| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 181 | Process for the production of improved metallized films | US10818801 | 2004-04-06 | US20050028923A1 | 2005-02-10 | Jean-Marc Francois |
| Improved metallized films are produced by transferring a protective layer onto a metal layer from the side of the film remote from the metal layer. The transfer preferably takes place in the metallizer shortly after metallization and before the metal layer is exposed to the atmosphere which reduces the tendency of the metal to oxidize leading to a purer metal layer with enhanced barrier properties. | ||||||
| 182 | Method for manufacturing polarizer, polarizer, polarizing plate, and image display | US10634823 | 2003-08-06 | US20040027663A1 | 2004-02-12 | Eiji Hamamoto |
| A polarizer comprising polyvinyl alcohol based films stretched at high stretching ratios stably manufactured: a method for manufacturing including a stretching processing process, a dyeing treatment process, and a boron compounds treatment process to a polyvinyl alcohol film, wherein the stretching processing is performed at least twice so that a total stretching ratio may become 5.5 times or more, and in a second stretching processing or later, wet stretching processing having stretching ratios of 1.2 times or more is performed applying a peripheral velocity difference between a first pinch roll and a second pinch roll, and in the wet stretching processing, a film conveyed out from the first pinch roll is passed on a first guide roll so as to make a holding angle (A) of 120 through 175null on a first guide roll to which the film first contacts. | ||||||
| 183 | Glass break repair kit apparatus and method | US09830525 | 2001-07-11 | US06685784B1 | 2004-02-03 | Gerald Jacino; Anthony Jacino |
| A kit for repairing a windshield break utilizing a light activated resin includes a light impervious pedestal and resin chamber with the pedestal being placed in airtight engagement about a windshield break. The kit also includes a syringe which is couplable to an opening in the chamber. The light activated resin is carried in a light impervious container having a neck dimensioned to deposit the resin directly into the chamber before the syringe is coupled to the chamber. The kit additionally includes a light transmissive film to cover the resin filled break during curing of the resin and a light impervious patch for covering the opposite face of the windshield. | ||||||
| 184 | Process for transferring a thin-film structure to a substrate | US09460488 | 1999-12-14 | US06183588B2 | 2001-02-06 | Kimberley A. Kelly; Ashwani K. Malhotra; Eric D. Perfecto; Roy Yu |
| A process for fabricating and releasing a thin-film structure from a primary carrier for further processing. The thin-film structure is built on a metal interconnect disposed on a dielectric layer which, in turn, is deposited on a primary carrier. The thin-film structure and metal interconnect are released from the dielectric layer and primary carrier along a release interface defined between the metal interconnect and the dielectric film. Release is accomplished by disturbing the interface, either by laser ablation or dicing. The process of the present invention has at least three, specific applications: (1) the thin-film structure and metal interconnect can be released to yield a free-standing film; (2) the thin-film structure and metal interconnect can be laminated onto a permanent substrate (when building top-side down structures) and then released; and (3) the thin-film structure can be transferred to a secondary temporary carrier (when building top-side up structures) for further processing and testing, then transferred to a permanent substrate before releasing the thin-film structure and metal interconnect. | ||||||
| 185 | Composite structure repair process | US09262807 | 1999-03-04 | US06174392B1 | 2001-01-16 | Carl Andrew Reis |
| A method for repairing a multi-layered damage area in a multi-layered composite structure. The method first includes obtaining depth measurement data, and obtaining topographical measurement data by laser scanning the surface of the damage area. This depth measurement data and topographical measurement data are inputted into a microprocessor along with thickness data of each layer. All inputted information is correlated among itself to thereby internally produce a three-dimensional damage area display-replica and interpolate a two-dimensional pattern of each layer of the damage area and of the surface of the damage area. The damage area is removed by first projecting a two-dimensional laser pattern of the damage area thereat on the surface of the structure, and thereafter manually removing the area to produce a void. Repair is accomplished by projecting onto respective replacement material a two-dimensional laser image pattern of each layer and manually cutting that layer according to the appropriate pattern. The cut layers then are arranged in accord with construction of the removed damage area to form a plug that is placed within the void. | ||||||
| 186 | Method of recycling disk recording medium and apparatus for recovering metal reflective film | US112227 | 1998-07-09 | US6066229A | 2000-05-23 | Tetsuya Komine; Hidemi Tomita; Mari Ichimura |
| A method of recycling a disk recording medium includes the steps of retaining the disk recording medium in a liquid medium, the disk recording medium having a layered structure including a substrate, a dye layer, a reflective film, and a protective layer; radiating ultrasonic waves onto the disk recording medium such that the substrate and the reflective film are separated from each other; and bringing a solution into contact with the substrate separated from the reflective film such that the dye layer is separated from the substrate in order to recover the substrate, the solution dissolving the dye layer. | ||||||
| 187 | Method for the production and repair of multicoat special-effect coating | US92734 | 1998-06-06 | US5849365A | 1998-12-15 | Heinz Topfel; Ewald Bischoff; Harry Libutzki; Jorge Wellmann; Dieter Herbst; Hans-Joachim Streitberger |
| The invention relates to a method for the production and repair of multicoat special-effect coatings, in which the basecoats is produced exclusively by elecrostatic �sic! spraying, a coating material with a specific rheological behavior is employed as the basecoats and the repair is carried out with the aid of a spray application process in which a spray jet is produced which is distinguished in that at most 40% of the coating droplets passing a measurement point which lies at the center of the spray jet and 300 mm away from the nozzle have a diameter which is less than 20 .mu.m and at least 5% of the coating droplets have a diameter which is greater than 60 .mu.m, at least 20% of the coating droplets passing the measurement point have a speed which is less than 6 m/s and at most 30% of the coating droplets have a speed of more than 10 m/s, and the coating droplets have a momentum which is equal to at least 4.times.10.sup.-5 g cm s.sup.-1, the diameter and the speed having been determined with the aid of the Doppler phase anemometry method. | ||||||
| 188 | Method of repairing sound attenuation structure used for aircraft applications | US509037 | 1995-07-28 | US5653836A | 1997-08-05 | Jason G. Mnich; David S. Marsh; Ralph T. Werley; Robert Bowman |
| A method and product for repairing sound attenuation structure for aircraft jet engine noise that includes a central honeycomb core having an imperforate facing sheet adhesively bonded thereto and a perforated facing sheet adhesively bonded to the opposing surface of the core with a woven wire cloth media adhesively bonded to the outer surface of the perforated sheet. The wire cloth is subject to deterioration and disbonding in service use. The method provides for the removal of the deteriorated wire cloth that has disbonded or deteriorated and, after cleaning of the perforated sheet and the associated honeycomb core area, and priming of the cleaned area of the perforated sheet replacement with a polymer film that is precoated with a pressure sensitive adhesive so that the film may be easily applied to the exposed perforated sheet area in place of the removed wire cloth. The film is laser drilled to provide microporous pores to permit the repaired product to substantially retain its original acoustic properties. A polyurethane film that is adapted to be erosion resistant and ultraviolet radiation resistant is disclosed. | ||||||
| 189 | Composite materials and process | US225095 | 1994-04-08 | US5429856A | 1995-07-04 | Dennis L. Krueger; Leigh E. Wood |
| Inelastic films comprising at least one elastomeric core and a surrounding inelastic matrix preferably prepared by coextrusion. The film when stretched and allowed to recover will create an elastomeric composite. | ||||||
| 190 | Flexible metal clad laminate, production method thereof and apparatus for the method | US360909 | 1989-05-03 | US5089355A | 1992-02-18 | Moritsugu Morita; Takushi Sato; Shusuke Yamanaka; Shunji Yoshida; Kenji Tanabe; Mitsuyuki Naito; Shigeyuki Shishido |
| An elongated flexible metal clad laminate formed of at least one metal layer and at least one plastic layer and having a smaller interlayer dimensional difference and excellent process-ability. A defect that a dimension of the metal layer is longer than a corresponding dimension of the plastic layer when they are compared to each other as discrete layers has been corrected by causing the metal layer to continually undergo compression plastic deformation in the form of the laminate and hence compressing the metal layer. A production method for the laminate and an apparatus for the method. | ||||||
| 191 | Seam for impenetrable material | US298687 | 1989-01-19 | US4981762A | 1991-01-01 | Robert D. Athey, Jr. |
| A seal for connecting abutting first and second elastomeric sheets having overlying metallic portions including an elastomeric strip. The elastomeric strip is bonded to the elastomeric portions of the first and second sheets. An electrically conductive filler is attached to the metallic portions of the abutting sheets. A metallic layer is then plated to the conductive filler. A layer of flexible and abrasion resistant material adheres to the metallic plate and the metallic portions of the abutting sheets. | ||||||
| 192 | Plastic laminate repair | US314187 | 1989-02-22 | US4948443A | 1990-08-14 | Lawrence Speer |
| A process for repairing plastic laminates comprising cleaning the damaged areas and filling the same with a suitably colored patch material. Preferably the patch material comprises a mixture of an aqueous dispersion of a vinyl acetate homopolymer with an aqueous dispersion of a vinly acetate/acrylic copolymer, together with a color pigment, and a filler. Desirable additonal ingredients to the patch material include an aqueous polyurethane dispersion and a thickening agent. An initial foundation base layer comprising an epoxy material may be applied to the damaged area before the patch material is applied. After drying and smoothing, the surface of the patch may be decorated with a design to match the undamaged area, and a clear coat of polyurethane is applied to the patch. | ||||||
| 193 | Compact tabletop machine for making labels and other laminations | US137770 | 1987-12-24 | US4882004A | 1989-11-21 | Douglas M. Watson |
| A compact tabletop machine for making laminations such as labels of the type including a central substrate layer and first and second outer layers having inside glue-bearing faces in face-to-face contact with opposite faces of the central layer. | ||||||
| 194 | Repair process for a fibre reinforced structure | US230917 | 1988-08-11 | US4855173A | 1989-08-08 | Peter B. Dore |
| A repair process for a damaged fibre-reinforced structure, such as the frame of a sports racquet, comprises the steps of making a window in the structure across the damaged area and filling the exposed cavity at the damaged area with a combination of reinforced fibres wetted out with a curable resin, and a plug. The plug is preferably a short length of solid rod, for instance of fibre-glass and polyester material, and is packed to either side in the structure with the reinforcing fibres which may be provided by Kevlar rovings. The repair is further reinforced by a curable overlay. | ||||||
| 195 | Sealing leaks by polymerization of volatilized aminosilane monomers | US966327 | 1978-12-04 | US4237172A | 1980-12-02 | Joseph J. Packo; Donald L. Bailey |
| Leaks in a vessel or pipeline or the like adapted for containing a fluid, are sealed by means of a volatilized polymerizable aminosilane supplied to the interior of the vessel under sufficient pressure and for a sufficient period of time to permit contact thereof and react in the presence of moisture or sand at the situs of the leak to provide a solid polysiloxane seal. | ||||||
| 196 | Process for applying photoresist | US3649283D | 1969-10-29 | US3649283A | 1972-03-14 | CHRISTENSEN CARL W; ISAACSON CALVIN M |
| 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.
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| 197 | Composites comprising adhered components | US14696360 | 2015-04-24 | US10137663B2 | 2018-11-27 | Carlos A. Fracchia; Terry A. Sewell; Charles A. Rhodes |
| A composite comprising adhered components and method of refurbishing such composites are described herein. The composite includes a first component, a second component, and the first component being adhered to the second component using an adhesive stack. The adhesive stack comprises a first adhesive-impregnated scrim layer disposed between the first component and the second component and a bulk adhesive layer disposed between the first component and the second component. | ||||||
| 198 | Composite textiles including spread filaments | US14034456 | 2013-09-23 | US10035323B2 | 2018-07-31 | Kenneth H. Griess; Jack J. Esposito; Gary E. Georgeson |
| An article comprises a multi-directional textile of first reinforcing fiber tows extending in a first direction and second reinforcing fiber tows extending in a second direction. Filaments in the first fiber tows extend past a boundary of the textile and are spread. The tows are embedded in resin. | ||||||
| 199 | Lens array fabrication method, and film containing base plate and film attaching instrument employed in same | US15410698 | 2017-01-19 | US09995856B2 | 2018-06-12 | Masahiro Tanazawa; Shimpei Morioka; Makoto Goto; Nobuhiro Hashimoto |
| 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). | ||||||
| 200 | METHOD FOR RECONDITIONING OF A DAMAGED PORTION OF A COMPONENT AND INSERT THEREFOR | US15697691 | 2017-09-07 | US20180133850A1 | 2018-05-17 | Alexei VICHNIAKOV; Waldemar MICHELSON |
| According to an embodiment, a method is provided for preparing a reconditioning of a damaged portion of a component, particularly of an aircraft, by adding an insert, which fills and/or bridges the damaged portion. The method involves: producing a 3D CAD repair model of the damaged portion by scanning; analysing the repair model and thus evaluating complexity of the damage and/or its reconditioning; as a function of the complexity, deciding between at least two alternative means to perform at least a following step, which is analysing the repair model and thus dimensioning the reconditioning including the insert. Further, an insert is provided for filling and/or bridging a damaged portion for reconditioning of the damaged portion of a component, particularly of an aircraft, produced according to the method. | ||||||
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