| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | Method of producing solar battery semiconductor | JP3946676 | 1976-04-09 | JPS51123591A | 1976-10-28 | AASAA JII MIRUZU; DONARUDO ERU FUOIHITO |
| 122 | APPLICATOR REPAIR FOR ADDITIVE MANUFACTURING SYSTEM | US15619772 | 2017-06-12 | US20180354208A1 | 2018-12-13 | Donnell Eugene Crear; Mikhail Pavlov; Felix Martin Gerhard Roerig; Dean Andrew Snelling |
| An applicator repair system for an additive manufacturing (AM) system, and an AM system including the same are disclosed. The applicator repair system includes a repair device including a repair element configured to repair a damaged applicator element on an applicator of an AM system. The damaged applicator element is configured to distribute a layer of raw material on a build platform of the AM system. The repair device is positioned within a processing chamber of the AM system. A damaged applicator controller may be provided that is configured to cause repair of the damaged active applicator in response to the damaged applicator being identified as damaged. | ||||||
| 123 | Cyanoacrylate composition | US15027302 | 2014-10-22 | US10144851B2 | 2018-12-04 | Ciaran McArdle; Arnau Pejoan Jiménez; Juan Andrés López Maeso; Stefano Gherardi |
| The present invention relates to a cyanoacrylate composition having a heterogeneous curing initiator which is a hydrated calcium silicate. The composition is suitable for repairing and filling depressions, cracks, or holes in a substrate or between substrates to be bonded. It also relates to an adhesive comprising said composition, to a syringe containing it, to a method for bonding substrates, to the use of said composition, and to the use of said hydrated calcium silicate as curing agent for cyanoacrylate compositions. | ||||||
| 124 | PATTERNING OF LIQUID CRYSTALS USING SOFT-IMPRINT REPLICATION OF SURFACE ALIGNMENT PATTERNS | US15841037 | 2017-12-13 | US20180164645A1 | 2018-06-14 | Chulwoo Oh; Chieh Chang; Sharad Bhagat; Michael Anthony Klug |
| Soft-imprint alignment processes for patterning liquid crystal polymer layers via contact with a reusable alignment template are described herein. An example soft-imprint alignment process includes contacting a liquid crystal polymer layer with a reusable alignment template that has a desired surface alignment pattern such that the liquid crystal molecules of the liquid crystal polymer are aligned to the surface alignment pattern via chemical, steric, or other intermolecular interaction. The patterned liquid crystal polymer layer may then be polymerized and separated from the reusable alignment template. The process can be repeated many times. The reusable alignment template may include a photo-alignment layer that does not comprise surface relief structures that correspond to the surface alignment pattern and a release layer above this photo-alignment layer. A reusable alignment template and methods of fabricating the same are also disclosed. | ||||||
| 125 | Methods for forming radius fillers for composite structures | US15486149 | 2017-04-12 | US09993980B2 | 2018-06-12 | William Thomas Kline; Thomas Dean Wilson; Bruno Zbinden; Dalton C. Bergan; Joseph Fount Warren, Jr.; Nicholas A. Boroughs; Scott Edward Krajca |
| 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. | ||||||
| 126 | Structural repair having optical witness and method of monitoring repair performance | US14722149 | 2015-05-27 | US09931827B2 | 2018-04-03 | Gary E. Georgeson; Kenneth Harlan Griess; Russell Lee Keller; Everett A. Westerman |
| A structural repair includes a tell-tale optical witness that allows the health of the repair to be visually monitored. The optical witness includes a stress sensitive fluorescent dye that shows changes in local strain/stress patterns when the repair is subjected to electromagnetic energy of a particular wavelength. The dyes fluoresce more or less strongly as a function of the local stress/strain. | ||||||
| 127 | PANEL EDGE ENCLOSURES | US15789102 | 2017-10-20 | US20180037785A1 | 2018-02-08 | Sylvain E. Gleyal; Laurent Meistermann |
| The present invention contemplates a method for enclosing a panel edge comprising forming a panel structure having at least one edge, applying a reformable epoxy resin material onto the at least one edge, and contacting the reformable epoxy resin material within about 10 minutes, or even about 5 minutes of applying the reformable epoxy resin material such that the reformable epoxy resin material is below its glass transition temperature and dry to the touch upon contact. | ||||||
| 128 | METHOD AND DEVICE FOR MODIFYING CATALYST LAYER | US15546687 | 2015-02-02 | US20180026273A1 | 2018-01-25 | Hiroshi OKONOGI; Aurel FUNAR; Yasuhiro NUMAO; Tooru KOSEMURA; Takayuki HIRAO; Kimio NISHIMURA |
| A method is provided that modifies a catalyst layer of a membrane catalyst layer assembly, which is manufactured by transferring the catalyst layer formed on a transfer sheet onto an electrolyte membrane. In the catalyst layer correction method, presence or absence of a defect in the catalyst layer is detected. The defect is removed based on the size and position of the detected defect. The portion from which the defect has been removed is repaired by application thereto of a correcting ink corresponding to the catalyst layer. | ||||||
| 129 | Methods to dismantle hermetically sealed chambers | US15237953 | 2016-08-16 | US09809019B2 | 2017-11-07 | Raymond Miller Karam; Thomas Wynne; Anthony Thomas Chobot |
| Embodiments generally relate to apparatus and methods for dismantling a hermetically sealed chamber. In one embodiment, an apparatus facilitating the opening of a hermetically sealed chamber in a device comprises a fixture configured to hold the device, and a system configured to create sufficient tensile or shear stress at a bond interface of the seal to open the seal under controlled conditions. In one embodiment, a method for opening a hermetic seal between first and second elements forming a chamber in a microfluidic chip comprises using a release technique creating sufficient tensile or shear stress at a bond interface of the seal to open the seal under controlled conditions. The release technique comprises introducing a tool to the vicinity of the interface without any contact between the tool and any material within the chamber. The breaking of the seal results in the complete separation of the first and second elements. | ||||||
| 130 | Method for holding a panel | US14337679 | 2014-07-22 | US09789980B2 | 2017-10-17 | Paul R. Gehlsen |
| 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. | ||||||
| 131 | SYSTEMS AND METHODS FOR FORMING RADIUS FILLERS FOR COMPOSITE STRUCTURES | US15615453 | 2017-06-06 | US20170266942A1 | 2017-09-21 | 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 |
| 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. | ||||||
| 132 | AIRCRAFT FRAME STRUCTURE AND ASSOCIATED METHOD | US15328284 | 2015-07-17 | US20170210458A1 | 2017-07-27 | Guy TOTHILL; Laid ADDA; Anthony LANGLEY |
| An aircraft frame structure including a grid support (such as a geodetic support) (2) and (i) an impact-resistant barrier (6) including a shear thickening fluid, and (ii) a water-resistant, elastically-deformable cover (4). Methods to make and repair an aircraft using the aircraft frame structure. | ||||||
| 133 | Melamine resin decorative sheet and method of refurbishing finished surface | US14382719 | 2013-03-06 | US09707740B2 | 2017-07-18 | Kousuke Arai |
| A melamine resin decorative sheet of the present invention includes a laminate structure of a surface layer and a core layer, in which the surface layer is configured of a surface layer material composed of a surface layer base material which carries a resin containing a melamine resin on a first surface side that serves as a design surface and which carries a solid content of a thermoplastic emulsion resin on a second surface side that contacts with the core layer, and in which the core layer is configured of a heat dissipative material layer. | ||||||
| 134 | Monitoring composite manufacturing and repair processes using chromatic films | US15173718 | 2016-06-06 | US09656453B2 | 2017-05-23 | Gary Ernest Georgeson; Richard H. Bossi |
| A composite structure is processed using heat and pressure. A chromatic film is placed in proximity to the composite structure and is used to monitor at least one of the temperature of the heat and the pressure during processing. | ||||||
| 135 | Wrinkle diffuser system for composites | US14222617 | 2014-03-22 | US09649809B2 | 2017-05-16 | Tristan E. Lee; Andrew M. Hopkins; William T. Kline |
| 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. | ||||||
| 136 | REPAIRING A CONTOURED COMPOSITE PANEL | US14810375 | 2015-07-27 | US20170029088A1 | 2017-02-02 | Eric G. Gruner |
| A method for repairing damage caused to a curved composite-material panel may include removal of a sector including through-thickness damage, installation of a patch performed from an exterior side of the panel, buildup of the void caused by removal of the sector, and installation of one or more composite repair plies. | ||||||
| 137 | Monitoring Composite Manufacturing and Repair Processes Using Chromatic Films | US15173718 | 2016-06-06 | US20160279923A1 | 2016-09-29 | Gary Ernest Georgeson; Richard H. Bossi |
| A composite structure is processed using heat and pressure. A chromatic film is placed in proximity to the composite structure and is used to monitor at least one of the temperature of the heat and the pressure during processing. | ||||||
| 138 | DEVICES, SYSTEMS AND METHODS FOR INFLATABLE PATCHING | US15168790 | 2016-05-31 | US20160271891A1 | 2016-09-22 | William Woodruff |
| The present system, method and apparatus are adapted for the quick and easy patching of inflatable devices. More specifically, the system, apparatus and methods comprise a tip, a body portion, an adhesive, a patch and a probe, wherein the tip and body portion are inserted into the inflatable device so as to apply the adhesive and patch to the interior of the device to create an air-tight seal. The disclosure thus provides an improved patching system, apparatus and method. | ||||||
| 139 | Monitoring composite manufacturing and repair processes using chromatic films | US13791207 | 2013-03-08 | US09446575B1 | 2016-09-20 | Gary Ernest Georgeson; Richard H. Bossi |
| A composite structure is processed using heat and pressure. A chromatic film is placed in proximity to the composite structure and is used to monitor at least one of the temperature of the heat and the pressure during processing. | ||||||
| 140 | CYANOACRYLATE COMPOSITION | US15027302 | 2014-10-22 | US20160251548A1 | 2016-09-01 | Ciaran MCARDLE; Arnau PEJOAN JIMÉNEZ; Juan Andrés LÓPEZ MAESO; Stefano GHERARDI |
| The present invention relates to a cyanoacrylate composition having a heterogeneous curing initiator which is a hydrated calcium silicate. The composition is suitable for repairing and filling depressions, cracks, or holes in a substrate or between substrates to be bonded. It also relates to an adhesive comprising said composition, to a syringe containing it, to a method for bonding substrates, to the use of said composition, and to the use of said hydrated calcium silicate as curing agent for cyanoacrylate compositions. | ||||||
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