序号 | 专利名 | 申请号 | 申请日 | 公开(公告)号 | 公开(公告)日 | 发明人 |
---|---|---|---|---|---|---|
21 | AIRCRAFT COMPONENT WITH CLOSED BOX STRUCTURE | US15152886 | 2016-05-12 | US20160332409A1 | 2016-11-17 | Jonathan PRICE; Chetan KORYA; Peter BAKER; Stephen WILLIAMS |
A method of manufacturing an aircraft component, the component comprising a pair of covers joined by a pair of spars. The covers and spars form a closed box structure with four corners, each corner providing a transition between one of the covers and one of the spars. The method comprises: laying up a laminated sheet of fibre plies; and after the sheet has been laid up, folding the sheet to form the four corners and then joining the sheet to itself to provide the closed box structure. | ||||||
22 | Long casing patch method | US14408508 | 2014-03-26 | US09481156B2 | 2016-11-01 | Toshikazu Igi |
To reduce operation time and ensure strength of a covering member.The method includes; causing the first sheet to memorize a shape of curvature having a predetermined radius of curvature by curing a first resin while holding the first sheet with the predetermined radius of curvature, the first sheet being impregnated with the first resin (S1); wrapping the first sheet around a radially expandable cylindrical packer and tentatively fastening the first sheet to the packer, wherein the packer has a radius that is smaller than the predetermined radius of curvature (S3); forming a laminated sheet assembly by attaching a plurality of sheets to each other with a second resin (S2); forming the covering member by wrapping the laminated sheet assembly around an outer surface of the first sheet via a third resin and tentatively fastening the laminated sheet assembly, the first sheet being wrapped around the packer (S4); applying a fourth resin to an outer surface of the laminated sheet assembly of the covering member and inserting the packer into a cylindrical tube (S5); radially expanding the packer in the cylindrical tube to release the tentative fastening of the first sheet and the laminated sheet assembly, thereby pressing the covering member against an inner wall of the cylindrical tube via the fourth resin (S6); pulling out the packer from the cylindrical tube (S7); and curing the second (S8). | ||||||
23 | CELL FORMING STRUCTURES AND THEIR USE IN DISPOSABLE CONSUMER PRODUCTS | US14850040 | 2015-09-10 | US20160067940A1 | 2016-03-10 | Tina LIEBE; Mathias Konrad HIPPE; Mark James KLINE |
The invention refers to a disposable absorbent article such as a diaper, a pant or a sanitary napkin. The disposable absorbent article further comprises a structure which is able to elongate and simultaneously convert from an initial flat configuration into an erected configuration. | ||||||
24 | ABSORBENT ARTICLES COMPRISING CELL FORMING STRUCTURES | US14479838 | 2014-09-08 | US20150073372A1 | 2015-03-12 | Matthias Konrad Hippe; Tina Liebe; Mark James Kline |
The invention refers to a disposable absorbent article such as a diaper, a pant or a sanitary napkin. The disposable absorbent article further comprises a structure which is able to elongate and simultaneously convert from an initial flat configuration into an erected configuration. | ||||||
25 | ABSORBENT ARTICLES COMPRISING EXTENSIBLE STRUCTURES WHICH INCREASE IN CALIPER | US14479883 | 2014-09-08 | US20150073369A1 | 2015-03-12 | Matthias Konrad Hippe; Tina Liebe; Mark James Kline |
The invention refers to a disposable absorbent article such as a diaper, a pant or a sanitary napkin. The disposable absorbent article further comprises a structure which is able to elongate and simultaneously convert from a flat configuration into an erected configuration. The structure consists of non-extensible and non-elastic materials. | ||||||
26 | Aircraft component with closed box structure | US15152886 | 2016-05-12 | US10118348B2 | 2018-11-06 | Jonathan Price; Chetan Korya; Peter Baker; Stephen Williams |
A method of manufacturing an aircraft component, the component comprising a pair of covers joined by a pair of spars. The covers and spars form a closed box structure with four corners, each corner providing a transition between one of the covers and one of the spars. The method comprises: laying up a laminated sheet of fiber plies; and after the sheet has been laid up, folding the sheet to form the four corners and then joining the sheet to itself to provide the closed box structure. | ||||||
27 | Molding compact, and manufacturing method for transdermal absorption sheet | US14709640 | 2015-05-12 | US10029081B2 | 2018-07-24 | Yanlong Che; Takayoshi Oyamada; Junya Yoshida; Shotaro Ogawa |
A molding compact for forming a transdermal absorption sheet on which a needle-shaped protruding part is arranged is a molding compact that is a laminate of: a first member having a needle-shaped recessed part formed on a front surface thereof, the needle-shaped recessed part being an inverse of the needle-shaped protruding part; a second member provided on a back surface of the first member, the second member being composed of a waterproof and moisture-permeable material; and a third member provided on a back surface of the second member, the third member being composed of a rigid body. Provided are a molding compact that makes it possible to prevent leakage of a drug-containing solution filled into the needle-shaped recessed part, and a manufacturing method for a transdermal absorption sheet using the molding compact. | ||||||
28 | Hollow body, process for manufacturing it and use thereof in a vehicle | US14367668 | 2012-12-21 | US09731485B2 | 2017-08-15 | Bjorn Criel; Pierre De Keyzer; Eric Boucaux |
A process for manufacturing a hollow body including a thermoplastic wall and a fibrous reinforcement welded on at least one portion of the surface of the wall, or its outer surface, the fibrous reinforcement including a thermoplastic similar to or compatible with that of the wall of the hollow body, having a thickness of at least 1 mm and from 30 to 60% in weight of fibers, the method including heating a portion of the outer surface of the hollow body where the reinforcement will be welded; heating the fibrous reinforcement to soften or melt the thermoplastic of the reinforcement; and moving the reinforcement and applying the reinforcement to the portion of the outer surface of the hollow body. The applying the reinforcement includes: applying an initial pressure on at least one portion of the reinforcement; and applying pressure for a final welding using robotized pressure applying mechanism. | ||||||
29 | Flexible PCM Sheet Materials | US15311633 | 2015-05-19 | US20170087799A1 | 2017-03-30 | Dirk BÜTTNER; Angelo SCHÜTZ; Martin GEISSENHÖNER |
The invention relates to flexible PCM sheet materials having a high latent thermal energy storage density for the purpose of heat management. The flexible PCM sheet material includes a flexible supporting structure and phase-change-material elements arranged thereon separately in a specific geometry. The phase-change-material elements are geometrically defined structures composed of polymer-bound phase-change material. The flexible PCM sheet materials are characterized by a high latent heat storage capacity and optimized thermal conductivity, are dimensionally stable even in the event of temperature changes and after phase transitions, can be rolled, folded, wound, or cut to size without problems, and can be transported, stored processed, or used in a single layer or in multiple layers. | ||||||
30 | METHOD OF FORMING COMPOSITE STRUCTURES | US15153216 | 2016-05-12 | US20160332392A1 | 2016-11-17 | Jonathan PRICE; Steven EVANS |
A method of forming composite components is described in which a composite lay-up is created using varying fibre types across the lay-up. This can adapt the lay-up to forming processes in regions of the lay-up to be formed and uses fibre types which give the greatest strength benefits in areas which do not need to be formed. Regions not requiring forming may have binders in them activated prior to a forming step or steps, after which the formed regions may be impregnated with a matrix and the component cured. | ||||||
31 | MOLDING COMPACT, AND MANUFACTURING METHOD FOR TRANSDERMAL ABSORPTION SHEET | US14709640 | 2015-05-12 | US20150238743A1 | 2015-08-27 | Yanlong CHE; Takayoshi OYAMADA; Junya YOSHIDA; Shotaro OGAWA |
A molding compact for forming a transdermal absorption sheet on which a needle-shaped protruding part is arranged is a molding compact that is a laminate of: a first member having a needle-shaped recessed part formed on a front surface thereof, the needle-shaped recessed part being an inverse of the needle-shaped protruding part; a second member provided on a back surface of the first member, the second member being composed of a waterproof and moisture-permeable material; and a third member provided on a back surface of the second member, the third member being composed of a rigid body. Provided are a molding compact that makes it possible to prevent leakage of a drug-containing solution filled into the needle-shaped recessed part, and a manufacturing method for a transdermal absorption sheet using the molding compact. | ||||||
32 | CELL FORMING STRUCTURES | US14479783 | 2014-09-08 | US20150073324A1 | 2015-03-12 | Tina Liebe; Matthias Konrad Hippe |
The invention refers to a disposable absorbent article such as a diaper, a pant or a sanitary napkin. The disposable absorbent article further comprises a structure which is able to elongate and simultaneously convert from an initial flat configuration into an erected configuration. | ||||||
33 | POLYURETHANE LAMINATES MADE WITH A DOUBLE BELT PRESS | US13668211 | 2012-11-02 | US20130115412A1 | 2013-05-09 | Gopalkrishna PADMANABHAN |
A fiber reinforced composite laminate with fibers generally oriented along two major axes and having a polyurethane resin matrix suitable for reinforcing wood based substrates such as trailer/container flooring, glulams, plywood, particle boards, laminated veneer lumber, and oriented strand board, is provided. The laminate is produced by pulling the fibers through a resin injection box, where a polyurethane resin is injected into the box to wet the fibers. The polyurethane resin wetted fiber layer is then covered with a release media on the top and bottom sides of the layer. The sandwich of fiber, resin and release media is fed to a double belt press capable of applying pressure and heat to consolidate and cure the laminate. The laminate thus made can be thinner than 0.080 inch and provides excellent flatness compared to pultruded thin laminates. | ||||||
34 | LONG CASING PATCH CONSTRUCTION METHOD | EP14867591 | 2014-03-26 | EP3012399A4 | 2017-01-25 | IGI TOSHIKAZU |
To reduce operation time and ensure strength of a covering member. The method includes; causing the first sheet to memorize a shape of curvature having a predetermined radius of curvature by curing a first resin while holding the first sheet with the predetermined radius of curvature, the first sheet being impregnated with the first resin (S1); wrapping the first sheet around a radially expandable cylindrical packer and tentatively fastening the first sheet to the packer, wherein the packer has a radius that is smaller than the predetermined radius of curvature (S3); forming a laminated sheet assembly by attaching a plurality of sheets to each other with a second resin (S2); forming the covering member by wrapping the laminated sheet assembly around an outer surface of the first sheet via a third resin and tentatively fastening the laminated sheet assembly, the first sheet being wrapped around the packer (S4); applying a fourth resin to an outer surface of the laminated sheet assembly of the covering member and inserting the packer into a cylindrical tube (S5); radially expanding the packer in the cylindrical tube to release the tentative fastening of the first sheet and the laminated sheet assembly, thereby pressing the covering member against an inner wall of the cylindrical tube via the fourth resin (S6); pulling out the packer from the cylindrical tube (S7); and curing the second (S8). | ||||||
35 | AIRCRAFT COMPONENT WITH CLOSED BOX STRUCTURE | EP16169115.9 | 2016-05-11 | EP3093121A1 | 2016-11-16 | Price, Jonathan; Korya, Chetan; Baker, Peter; Williams, Stephen |
A method of manufacturing an aircraft component, the component comprising a pair of covers (2,3) joined by a pair of spars (4,5). The covers and spars form a closed box structure with four corners (6,7,8,9), each corner providing a transition between one of the covers and one of the spars. The method comprises: laying up a laminated sheet of fibre plies; and after the sheet has been laid up, folding the sheet to form the four corners and then joining the sheet to itself to provide the closed box structure. |
||||||
36 | CELL FORMING STRUCTURES | EP14766640.8 | 2014-09-08 | EP3043758A1 | 2016-07-20 | HIPPE, Matthias, Konrad; LIEBE, Tina; KLINE, Mark, James |
The invention refers to a disposable absorbent article such as a diaper, a pant or a sanitary napkin. The disposable absorbent article further comprises a structure which is able to elongate and simultaneously convert from an initial flat configuration into an erected configuration. | ||||||
37 | MULTI-LEVEL CELL FORMING STRUCTURES AND THEIR USE IN DISPOSABLE CONSUMER PRODUCTS | EP14184265.8 | 2014-09-10 | EP2995289A1 | 2016-03-16 | Liebe, Tina; Hippe, Matthias Konrad; Kline, Mark |
The invention refers to a structure which is able to elongate and simultaneously convert from an initial flat configuration into an erected configuration and which comprises multiple levels. The structure may be part of a flexible package or of a disposable absorbent article such as a diaper, a pant or a sanitary napkin. |
||||||
38 | リフトオフ方法 | JP2014020126 | 2014-02-05 | JP6294090B2 | 2018-03-14 | 森數 洋司 |
39 | キャリパが増大する伸展性オーゼティック構造体を含む吸収性物品 | JP2016540453 | 2014-09-08 | JP6227787B2 | 2017-11-08 | マティアス、コンラッド、ヒッペ; ティナ、リーベ; マーク、ジェームズ、クライン |
40 | キャリパが増大する伸展性オーゼティック構造体を含む吸収性物品 | JP2016540453 | 2014-09-08 | JP2016533843A | 2016-11-04 | マティアス、コンラッド、ヒッペ; ティナ、リーベ; マーク、ジェームズ、クライン |
本発明は、おむつ、パンツ又は生理用ナプキンなどの使い捨て吸収性物品に関する。使い捨て吸収性物品は、伸長し、同時に、扁平構成から直立構成へ変形することができる構造体を更に含み、その直立構成はより高いキャリパ(厚さ)を有する。構造体は非伸展性及び非弾性材料からなる。 |