| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 261 | 복합체 패널 및 이의 제조 방법 | KR1020127011131 | 2010-09-30 | KR101359827B1 | 2014-02-07 | 데이스티븐더블유; 셰파드마이클에스; 스톨프레데릭; 틸톤대니 |
| 저밀도 셀형 물질, 예를 들어 발포체 플라스틱의 복수개의 조각들은 대향 측면을 갖는 코어 패널을 형성하고, 여기서 인접하는 상기 조각들은, 상기 측면들 사이에서 연장되는 마주보는 가장자리면을 갖는다. 가요성 물질의 시트, 예를 들어 시트 또는 매트 또는 스크림은 상기 측면에 접착제로 부착되고, 하나의 시트의 일부가 상기 패널의 구부러짐을 제한하기 위해서, 인접하는 상기 마주보는 가장자리면들 사이에서 연장된다. 상기 조각들은 테이퍼링되고, 하나의 시트의 일부가 가장자리면들 사이에서 돌출되어, 부분적으로 또는 전체적으로 이중벽 웹을 형성할 수 있다. 상기 웹들은, 상기 대향 측면들 위의 다른 시트에 접착제로 부착된 플랜지를 가질 수 있다. 하나의 시트는, 대향 측면 상에서 시트에 의해 유지되는 편평한 상태로부터 패널이 구부러지도록 하기 위하여, 상기 조각들에 접착제로 부착되지 않는 영역에서 연신성일 수도 있다.
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| 262 | 복합 구조체의 개선 또는 복합 구조체에 관한 개선 | KR1020117027845 | 2010-04-23 | KR101311976B1 | 2013-09-26 | 애플턴스티브; 닐센크누드스텐벡 |
| 복합 구조체용 코어가 개시된다. 그 코어는 제1 코어 층, 제2 코어 층, 및 제1 코어 층과 제2 코어 층 사이의 간층 영역을 구비한다. 제1 코어 층과 제2 코어 층 중의 적어도 하나는 간층 영역을 방해하지 않고 코어의 걸쳐짐을 용이하게 하는 힌지 부분들을 구비한다. 그 간층 영역은 레이더 반사 층 및/또는 광학 섬유들과 같은 기능성을 포함할 수 있다. 대안적으로, 그 코어는 제1 코어 층과 제2 코어 층을 함께 접합시키기 위한 접착층을 포함하는 간층 영역을 구비한 접합 코어일 수 있다.
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| 263 | 섬유 강화 복합 몰딩 | KR1020137002807 | 2011-07-01 | KR1020130089244A | 2013-08-09 | 보르자,아다스미야라밀러레이; 두모라드,진클라우데; 라르센,플레밍; 쇠플링거,만프레드 |
| 본 발명은 외부 구조(102) 및 내부 구조(106)를 갖는 섬유-강화 복합 몰딩으로서, 외부 구조(102)는 적어도 하나의 섬유 강화 물질 층 및 경화된 제 1 수지 물질로부터 형성되며, 내부 구조(106)는 복수의 섬유 강화 물질 층 및 경화된 제 2 수지 물질로부터 형성되며, 비경화된 제 1 수지 물질의 점도는 비경화된 제 2 수지 물질의 점도 보다 낮으며, 복합 몰딩에서 두 개의 수지 물질은 서로 적어도 일부 혼합되는, 섬유-강화 복합 몰딩에 관한 것이다. 본 발명은 또한, 이러한 섬유-강화 복합 몰딩의 생산 방법에 관한 것이다.
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| 264 | 풍력 발전소에서의 층 구조의 용도 | KR1020127015048 | 2010-12-06 | KR1020120104573A | 2012-09-21 | 파스만,디르크; 프란켄,클라우스; 린드너,스테판 |
| 본 발명은 풍력 발전소용 로터 블레이드의 제조에서의 층 구조의 용도, 및 풍력 발전소용 로터 블레이드에 관한 것이다. | ||||||
| 265 | 열적 항빙 장치를 위한 변형 가능한 전도성/저항성 복합혼성 히터 | KR1020077027512 | 2006-05-26 | KR1020080033155A | 2008-04-16 | 올드로이드,폴,케이. |
| A rotor blade of a helicopter is presented. In an embodiment, the rotor blade includes a body; and a heating mat arranged in the body and configured to supply heat to said body. The heating mat includes a first plurality of fibers and a second plurality of fibers electrically connected to the first plurality of fibers. The first plurality of fibers define a positive angle smaller than about +45° relative to a first direction perpendicular to a longitudinal direction of the body. The second plurality of fibers define a negative angle greater than about-45° relative to the first direction. | ||||||
| 266 | 풍력발전 터빈 블레이드용 탄소-유리섬유 하이브리드복합체 제조방법 | KR1020060124850 | 2006-12-08 | KR100759595B1 | 2007-09-18 | 한인섭; 김세영; 서두원; 홍기석; 이시우; 유지행; 우상국 |
| A method for manufacturing a carbon-glass fiber hybrid composite for a wind turbine blade is provided to increase rigidity and strength by aligning carbon fibers in the center of the carbon-glass fiber hybrid composite and to decrease the density by 10%. A method for manufacturing a carbon-glass fiber hybrid composite for a wind turbine blade comprises the steps of: treating glass fiber and carbon fiber with a releasing agent by VARTM(Vacuum Assisted Resin Transfer Molding) and forming the composite by positioning the carbon fiber in a middle layer and stacking the glass fiber on upper and lower layers in the same thickness on a dried mold(S1); successively stacking a peel ply fabric cloth and a mat for improving the flow of resin, on the glass fiber forming the upper layer and covering and sealing the part of the mold except a resin injection port and a vacuum port, with a transparent nylon bagging film(S2); pressing the stacked fibers by closing up the resin injection port and reducing pressure through the vacuum port over 1 atmosphere(S3); impregnating the fiber with resin by injecting the resin into the sealed mold through vacuum pressure by opening the resin injection port, and then closing up the resin injection port to cut off the inflow of the air(S4); and hardening the resin with continuously applying vacuum pressure to the inside of the mold(S5). | ||||||
| 267 | HIGH-MODULUS COATING FOR LOCAL STIFFENING OF AIRFOIL TRAILING EDGES | PCT/US2014045929 | 2014-07-09 | WO2015053832A3 | 2015-06-18 | TWELVES WENDELL V; COOK III GRANT O |
| An airfoil is disclosed. The airfoil may comprise a leading edge, a body portion and a trailing edge formed from a high-modulus plating. The body portion of the airfoil may be formed from a material having a lower elastic modulus than the high-modulus plating. The high-modulus plating may improve the stiffness of the trailing edge, allowing for thinner trailing edges with improved fatigue life to be formed. | ||||||
| 268 | FAST CURE EPOXY RESIN SYSTEMS | PCT/EP2013077863 | 2013-12-20 | WO2014096435A2 | 2014-06-26 | HARRINGTON CHRIS |
| A fast cure epoxy resin system is provided that upon curing has a Tg no greater than 140°C and a Phase angle below 20° at a temperature of 140°C or below, and prepregs and mouldings based on the system. The resin formulation matches the reactivity of the resin to the amount of curative and hardener employed. | ||||||
| 269 | ARTICLE INCLUDING AIRFOIL OR HYDROFOIL AND METHOD OF MAKING THE SAME | PCT/US2011064515 | 2011-12-13 | WO2012082667A3 | 2013-02-28 | IZZI GUGLIELMO M; FRONEK DANIEL R; HERDTLE THOMAS; SEWALL NELSON D; MAZUREK MIECZYSLAW H; FLEMING DANNY L; JONES VIVIAN W |
| An article including an airfoil or hydrofoil is disclosed. On at least a portion of a surface of the airfoil or hydrofoil there is a seamless film having a series of substantially parallel peaks separated from each other by a series of substantially parallel valleys on a patterned first surface of the film, wherein the seamless film has a long dimension that is at least two meters long substantially aligned with the span of the airfoil or hydrofoil, and wherein an angle between the parallel peaks and valleys to the long dimension of the seamless film is at least five degrees. Methods of making the article are also disclosed. | ||||||
| 270 | COMPOSITE TAPE FOR USE IN AUTOMATED TAPE LAYING MACHINES | PCT/IB2008000431 | 2008-02-18 | WO2009104040A3 | 2009-12-03 | ELLIS JOHN |
| A tape for use in automated tape laying machines that includes a multi-layer substrate composed of a plastic layer that includes at least one plastic film having an outer film surface and an inner film surface. The plastic film is adhered to a fibrous layer so that the inner surface of the fibrous layer is bonded to the inner film surface. An uncured composite material layer composed of a fibrous reinforcement and an uncured resin matrix is releasably adhered to either the plastic layer surface or the outer fiber layer surface to provide a tape suitable for use in an automatic tape layer. | ||||||
| 271 | STRAINED CAPABLE CONDUCTIVE/RESISTIVE COMPOSITE HYBRID HEATER FOR THERMAL ANTI-ICE DEVICE | PCT/US2006020377 | 2006-05-26 | WO2006130454A3 | 2007-08-09 | OLDROYD PAUL K |
| A rotor blade of a helicopter is presented. In an embodiment, the rotor blade (100) includes a body (105) ; and a heating mat (301) arranged in the body (105) and configured to supply heat to said body. The heating mat (301) includes a first (505) plurality of fibers (400) and a second (510) plurality of fibers (400) electrically connected to the first plurality of fibers. The first plurality of fibers define a positive angle smaller than about +45° relative to a first direction perpendicular to a longitudinal direction of the body. The second plurality of fibers define a negative angle greater than about -45° relative to the first direction. | ||||||
| 272 | COMPOSITE ARTICLES COMPRISING PROTECTIVE SHEETS AND RELATED METHODS | PCT/US2006060160 | 2006-10-23 | WO2007048141A2 | 2007-04-26 | MCGUIRE JAMES E; STRANGE ANDREW C |
| Methods of the invention include those for applying protective sheets to composite articles. According to these methods and resulting composite articles, a protective sheet is applied to at least a portion of an exterior surface formed from a composite material and where protection is desired. At least one exterior surface of the composite article to be protected can be integrally formed in the presence of the protective sheet. Improved bonding of the protective sheet to the composite article and improved processing efficiency are advantageously achieved according to the invention. | ||||||
| 273 | DOUBLE-LAYER COMPONENT, METHOD FOR PRODUCING A DOUBLE-LAYER COMPONENT AND HEAT ENGINE COMPRISING A PLURALITY OF DOUBLE-LAYER COMPONENTS | US16343400 | 2017-10-19 | US20190242369A1 | 2019-08-08 | Martin Huber |
| The invention relates to a double-layer component (1) having a first layer (2) and a second layer (3), wherein the layers (2, 3) are connected to one another, wherein the two layers (2, 3) have different coefficients of thermal expansion, wherein the first layer (2) comprises a first plastic and the second layer (3) comprises a second plastic or carbon fibres, wherein the double-layer component (1) is reversibly deformable under the influence of heat. The double-layer component (1) is improved in that the double-layer component (1) can be inserted into a heat engine (4), wherein the thickness of the double-layer component (1) is at least 0.1 mm, wherein the thickness of the double-layer component (1) is 5 cm or less than 5 cm. | ||||||
| 274 | WIND TURBINE GENERATOR SYSTEM, WIND TURBINE BLADE, AND REINFORCING METHOD FOR WIND TURBINE BLADE | US16019462 | 2018-06-26 | US20180306167A1 | 2018-10-25 | Yasutaka KIMURA; Takao KUROIWA; Keisuke OTA |
| A wind turbine blade is reinforced while suppressing possible stress concentration resulting from a load imposed on a blade root portion of the wind turbine blade in a flap direction. The wind turbine blade includes a blade main body extending from the blade root portion toward a blade tip portion and an FRP reinforcing layer formed so as to cover at least a part of the outer surface of the blade root portion of the blade main body. The FRP reinforcing layer includes a plurality of laminated fiber layers and a resin with which the plurality of fiber layers is impregnated. The FRP reinforcing layer is formed such that, in a cross section along a longitudinal direction of the blade main body, both ends of the plurality of laminated fiber layers in the longitudinal direction are tapered. | ||||||
| 275 | Fiber-reinforced composite material | US14378726 | 2013-02-12 | US10081157B2 | 2018-09-25 | Yoshihiro Fukuda; Takayuki Matsumoto; Masaki Minami; Naoyuki Sekine; Masanori Nakajima |
| A fiber-reinforced composite material is provided which is capable of achieving CAI, ILSS, and interlaminar fracture toughness concurrently at high levels, in particular, capable of achieving high CAI. The composite material is composed of a laminated body including a plurality of reinforcing-fiber-containing layers and a resin layer in each interlaminar region between adjacent reinforcing-fiber-containing layers, wherein the resin layer is a layer wherein a cured product of a compound having in its molecule a benzoxazine ring of formula (1) and epoxy resin is impregnated with at least polyamide 12 powder: (R1: C1-C12 chain alkyl group or the like; H is bonded to at least one of the carbon atoms of the aromatic ring at ortho- or para-position with respect to C to which the oxygen atom is bonded). | ||||||
| 276 | PREFORM, FIBER-REINFORCED COMPOSITE MATERIAL, AND METHOD OF MANUFACTURING FIBER-REINFORCED COMPOSITE MATERIAL | US15548268 | 2016-02-02 | US20180264754A1 | 2018-09-20 | Masanori Hirano; Kazunori Hondo; Nobuyuki Tomioka |
| A preform includes a plurality of reinforcement fiber layers connected to each other by binder resin, the binder resin containing spacer particles insoluble in the binder resin, the spacer particles accounting for a volume proportion of 10% to 80% in the binder resin present in interlaminar gaps between the reinforcement fiber layers. | ||||||
| 277 | FIBER-REINFORCEMENT OF BLOWING-AGENT CONTAINING FOAM MATERIALS | US15538704 | 2015-12-15 | US20180257345A1 | 2018-09-13 | Holger RUCKDÄSCHEL; Rene ARBTER; Robert STEIN; Daniela LONGO-SCHEDEL; Tim DIEHLMANN; Bangaru SAMPATH; Peter GUTMANN; Alexandre TERRENOIRE; Markus HARTENSTEIN; Andreas KIRGIS; Alessio MORINO; Gregor DAUN; Marc Claude MARTIN; Peter MERKEL; Thomas KICIAK |
| The present invention relates to a process for producing a molding made from blowing agent-containing foam comprising at least one fiber (F), wherein the at least one fiber (F) is partially introduced into the blowing agent-containing foam. The two ends of the respective fiber (F) that are not surrounded by the blowing agent-containing foam thus project from one side of the corresponding molding. The present invention also provides the molding as such. The present invention further provides a panel comprising at least one such molding, produced by the process according to the invention, and at least one further layer (S1). The present invention also provides for the production of the panels of the invention and for the use thereof, for example as a rotor blade in wind turbines. | ||||||
| 278 | Spar cap for a wind turbine rotor blade formed from pre-cured laminate plates of varying thicknesses | US14754764 | 2015-06-30 | US10072632B2 | 2018-09-11 | Aaron A. Yarbrough; Christopher Daniel Caruso |
| A spar cap for a rotor blade of a wind turbine may generally include an assembly of pre-cured laminate plates stacked on one top of the other, with the assembly including an outermost pre-cured plate, an innermost pre-cured plate positioned opposite the outermost pre-cured plate and a plurality of intermediate pre-cured plates stacked directly between the outermost and innermost pre-cured plates. The outermost pre-cured plate may be configured to be positioned adjacent to an inner surface of a body shell of the rotor blade. In addition, the outermost pre-cured plate may define a plate thickness that differs from a plate thickness defined by the innermost pre-cured plate by at least 50%. | ||||||
| 279 | WIND TURBINE GENERATOR SYSTEM, WIND TURBINE BLADE, AND REINFORCING METHOD FOR WIND TURBINE BLADE | US15705245 | 2017-09-14 | US20180223799A1 | 2018-08-09 | Yasutaka KIMURA; Takao KUROIWA; Keisuke OTA |
| A wind turbine blade is reinforced while suppressing possible stress concentration resulting from a load imposed on a blade root portion of the wind turbine blade in a flap direction. The wind turbine blade includes a blade main body extending from the blade root portion toward a blade tip portion and an FRP reinforcing layer formed so as to cover at least a part of the outer surface of the blade root portion of the blade main body. The FRP reinforcing layer includes a plurality of laminated fiber layers and a resin with which the plurality of fiber layers is impregnated. The FRP reinforcing layer is formed such that, in a cross section along a longitudinal direction of the blade main body, both ends of the plurality of laminated fiber layers in the longitudinal direction are tapered. | ||||||
| 280 | Bar of composite matrix material | US14228557 | 2014-03-28 | US10040546B2 | 2018-08-07 | Rupert Pfaller; Wolfgang J. Wagner; Martin Ortner |
| In a rotary wing aircraft a bar (1) of composite matrix material has a longitudinal axis (8) perpendicular to a cross section with upper and lower surfaces (2, 3). At least one torsion box (17) comprises an upper and a lower layers (10, 21, 11, 22) respectively offset of a longitudinal axis (8) and of the upper and the lower surfaces (2, 3), said upper and lower layers (10, 21, 11, 22) being laterally joint, while cross sections are filled with the first group of fibers extending essentially parallel to the longitudinal axis (8). | ||||||
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