公开(公告)号：US5906550A

公开(公告)日：1999-05-25

申请号：US982779

申请日：1997-12-02

申请人： William R. Kingston

发明人： William R. Kingston

IPC分类号： A63B53/10 ,  A63B59/06 ,  B32B5/26 ,  B32B15/08 ,  A63B53/12

CPC分类号： B32B38/0036 ,  B32B15/08 ,  B32B5/26 ,  A63B2102/18 ,  A63B2209/02 ,  A63B53/10 ,  A63B59/50 ,  A63B60/54 ,  B32B2038/0016 ,  B32B2038/0076 ,  B32B2305/08 ,  B32B2311/00 ,  B32B2311/18

摘要： A sports bat such as used to play baseball or softball, comprising a shell which includes a first layer of titanium alloy-fiber reinforced composite laminate, a second layer of titanium alloy-fiber reinforced composite laminate and a core layer between the first layer and the second layer. Further, a method of making a bat comprising a shell which includes a first layer of titanium alloy-fiber reinforced composite laminate, a second layer of titanium alloy-fiber reinforced composite laminate and a core layer between the first layer and the second layer.

摘要翻译： 用于玩棒球或垒球的运动蝙蝠，包括壳体，其包括第一层钛合金纤维增强复合层压板，第二层钛合金纤维增强复合层压板和第一层和第二层之间的芯层 第二层。 此外，制造包括壳的蝙蝠的方法包括第一层钛合金纤维增强复合层压板，第二层钛合金纤维增强复合层压板和在第一层和第二层之间的芯层。

公开(公告)号：US5866272A

公开(公告)日：1999-02-02

申请号：US585304

申请日：1996-01-11

申请人： Willard N. Westre ,  Heather C. Allen-Lilly ,  Donald J. Ayers ,  Samuel E. Cregger ,  David W. Evans ,  Donald L. Grande ,  Daniel J. Hoffman ,  Mark E. Rogalski ,  Robert J. Rothschilds

发明人： Willard N. Westre ,  Heather C. Allen-Lilly ,  Donald J. Ayers ,  Samuel E. Cregger ,  David W. Evans ,  Donald L. Grande ,  Daniel J. Hoffman ,  Mark E. Rogalski ,  Robert J. Rothschilds

IPC分类号： B32B15/08 ,  B64C1/00 ,  B64C1/12 ,  B64C30/00 ,  B32B3/12

CPC分类号： B64C30/00 ,  B32B15/08 ,  B32B15/14 ,  B32B3/12 ,  B32B37/146 ,  B32B5/02 ,  B32B5/12 ,  B32B7/005 ,  B64C1/12 ,  B64C3/26 ,  B32B2250/42 ,  B32B2255/06 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/10 ,  B32B2262/106 ,  B32B2305/076 ,  B32B2307/306 ,  B32B2307/54 ,  B32B2307/552 ,  B32B2307/714 ,  B32B2311/18 ,  B32B2605/18 ,  B64C2001/0072 ,  Y02T50/433 ,  Y10T428/1234 ,  Y10T428/12431 ,  Y10T428/12444 ,  Y10T428/12569 ,  Y10T428/12806 ,  Y10T428/24165 ,  Y10T428/249942 ,  Y10T428/26 ,  Y10T428/31678

摘要： The invention provides a hybrid laminate and skin panels of hybrid laminate structure that are suitable for a supersonic civilian aircraft. The hybrid laminates include layups of layers of titanium alloy foil and composite plies, that are optimally oriented to counteract forces encountered in use, that are bonded to a central core structure, such as titanium alloy honeycomb. The reinforcing fibers of the composite plies are selected from carbon and boron, and the fibers are continuous and parallel oriented within each ply. However, some plies may be oriented at angles to other plies. Nevertheless, in a preferred embodiment of the invention, a substantial majority of, or all of, the fibers of the hybrid laminates are oriented in a common direction. The outer surfaces of the laminates include a layer of titanium foil to protect the underlying composite-containing structure from the environment, and attack by solvents, and the like.

公开(公告)号：US3916048A

公开(公告)日：1975-10-28

申请号：US36256173

申请日：1973-05-21

申请人： DOW CHEMICAL CO

发明人： WALLES WILHELM E

IPC分类号： B65D1/02 ,  A47J41/02 ,  A61J1/00 ,  B32B1/02 ,  B32B7/00 ,  B32B15/08 ,  B65D1/00 ,  B65D8/06 ,  B65D39/04 ,  B65D39/08 ,  B65D81/38 ,  C23C18/16 ,  C23C18/30 ,  C23C18/31 ,  C23C18/44 ,  C23C18/50 ,  E04B1/80 ,  F17C3/08

CPC分类号： B32B1/02 ,  A47J41/022 ,  B32B15/08 ,  B32B15/082 ,  B32B15/085 ,  B32B15/088 ,  B32B15/09 ,  B32B15/098 ,  B32B15/20 ,  B32B27/285 ,  B32B27/306 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B32B27/42 ,  B32B2311/04 ,  B32B2311/08 ,  B32B2311/12 ,  B32B2311/14 ,  B32B2311/16 ,  B32B2311/18 ,  B32B2311/22 ,  B32B2311/24 ,  B32B2323/00 ,  B32B2361/00 ,  B32B2367/00 ,  B32B2369/00 ,  B32B2371/00 ,  B32B2377/00 ,  B32B2439/60 ,  B65D11/16 ,  B65D81/3846 ,  C23C18/1646 ,  C25D5/56 ,  E04B1/80 ,  F17C3/08 ,  F17C2201/0109 ,  F17C2203/0391 ,  F17C2203/0395 ,  F17C2203/0607 ,  F17C2203/0629 ,  F17C2203/0636 ,  F17C2203/066 ,  F17C2205/0311 ,  Y10T428/1359 ,  Y10T428/31699

摘要： A plastic article is rendered essentially impermeable to atmospheric gases and other vapors by metallizing the wall structure of the plastic article with a metal to form a thin metal layer and overcoating the metal layer with a latex of an organic polymer, particularly a barrier polymer such as a vinylidene chloride polymer, to provide alayer of the organic polymer adherent to the metal layer.

公开(公告)号：US3856172A

公开(公告)日：1974-12-24

申请号：US38974873

申请日：1973-08-20

申请人： DOW CHEMICAL CO

发明人： WALLES W

IPC分类号： B65D1/02 ,  A47J41/02 ,  A61J1/00 ,  B32B1/02 ,  B32B7/00 ,  B32B15/08 ,  B65D1/00 ,  B65D8/06 ,  B65D39/04 ,  B65D39/08 ,  B65D81/38 ,  C23C18/16 ,  C23C18/30 ,  C23C18/31 ,  C23C18/44 ,  C23C18/50 ,  E04B1/80 ,  F17C3/08

CPC分类号： B32B1/02 ,  A47J41/022 ,  B32B15/08 ,  B32B15/082 ,  B32B15/085 ,  B32B15/088 ,  B32B15/09 ,  B32B15/098 ,  B32B15/20 ,  B32B27/285 ,  B32B27/306 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B32B27/42 ,  B32B2311/04 ,  B32B2311/08 ,  B32B2311/12 ,  B32B2311/14 ,  B32B2311/16 ,  B32B2311/18 ,  B32B2311/22 ,  B32B2311/24 ,  B32B2323/00 ,  B32B2361/00 ,  B32B2367/00 ,  B32B2369/00 ,  B32B2371/00 ,  B32B2377/00 ,  B32B2439/60 ,  B65D11/16 ,  B65D81/3846 ,  C23C18/1646 ,  C25D5/56 ,  E04B1/80 ,  F17C3/08 ,  F17C2201/0109 ,  F17C2203/0391 ,  F17C2203/0395 ,  F17C2203/0607 ,  F17C2203/0629 ,  F17C2203/0636 ,  F17C2203/066 ,  F17C2205/0311 ,  Y10T428/1359 ,  Y10T428/31699

摘要： Heat insulative properties of vacuum containers such as vacuum bottles are significantly improved by stoppering the container with a vacuumized plastic cap having a boundary wall of structural plastic material wherein the inner surface of the boundary wall is coated with a thin metallic layer and a layer of barrier plastic such as a vinylidene chloride copolymer and which encloses an evacuated space filled with a gas absorbing material such as activated charcoal.

摘要翻译： 通过用具有结构塑料材料的边界壁的真空塑料帽塞住容器，显着改善真空容器如真空瓶的绝热性能，其中边界壁的内表面涂覆有薄的金属层和一层屏障 塑料如偏二氯乙烯共聚物，并且包围填充有气体吸收材料如活性炭的抽空空间。

公开(公告)号：US3853690A

公开(公告)日：1974-12-10

申请号：US26584872

申请日：1972-06-23

申请人： AMERICAN CYANAMID CO

发明人： MCGARRY F ,  SUEN T

IPC分类号： B32B15/08 ,  C09J201/00 ,  B32B27/06 ,  C09J3/14

CPC分类号： B32B15/08 ,  B32B3/12 ,  B32B2311/18 ,  B32B2311/24 ,  B32B2311/30 ,  B32B2315/085 ,  B32B2327/18 ,  B32B2361/00 ,  B32B2363/00 ,  B32B2367/00 ,  B32B2398/10 ,  C08L2666/02 ,  C09J201/00 ,  Y10T428/31522 ,  Y10T428/31544

摘要： Various substrates are bonded together with adhesives comprising a thermosetting resin containing from about 1 percent to about 40 percent of polytetrafluoroethylene. The resultant articles exhibit excellent structural properties and find use in such areas as the aerospace industry.

摘要翻译： 各种基材与含有约1％至约40％的聚四氟乙烯的热固性树脂的粘合剂粘合在一起。 所得物品具有优异的结构性能，可用于航空航天工业等领域。

公开(公告)号：US20190193370A1

公开(公告)日：2019-06-27

申请号：US16293323

申请日：2019-03-05

申请人： SHENZHEN FUTAIHONG PRECISION INDUSTRY CO., LTD. ,  FIH (HONG KONG) LIMITED

发明人： CHWAN-HWA CHIANG ,  BAO-SHEN ZHANG ,  CHIEH-HSIANG WANG

IPC分类号： B32B3/26 ,  B32B15/04 ,  B32B27/06 ,  B32B27/28 ,  B29C45/14 ,  B29C45/00

CPC分类号： B32B3/26 ,  B29C45/00 ,  B29C45/14311 ,  B29C2045/14868 ,  B32B15/04 ,  B32B15/08 ,  B32B15/09 ,  B32B15/18 ,  B32B15/20 ,  B32B27/06 ,  B32B27/285 ,  B32B27/286 ,  B32B27/288 ,  B32B27/304 ,  B32B27/36 ,  B32B27/365 ,  B32B2250/02 ,  B32B2255/06 ,  B32B2255/20 ,  B32B2310/00 ,  B32B2311/18 ,  B32B2311/20 ,  B32B2311/24 ,  B32B2311/30 ,  B32B2327/06 ,  B32B2367/00 ,  B32B2369/00 ,  B32B2371/00 ,  B32B2509/00 ,  B32B2605/08 ,  Y10T428/24996

摘要： A method for making a metal-and-resin composite, including: providing a metal substrate made of stainless steel; forming a plurality of nano pores on a surface of the metal substrate by chemical etching the metal substrate; forming an intermediate layer on the metal substrate by dipping the metal substrate in a coupling agent solution, the intermediate layer filling at least portion of each nano pore; and forming a resin member by placing the metal substrate in a mold and molding molten resin on a surface of the intermediate layer, the resin member covering and bonding with the intermediate layer, treating the metal substrate with a coupling solution having a silane compound coupling agent to make the intermediate layer.

公开(公告)号：US20180355485A1

公开(公告)日：2018-12-13

申请号：US15781746

申请日：2016-12-06

申请人： Michiels Group ,  Universiteit Gent

发明人： Klaartje DE BUYSSER ,  Matthias IDE ,  Matthias VAN ZELE ,  Isabel VAN DRIESSCHE

IPC分类号： C23C18/12 ,  C23C14/08 ,  B32B17/06 ,  B32B27/36

CPC分类号： C23C18/1254 ,  B32B17/064 ,  B32B27/36 ,  B32B2255/205 ,  B32B2307/30 ,  B32B2307/536 ,  B32B2307/584 ,  B32B2311/18 ,  C08J7/045 ,  C08J2367/02 ,  C08J2483/04 ,  C23C14/08 ,  C23C18/1208 ,  C23C18/1233

摘要： The invention relates to a method of manufacturing a coated polymer substrate having low emissivity properties and a high hardness. The method comprises the steps of providing a polymer substrate; applying at least one adhesion promoting layer on one side of said polymer substrate; applying at least one silica or silica-based layer on said at least one adhesion promoting layer by a sol-gel process. The invention further relates to a coated polymer substrate having low emissivity properties, to a glass substrate provided with a coated polymer substrate and to the use of such a coated substrate as substrate having low emissivity properties.

公开(公告)号：US09919507B2

公开(公告)日：2018-03-20

申请号：US15384767

申请日：2016-12-20

申请人： The Boeing Company

发明人： Gary Ernest Georgeson ,  Kenneth Harlan Griess

IPC分类号： B29C65/48 ,  B32B37/14 ,  B32B37/18 ,  B32B37/12 ,  B29C65/00 ,  B29C65/82

CPC分类号： B32B3/06 ,  B29C65/48 ,  B29C65/4855 ,  B29C65/8253 ,  B29C65/8269 ,  B29C66/112 ,  B29C66/114 ,  B29C66/1248 ,  B29C66/128 ,  B29C66/1282 ,  B29C66/1284 ,  B29C66/20 ,  B29C66/43 ,  B29C66/54 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/723 ,  B29C66/72321 ,  B29C66/7394 ,  B29C66/742 ,  B29C70/86 ,  B29K2703/06 ,  B29L2031/3002 ,  B29L2031/3076 ,  B32B1/00 ,  B32B3/14 ,  B32B3/18 ,  B32B7/12 ,  B32B15/01 ,  B32B15/08 ,  B32B15/20 ,  B32B27/20 ,  B32B27/38 ,  B32B37/02 ,  B32B37/12 ,  B32B37/14 ,  B32B37/18 ,  B32B2250/05 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2305/076 ,  B32B2305/77 ,  B32B2307/558 ,  B32B2307/714 ,  B32B2307/752 ,  B32B2311/18 ,  B32B2313/04 ,  B32B2605/00 ,  B32B2605/18 ,  B64C1/061 ,  B64C1/12 ,  B64C3/26 ,  C22C14/00 ,  Y02T50/43 ,  Y10T156/10 ,  Y10T156/109 ,  Y10T156/1092 ,  Y10T428/192 ,  Y10T428/195 ,  B29K2307/04 ,  B29K2063/00

摘要： A composite structure comprises stacked sets of laminated fiber reinforced resin plies and metal sheets. Edges of the resin plies and metal sheets are interleaved to form a composite-to-metal joint connecting the resin plies with the metal sheets.

公开(公告)号：US09808996B2

公开(公告)日：2017-11-07

申请号：US14469575

申请日：2014-08-26

申请人： The Boeing Company

发明人： Jeffery L. Marcoe

IPC分类号： B29C70/30 ,  B32B1/08 ,  B64C3/00 ,  B64C3/18 ,  B32B5/02 ,  B32B15/08 ,  B32B27/12 ,  B32B37/02 ,  B32B38/00

CPC分类号： B29C70/30 ,  B32B1/08 ,  B32B5/02 ,  B32B15/08 ,  B32B27/12 ,  B32B37/02 ,  B32B38/004 ,  B32B2262/10 ,  B32B2307/202 ,  B32B2307/544 ,  B32B2307/558 ,  B32B2311/18 ,  B32B2311/24 ,  B32B2311/30 ,  B32B2313/04 ,  B32B2605/00 ,  B32B2605/18 ,  B64C3/00 ,  B64C3/18 ,  Y02T50/43 ,  Y10T29/49826

摘要： In an embodiment of the disclosure, there is provided a method of fabricating a thermoplastic torque box assembly. The method includes providing a plurality of braided thermoplastic tubular spar caps, connecting one or more connector elements to one or more of the braided thermoplastic tubular spar caps, and laying up an inner thermoplastic facesheet in a continuous manner around the one or more braided thermoplastic tubular spar caps. The method further includes attaching a plurality of skin panel stabilization elements to the inner thermoplastic facesheet to define four torque box side portions, laying up and attaching an outer thermoplastic facesheet in a continuous manner around the plurality of skin panel stabilization elements, and heating at an effective temperature and an effective pressure the thermoplastic torque box assembly.

公开(公告)号：US20170292452A1

公开(公告)日：2017-10-12

申请号：US15096619

申请日：2016-04-12

申请人： UNITED TECHNOLOGIES CORPORATION

发明人： Gary D. Roberge

IPC分类号： F02C7/24 ,  B23K26/36 ,  C25D7/00 ,  C25D5/40 ,  C25D5/38 ,  C25D5/36 ,  C23C4/134 ,  C23C4/129 ,  C23C24/04 ,  C23C14/16 ,  C23C14/30 ,  C23C16/06 ,  F02K1/04 ,  B21D22/02 ,  B23H9/14

CPC分类号： F02C7/24 ,  B21D22/02 ,  B23H9/14 ,  B23K26/36 ,  B32B1/00 ,  B32B3/26 ,  B32B3/263 ,  B32B3/266 ,  B32B3/30 ,  B32B5/00 ,  B32B5/22 ,  B32B15/00 ,  B32B15/01 ,  B32B15/04 ,  B32B15/046 ,  B32B15/18 ,  B32B15/20 ,  B32B37/24 ,  B32B38/04 ,  B32B2037/243 ,  B32B2037/246 ,  B32B2038/047 ,  B32B2250/03 ,  B32B2266/00 ,  B32B2266/045 ,  B32B2266/06 ,  B32B2266/08 ,  B32B2305/02 ,  B32B2305/022 ,  B32B2307/00 ,  B32B2307/10 ,  B32B2307/102 ,  B32B2311/12 ,  B32B2311/18 ,  B32B2311/22 ,  B32B2311/24 ,  B32B2311/30 ,  B32B2605/18 ,  C23C4/08 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  C23C14/16 ,  C23C14/30 ,  C23C16/06 ,  C23C24/04 ,  C23C28/021 ,  C25D5/36 ,  C25D5/38 ,  C25D5/40 ,  C25D7/00 ,  F02K1/04 ,  F05D2220/32 ,  F05D2230/12 ,  F05D2230/13 ,  F05D2230/31 ,  F05D2240/12 ,  F05D2260/96

摘要： A method of making a light weight component is provided. The method including the steps of: forming a metallic foam core into a desired configuration; applying an external metallic shell to an exterior surface of the metallic foam core after it has been formed into the desired configuration; and attenuating the component to a desired frequency by forming a plurality of openings in the external metallic shell.