| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | Connection element, connection arrangement, method for producing a connection element and method for producing a connection arrangement | US15371890 | 2016-12-07 | US10150277B2 | 2018-12-11 | Thomas Meer |
| A connection element includes a composite component with a cured epoxy resin, a first layer including a first thermoplastic polymer and an intermediate layer arranged between the composite component and the first layer, the first layer containing both the cured epoxy resin of the composite component and the first thermoplastic polymer of the first layer. The first thermoplastic polymer has a melting point above a curing temperature of the epoxy resin and is soluble at a temperature of at least 150° C. in the epoxy resin used for producing the composite component. | ||||||
| 2 | Friction Heating for Joining Dissimilar Materials | US12196743 | 2008-08-22 | US20080308236A1 | 2008-12-18 | Yen-Lung Chen; Peter H. Foss; Mark W. Verbrugge; Xiaohong Q. Gayden |
| One side of a metal sheet is joined to a polymer layer by applying heat to a joining area on the opposite side of the metal. The heat flows through the thin metal to activate a thermoplastic material or heat setting polymer into a bond with the metal. The method can be used to bond the metal sheet to a plastic body or another metal member. It is preferred to use a friction or friction stir tool to heat the metal surface. | ||||||
| 3 | Method of sealing materials together by a rubbing treatment and articles produced thereby | US34556164 | 1964-02-18 | US3418196A | 1968-12-24 | JANE LUC |
| 4 | Composite Panel Tool | US15784501 | 2017-10-16 | US20180105290A1 | 2018-04-19 | 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. | ||||||
| 5 | Composite Panel Tool | US14337679 | 2014-07-22 | US20160023779A1 | 2016-01-28 | 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. | ||||||
| 6 | Friction heating for joining dissimilar materials | US12196743 | 2008-08-22 | US07955459B2 | 2011-06-07 | Yen-Lung Chen; Peter H. Foss; Mark W. Verbrugge; Xiaohong Q. Gayden |
| One side of a metal sheet is joined to a polymer layer by applying heat to a joining area on the opposite side of the metal. The heat flows through the thin metal to activate a thermoplastic material or heat setting polymer into a bond with the metal. The method can be used to bond the metal sheet to a plastic body or another metal member. It is preferred to use a friction or friction stir tool to heat the metal surface. | ||||||
| 7 | Plastics film and bags and sacks therefrom | EP83302759.2 | 1983-05-16 | EP0095299B1 | 1987-09-09 | Cowan, Michael Anthony |
| A thermoplastics bag whose wall includes first and second layers each formed by melt extrusion from a synthetic thermoplastics material, one of said layers comprising a blend of linear low density ethylene polymer and at least one of (a) a second ethylene polymer which has a higher density and is selected from ethylene homopolymers and copolymers of ethylene and at least one other alpha -olefin and (b) polypropylene, and the other of said layers comprising linear low density ethylene polymer; at least one of said layers providing a face of the wall and at least a part of the surface of the outer face of the wall having a higher coefficient of friction than the inner face. Also a multilayer film suitable for use in the manufacture of the bag. | ||||||
| 8 | COVER FOR A SEAT AND METHOD FOR PRODUCING A COVER | US15944937 | 2018-04-04 | US20190248105A1 | 2019-08-15 | Niels MONDELAERS; Uwe SCHULZE |
| A cover (1), in particular a backrest cover or a lateral cover for a vehicle seat, is molded from a covering material layer (2), in particular from a covering material blank (2.1) and from a carrier material layer (4), in particular from a carrier material blank (4.1). An adhesive non-woven (3) or an adhesive layer is disposed between the covering material blank (2.1) and the carrier material blank (4.1). | ||||||
| 9 | 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. | ||||||
| 10 | CONNECTION ELEMENT, CONNECTION ARRANGEMENT, METHOD FOR PRODUCING A CONNECTION ELEMENT AND METHOD FOR PRODUCING A CONNECTION ARRANGEMENT | US15371890 | 2016-12-07 | US20170157908A1 | 2017-06-08 | Thomas MEER |
| A connection element includes a composite component with a cured epoxy resin, a first layer including a first thermoplastic polymer and an intermediate layer arranged between the composite component and the first layer, the first layer containing both the cured epoxy resin of the composite component and the first thermoplastic polymer of the first layer. The first thermoplastic polymer has a melting point above a curing temperature of the epoxy resin and is soluble at a temperature of at least 150° C. in the epoxy resin used for producing the composite component. | ||||||
| 11 | Friction heating for joining dissimilar materials | US12196850 | 2008-08-22 | US07695656B2 | 2010-04-13 | Yen-Lung Chen; Peter H. Foss; Mark W. Verbrugge; Xiaohong Q. Gayden |
| One side of a metal sheet is joined to a polymer layer by applying heat to a joining area on the opposite side of the metal. The heat flows through the thin metal to activate a thermoplastic material or heat setting polymer into a bond with the metal. The method can be used to bond the metal sheet to a plastic body or another metal member. It is preferred to use a friction or friction stir tool to heat the metal surface. | ||||||
| 12 | Friction heating for joining dissimilar materials | US11466168 | 2006-08-22 | US07497917B2 | 2009-03-03 | Yen-Lung Chen; Peter H. Foss; Mark W. Verbrugge; Xiaohong Q. Gayden |
| One side of a metal sheet is joined to a polymer layer by applying heat to a joining area on the opposite side of the metal. The heat flows through the thin metal to activate a thermoplastic material or heat setting polymer into a bond with the metal. The method can be used to bond the metal sheet to a plastic body or another metal member. It is preferred to use a friction or friction stir tool to heat the metal surface. | ||||||
| 13 | Friction heating for joining dissimilar materials | US12196850 | 2008-08-22 | US20080302474A1 | 2008-12-11 | Yen-Lung Chen; Peter H. Foss; Mark W. Verbrugge; Xiaohong Q. Gayden |
| One side of a metal sheet is joined to a polymer layer by applying heat to a joining area on the opposite side of the metal. The heat flows through the thin metal to activate a thermoplastic material or heat setting polymer into a bond with the metal. The method can be used to bond the metal sheet to a plastic body or another metal member. It is preferred to use a friction or friction stir tool to heat the metal surface. | ||||||
| 14 | Friction Heating for Joining Dissimilar Materials | US11466168 | 2006-08-22 | US20070044901A1 | 2007-03-01 | Yen-Lung Chen; Peter Foss; Mark Verbrugge; Xiaohong Gayden |
| One side of a metal sheet is joined to a polymer layer by applying heat to a joining area on the opposite side of the metal. The heat flows through the thin metal to activate a thermoplastic material or heat setting polymer into a bond with the metal. The method can be used to bond the metal sheet to a plastic body or another metal member. It is preferred to use a friction or friction stir tool to heat the metal surface. | ||||||
| 15 | Plastics film and bags and sacks therefrom | EP83302759 | 1983-05-16 | EP0095299A3 | 1984-09-26 | Cowan, Michael Anthony |
A thermoplastics bag whose wall includes first and second layers each formed by melt extrusion from a synthetic thermoplastics material, one of said layers comprising a blend of linear low density ethylene polymer and at least one of (a) a second ethylene polymer which has a higher density and is selected from ethylene homopolymers and copolymers of ethylene and at least one other a-olefin and (b) polypropylene, and the other of said layers comprising linear low density ethylene polymer; at least one of said layers providing a face of the wall and at least a part of the surface of the outer face of the wall having a higher coefficient of friction than the inner face. Also a multilayer film suitable for use in the manufacture of the bag. |
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| 16 | Plastics film and bags and sacks therefrom | EP83302759.2 | 1983-05-16 | EP0095299A2 | 1983-11-30 | Cowan, Michael Anthony |
A thermoplastics bag whose wall includes first and second layers each formed by melt extrusion from a synthetic thermoplastics material, one of said layers comprising a blend of linear low density ethylene polymer and at least one of (a) a second ethylene polymer which has a higher density and is selected from ethylene homopolymers and copolymers of ethylene and at least one other a-olefin and (b) polypropylene, and the other of said layers comprising linear low density ethylene polymer; at least one of said layers providing a face of the wall and at least a part of the surface of the outer face of the wall having a higher coefficient of friction than the inner face. Also a multilayer film suitable for use in the manufacture of the bag. |
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| 17 | VERBINDUNGSELEMENT, VERBINDUNGSANORDNUNG, VERFAHREN ZUM HERSTELLEN EINES VERBINDUNGSELEMENTS UND VERFAHREN ZUM HERSTELLEN EINER VERBINDUNGSANORDNUNG | EP16202494.7 | 2016-12-06 | EP3199343A1 | 2017-08-02 | Meer, Thomas |
Die vorliegende Erfindung schafft ein Verbindungselement, mit: einem Verbundbauteil, welches ein gehärtetes Epoxidharz umfasst; einer ersten Schicht, welche ein erstes thermoplastisches Polymer umfasst; einer Zwischenschicht, welche zwischen dem Ver-bundbauteil und der ersten Schicht angeordnet ist und sowohl das gehärtete Epoxidharz des Verbundbauteils wie auch das erste thermoplastische Polymer der ersten Schicht enthält; wobei das erste thermoplastische Polymer eine Schmelztemperatur, insbesondere Glasübergangstemperatur, aufweist, die über einer Aushärtetemperatur des Epoxidharzes liegt; und wobei das erste thermoplastische Polymer bei einer Temperatur von mindestens 150 °C in dem Epoxidharz, das zur Herstellung des Verbundbauteils verwendet wird, lösbar ist. Die vorliegende Erfindung schafft ferner eine Verbindungsanordnung mit einem solchen Verbindungselement, ein Verfahren zum Herstellen eines solchen Verbindungselement sowie ein Verfahren zum Herstellen der Verbindungsanordnung.
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| 18 | TOOL FOR A COMPOSITE PANEL | EP15177606.9 | 2015-07-21 | EP2977320A1 | 2016-01-27 | Gehlsen, Paul R. |
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.
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