11 , G03F7/16 , H05K3/00 , G03C1/86
CPC分类号： B32B27/10 , B32B7/12 , B32B27/00 , B32B37/1284 , B32B43/00 , B32B2307/726 , B32B2457/08 , G03F7/092 , G03F7/161 , H05K3/0079 , Y10S430/136
摘要： This invention is for a process for applying a smooth uniform layer of a photoresist to a base material. In the process, a laminate is provided comprising a layer of light-sensitive photoresist, a permeable backing layer and an intermediate layer displaced between the light-sensitive photoresist layer and the backing layer, the intermediate layer being soluble or degradable in water or developer for the light-exposed photoresist of the laminate. In use, this laminate with the light-sensitive photoresist layer face downward is adhered to a base material and washed with a solvent for the intermediate layer. The solvent permeates and undercuts the backing layer thereby solvating the intermediate layer, and breaking the bond between the backing layer and the light-sensitive layer. The backing layer may then be peeled from the photoresist layer. If the backing layer transmits light, the composite comprising the base material and the laminate may be exposed prior to the washing step and the washing step may be performed with a developer for the lightexposed light-sensitive photoresist layer. A preferred backing layer is clay filled paper having a smooth, glazed surface. An adhering agent may be applied over the photoresist layer if desired.
摘要翻译：本发明用于将光致抗蚀剂的光滑均匀层施加到基材上的方法。在该过程中，提供了包括光敏光刻胶层，可渗透背衬层和在光敏光致抗蚀剂层和背衬层之间位移的中间层的层压体，中间层在水或显影剂中可溶或可降解，曝光后的光刻胶层压板。在使用中，将具有光敏光致抗蚀剂层的层压体面向下粘附到基材上并用用于中间层的溶剂洗涤。溶剂渗透并且底切底层，从而溶解中间层，并破坏背衬层和感光层之间的结合。然后可以将背衬层从光致抗蚀剂层剥离。如果背衬层透光，则可以在洗涤步骤之前暴露包含基材和层压材料的复合材料，并且可以用用于曝光的光敏光致抗蚀剂层的显影剂进行洗涤步骤。优选的背衬层是具有光滑的玻璃表面的粘土填充纸。如果需要，粘合剂可以施加在光致抗蚀剂层上。

73. 发明申请

US20190016107A1 STRUCTURAL PRE-CURED REPAIR PATCH FOR REPAIR TO HIGHLY LOADED PRIMARY AND SECONDARY STRUCTURAL COMPONENTS 审中-公开
公开(公告)号：US20190016107A1
公开(公告)日：2019-01-17
申请号：US15646606
申请日：2017-07-11
申请人： The Boeing Company
发明人： Blake A. BERTRAND , Arne K. LEWIS
IPC分类号： B32B43/00 , B32B37/12 , B32B7/12
CPC分类号： B32B43/00 , B29C73/10 , B32B7/12 , B32B37/12
摘要： Provided is a method a method for reworking an article. The method includes forming a patch over an area of a composite structure requiring rework. The forming includes placing a first film-adhesive over the area of the composite structure requiring rework, wherein the first film-adhesive extends over a first surface area of the structure including beyond an entirety of the area requiring rework, placing a first pre-cured ply stack over the first film-adhesive, wherein the first pre-cured ply stack extends over a second surface area of the composite structure; placing a second film-adhesive over the first pre-cured ply stack, wherein the second film-adhesive extends over a third surface area of the composite structure; and placing a second pre-cured ply stack over the second film-adhesive, wherein the second pre-cured ply stack extends over a fourth surface area of the composite structure.

74. 发明授权

US09995856B2 Lens array fabrication method, and film containing base plate and film attaching instrument employed in same 有权
公开(公告)号：US09995856B2
公开(公告)日：2018-06-12
申请号：US15410698
申请日：2017-01-19
申请人： ENPLAS CORPORATION
发明人： Masahiro Tanazawa , Shimpei Morioka , Makoto Goto , Nobuhiro Hashimoto
IPC分类号： B32B37/00 , G02B3/00 , G02B5/20 , G02B6/42
CPC分类号： G02B3/0012 , B29C65/4825 , B29D11/00298 , B29L2011/0016 , B32B38/10 , B32B43/00 , G02B3/005 , G02B3/0056 , G02B3/0075 , G02B5/205 , G02B6/32 , G02B6/3845 , G02B6/3882 , G02B6/3885 , G02B6/3898 , G02B6/4204 , G02B6/4239 , G02B6/4249 , G02B6/4292 , G02B7/004 , Y10T156/1089 , Y10T156/1195
摘要： A lens array fabrication method for fabricating a lens array includes: receiving pins (16) of a film attaching instrument (jig) in second guide holes (10) of a film-containing base plate; bonding a placement area and an adhesion layer (F); removing the pins (16); causing a detachment between a first detachment film (C) and a pressure-sensitive adhesive optical film (D); separating three layers (D) to (F) from two layers (B) and (C); receiving the pins (16) in first guide holes (7) of a lens array main unit; fitting a film holding protrusion (15) in a depression part (6); bonding the film (D) to a bonding region (i); removing the pins (16); and causing a detachment between the film (D) and a second detachment film (E).

75. 发明授权

US09993980B2 Methods for forming radius fillers for composite structures 有权
公开(公告)号：US09993980B2
公开(公告)日：2018-06-12
申请号：US15486149
申请日：2017-04-12
申请人： The Boeing Company
发明人： William Thomas Kline , Thomas Dean Wilson , Bruno Zbinden , Dalton C. Bergan , Joseph Fount Warren, Jr. , Nicholas A. Boroughs , Scott Edward Krajca
IPC分类号： B32B41/00 , B29C70/38 , B29C70/34 , B29C70/54 , B29K105/08 , B29L31/30
CPC分类号： B29C70/386 , B29C70/34 , B29C70/545 , B29K2105/0872 , B29L2031/3076 , B32B3/18 , B32B5/12 , B32B5/26 , B32B7/045 , B32B27/08 , B32B27/12 , B32B27/18 , B32B27/38 , B32B38/10 , B32B38/1808 , B32B43/00 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/103 , B32B2262/106 , B32B2307/50 , B32B2605/08 , B32B2605/18
摘要： Methods for forming radius fillers for composite structures are disclosed herein. The methods include locating a sheet of composite material on a first support surface and translating the sheet of composite material such that a first portion of the sheet is supported by the first support surface and a second portion of the sheet extends past the support surface edge. The methods also include supporting the second portion of the sheet with a second support surface and separating the second portion of the sheet from the first portion of the sheet to form a strip of composite material. The methods further include conveying the strip of composite material onto a layup surface.

76. 发明申请

US20180105290A1 Composite Panel Tool 审中-公开
公开(公告)号：US20180105290A1
公开(公告)日：2018-04-19
申请号：US15784501
申请日：2017-10-16
申请人： The Boeing Company
发明人： Paul R. Gehlsen
IPC分类号： B64F5/10 , B32B37/12 , B32B43/00 , B64F5/40
CPC分类号： B64F5/10 , B32B37/12 , B32B43/00 , B32B2309/68 , B32B2310/027 , B32B2405/00 , B32B2605/18 , B64F5/40 , Y10T29/49233
摘要： A method and apparatus for holding a panel. A rigid frame is secured on an aircraft on a rework area on the aircraft. A carrier is attached to the rigid frame. The panel is held on the carrier and the carrier moves the panel about a plurality of axes. The panel moves with the carrier such that the panel has a desired position relative to a rework opening in the rework area. The panel is attached to the aircraft while the panel is held in the desired position relative to the rework opening.

77. 发明申请

US20170266942A1 SYSTEMS AND METHODS FOR FORMING RADIUS FILLERS FOR COMPOSITE STRUCTURES 审中-公开
公开(公告)号：US20170266942A1
公开(公告)日：2017-09-21
申请号：US15615453
申请日：2017-06-06
申请人： The Boeing Company
发明人： Elise Rae Ermitano Castorina , Erik Lund , Nicholas A. Boroughs , Matt Christner , Gabriel Zane Forston , William Thomas Kline , Thomas Dean Wilson , Bruno Zbinden , Dalton C. Bergan , Joseph Fount Warren, JR. , Scott Edward Krajca
IPC分类号： B32B38/18
CPC分类号： B32B38/1808 , B29C70/30 , B29C70/386 , B29D99/0003 , B29K2105/0872 , B29L2031/3076 , B32B3/18 , B32B5/12 , B32B5/26 , B32B7/04 , B32B7/045 , B32B27/08 , B32B27/12 , B32B27/18 , B32B27/20 , B32B27/38 , B32B38/10 , B32B43/00 , B32B2260/021 , B32B2260/023 , B32B2260/046 , B32B2262/101 , B32B2262/103 , B32B2262/106 , B32B2307/50 , B32B2307/54 , B32B2605/08 , B32B2605/18
摘要： Systems and methods for forming radius fillers for composite structures are disclosed herein. The systems include a sheet-locating structure that has a support surface and a support surface edge. The systems further include a separation device, a conveyance structure, and a layup surface. The methods include locating a sheet of composite material on a first support surface and translating the sheet of composite material such that a first portion of the sheet is supported by the first support surface and a second portion of the sheet extends past the support surface edge. The methods also include separating the second portion of the sheet from the first portion of the sheet to form a strip of composite material. The methods further include conveying the strip of composite material onto a layup surface and repeating the methods to form the radius filler from a plurality of strips of composite material.

78. 发明授权

US09744719B2 Method and apparatus for repairing composite materials 有权
公开(公告)号：US09744719B2
公开(公告)日：2017-08-29
申请号：US15407216
申请日：2017-01-16
申请人： The Boeing Company
发明人： Moushumi Shome , Adriana Willempje Blom , Sahrudine Apdalhaliem , Waeil M. Ashmawi
IPC分类号： B29C65/48 , B29C65/00 , B32B41/00 , B32B37/00 , B29C65/50 , B29C35/08 , B29C65/14 , B29C73/10 , B29C73/12 , B29C73/34 , B32B37/06 , B29K101/10 , B29K63/00 , B29K105/00 , B29L31/30
CPC分类号： B29C66/9141 , B29C35/08 , B29C35/0805 , B29C65/1425 , B29C65/1467 , B29C65/1496 , B29C65/4835 , B29C65/5021 , B29C65/5028 , B29C65/5057 , B29C65/5078 , B29C66/0342 , B29C66/12463 , B29C66/5326 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/72323 , B29C66/73941 , B29C66/843 , B29C66/8742 , B29C66/91216 , B29C66/91221 , B29C66/91411 , B29C66/91443 , B29C66/9161 , B29C66/919 , B29C66/91951 , B29C66/949 , B29C66/961 , B29C66/9672 , B29C66/9674 , B29C73/10 , B29C73/12 , B29C73/34 , B29C2035/0855 , B29K2063/00 , B29K2101/10 , B29K2105/0097 , B29L2031/30 , B29L2031/3076 , B29L2031/3082 , B29L2031/3085 , B29L2031/3091 , B29L2031/5254 , B29L2031/7692 , B32B37/0046 , B32B37/06 , B32B37/18 , B32B38/0008 , B32B41/00 , B32B43/00 , Y10T156/10 , B29K2307/04
摘要： A method of bonding materials may comprise defining a bond interface between two materials in a cure zone on a surface of an object, and non-conductively heating the bond interface without directly heating the surface outside of the cure zone. Non-conductively heating the bond interface may involve applying microwave radiation to the bond interface.

79. 发明授权

US09649809B2 Wrinkle diffuser system for composites 有权
公开(公告)号：US09649809B2
公开(公告)日：2017-05-16
申请号：US14222617
申请日：2014-03-22
申请人： The Boeing Company
发明人： Tristan E. Lee , Andrew M. Hopkins , William T. Kline
IPC分类号： B29C53/18 , B32B38/18 , B32B43/00 , B29C70/54 , B29C70/56 , B29C33/42
CPC分类号： B29C53/18 , B29C33/42 , B29C70/543 , B29C70/56 , B32B38/18 , B32B43/00 , Y10T156/1002 , Y10T156/1043 , Y10T428/24628 , Y10T428/24694
摘要： A system for diffusing wrinkles in a composite laminate may include at least one wrinkle diffuser. The wrinkle diffuser may include a diffuser body may be mounted to a tool in a manner such that a composite ply at least partially overlaps the wrinkle diffuser. A plurality of diffuser elements may be formed in the diffuser body to define a corrugated surface. The corrugated surface may cause a portion of the composite ply to assume a corrugated shape when a compaction pressure is applied to force the composite ply against the corrugated surface. The wrinkle diffuser may include an indexing feature to index the wrinkle diffuser to a ply edge of the composite ply.

80. 发明申请

US20170131486A1 LENS ARRAY FABRICATION METHOD, AND FILM CONTAINING BASE PLATE AND FILM ATTACHING INSTRUMENT EMPLOYED IN SAME 审中-公开
公开(公告)号：US20170131486A1
公开(公告)日：2017-05-11
申请号：US15415670
申请日：2017-01-25
申请人： ENPLAS CORPORATION
发明人： Masahiro TANAZAWA , Shimpei MORIOKA , Makoto GOTO , Nobuhiro HASHIMOTO
IPC分类号： G02B6/38 , B29D11/00 , G02B6/42 , B29C65/48 , G02B3/00 , G02B6/32
CPC分类号： G02B3/0012 , B29C65/4825 , B29D11/00298 , B29L2011/0016 , B32B38/10 , B32B43/00 , G02B3/005 , G02B3/0056 , G02B3/0075 , G02B5/205 , G02B6/32 , G02B6/3845 , G02B6/3882 , G02B6/3885 , G02B6/3898 , G02B6/4204 , G02B6/4239 , G02B6/4249 , G02B6/4292 , G02B7/004 , Y10T156/1089 , Y10T156/1195
摘要： A film attaching jig (III) is used in a method for fabricating a lens array to attach a pressure-sensitive adhesive optical film (D) onto an adhesion area (i) and has: (1) a main body having a first end face in a z′-direction being an end face to be directed to a film-containing base plate (II) and a lens array main unit (I); (2) a film holding projection that is provided on the first end face and protrudes in parallel to the z′-direction toward the film-containing base plate (II) and the lens array main unit (I), the film holding projection having a holding area (iii) at its front end face for temporarily holding the pressure-sensitive adhesive optical film (D); and (3) a pair of pins or holes disposed on the first end face in parallel to the z′-direction, and provided at opposite positions over the film holding projection.

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