公开(公告)号：EP2660146A1

公开(公告)日：2013-11-06

申请号：EP12305486.8

申请日：2012-04-30

申请人： Hamilton Sundstrand Corporation ,  RATIER-FIGEAC

发明人： Nagle, David P. ,  Brion, Patrice ,  Prunet, Ludovic

IPC分类号： B64C11/26 ,  B64C27/473

CPC分类号： F01D5/147 ,  B64C11/26 ,  Y10T29/49332

摘要： A propeller blade (100) includes a foam core (205) and a structural layer formed of multiple layers (206a, 206b) that surrounds at least a portion of the foam core (205). The structural layer includes a mid-thickness location defined between the foam core and an outer edge of the structural layer and the multiple layers (206a, 206b) include at least one unidirectional layer (206b) and at least one biased layer (206b) disposed asymmetrically about the mid-thickness location.

摘要翻译： 螺旋桨叶片（100）包括泡沫芯（205）和由围绕泡沫芯（205）的至少一部分的多层（206a，206b）形成的结构层。 结构层包括限定在泡沫芯和结构层的外边缘之间的中间厚度位置，并且多层（206a，206b）包括至少一个单向层（206b）和至少一个偏置层（206b） 不对称地关于中间厚度位置。

公开(公告)号：EP2594482A1

公开(公告)日：2013-05-22

申请号：EP11195396.4

申请日：2011-12-22

申请人： Bell Helicopter Textron Inc.

发明人： Stamps, Frank B. ,  Tisdale, Patrick ,  Corrigan, John J.

IPC分类号： B64C27/51 ,  B64C29/00

CPC分类号： B64C27/51 ,  B64C27/635 ,  B64C29/0033 ,  Y10T29/49332

摘要： A rotor hub assembly (103, 203, 301) and method for controlling movement of a rotor blade (107, 303) relative to a swashplate (305). The hub assembly having an attachment device (315) operably associated with the rotor blade and the swashplate. The attachment device provides pivot and rotational blade movement relative to the swashplate. A dual spring-rate damper (321, 323) is operably associated with the attachment device. The damper (321, 323) switches between a first spring rate and a second spring rate during flight to control movement of the rotor blade. The method includes the process of switching the damper between the first spring rate and the second spring rate during flight.

摘要翻译： 一种用于控制转子叶片（107,303）相对于斜盘（305）的运动的转子轮毂组件（103,203,301）和方法。 轮毂组件具有可操作地与转子叶片和斜盘相关联的附接装置（315）。 附接装置提供了相对于斜盘的枢转和旋转刀片运动。 双弹簧阻尼器（321,323）可操作地与附接装置相关联。 阻尼器（321,323）在飞行期间在第一弹簧刚度和第二弹簧刚度之间切换，以控制转子叶片的运动。 该方法包括在飞行期间将阻尼器在第一弹簧刚度和第二弹簧刚度之间切换的过程。

公开(公告)号：EP2134963A4

公开(公告)日：2013-02-27

申请号：EP07842393

申请日：2007-09-13

申请人： MODULAR WIND ENERGY INC

发明人： BAKER MYLES L ,  ARENDT CORY P

IPC分类号： F03D1/06

CPC分类号： F03D1/0633 ,  F03D1/0675 ,  F05B2250/71 ,  F05B2280/6003 ,  F05B2280/6013 ,  F05C2253/04 ,  F05C2253/16 ,  Y02E10/721 ,  Y10T29/49332

公开(公告)号：EP2229258B1

公开(公告)日：2012-08-29

申请号：EP08871133.8

申请日：2008-12-20

申请人： MTU Aero Engines GmbH

发明人： BAYER, Erwin ,  BUSSMANN, Martin ,  PLATZ, Albin

IPC分类号： B23H9/10

CPC分类号： B23H9/10 ,  Y10T29/49332

公开(公告)号：EP2061699B1

公开(公告)日：2012-05-16

申请号：EP07872598.3

申请日：2007-08-03

申请人： Bell Helicopter Textron Inc.

发明人： AGNIHOTRI, Ashok, K. ,  NARRAMORE, Jimmy, C. ,  SCHILLINGS, John, J.

IPC分类号： B64C27/467

CPC分类号： B64C27/467 ,  Y10S416/02 ,  Y10T29/49332

摘要： One embodiment of the present invention is a main rotor helicopter blade for generating higher lift with less drag and delaying stall at high Mach numbers. A cross-section of this blade includes aft camber. The difference between a chord line of the cross-section and a camber line of the cross-section increases from a leading edge of the cross-section to a maximum between a trailing edge of the cross-section and a midpoint of the chord line and decreases to the trailing edge producing the aft camber of the blade. The aft camber generates higher lift with less drag and delays stall at high Mach numbers.

公开(公告)号：EP2302172A1

公开(公告)日：2011-03-30

申请号：EP10188274.4

申请日：2005-11-11

申请人： Board of Trustees of Michigan State University

发明人： Muller, Norbert

IPC分类号： F01D5/34 ,  F04D29/02

CPC分类号： F01D5/34 ,  F04D29/023 ,  F04D29/321 ,  F05D2300/44 ,  F05D2300/603 ,  F05D2300/614 ,  F05D2300/702 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/4932 ,  Y10T29/49321 ,  Y10T29/49332

摘要： The invention is related to a machine having a stator (435) including a member consisting of: (a) electrically conductive wire windings (439), or (b) a magnet (16); and a rotor (15; 413) comprising vanes including stacked layers of at least one elongated fiber (12), the rotor including a member consisting of: (a) electrically conductive wire windings (439), or (b) a magnet (16); the rotor operably rotating adjacent the stator and electromagnetism passing between the rotor and the stator during the rotation.
The invention is also related to a method of making a machine.

摘要翻译： 本发明涉及具有定子（435）的机器，该定子包括由以下部件组成的部件：（a）导电线绕组（439）或（b）磁体（16）; 以及转子（15; 413），其包括包括至少一根细长纤维（12）的堆叠层的叶片，所述转子包括由以下部件组成的部件：（a）导电线绕组（439）或（b）磁体 ）; 转子在转子周围可操作地旋转并且在旋转期间在转子和定子之间通过电磁体。 本发明还涉及制造机器的方法。

公开(公告)号：EP2302171A1

公开(公告)日：2011-03-30

申请号：EP10188273.6

申请日：2005-11-11

申请人： Board of Trustees of Michigan State University

发明人： Muller, Norbert

IPC分类号： F01D5/34 ,  F04D29/02

CPC分类号： F01D5/34 ,  F04D29/023 ,  F04D29/321 ,  F05D2300/44 ,  F05D2300/603 ,  F05D2300/614 ,  F05D2300/702 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/4932 ,  Y10T29/49321 ,  Y10T29/49332

摘要： The invention is related to a turbomachine having a first impeller (403) and at least a second impeller (405) rotating about a common axis, each of the impellers comprising multiple blades including at least one continuous fiber having a stacked arrangement on the blades.
The invention is also related to a method for using rotors, the method comprising: rotating a first woven rotor (403) about an axis (419), the first woven rotor including multiple vanes made from an elongated fiber ; and rotating at least a second woven rotor (405) about the same axis, the second woven rotor including multiple vanes made from another elongated fiber.

摘要翻译： 本发明涉及具有第一叶轮（403）和绕共同轴线旋转的至少第二叶轮（405）的涡轮机，每个叶轮包括多个叶片，其包括在叶片上具有堆叠布置的至少一个连续纤维。 本发明还涉及一种使用转子的方法，所述方法包括：围绕轴线（419）旋转第一编织转子（403），所述第一编织转子包括由细长纤维制成的多个叶片; 以及围绕相同的轴线旋转至少第二编织转子（405），所述第二织造转子包括由另一细长纤维制成的多个叶片。

公开(公告)号：EP2239459A2

公开(公告)日：2010-10-13

申请号：EP10158285.6

申请日：2010-03-30

申请人： Vestas Wind Systems A/S

发明人： Jørgensen, Henning ,  Hansen, Jens Jessen

IPC分类号： F03D1/00

CPC分类号： F03D13/40 ,  Y02E10/72 ,  Y10T29/49332

摘要： The present invention relates to a transport system for transporting at least one blade or spar for a wind turbine. The blade or spar has a root end and a tip end. The transport system comprises a root frame structure for holding the root end and a fixation device adapted to fixate and support the blade or spar between the root end and tip end.

公开(公告)号：EP2149711A2

公开(公告)日：2010-02-03

申请号：EP09166516.6

申请日：2009-07-27

申请人： General Electric Company

发明人： Kray, Nicholas Joseph ,  Davis, Tod ,  Mcafee, Christopher Lee ,  Franks, Michael John ,  Kirkeng, Kevin Lee ,  Crall, David

IPC分类号： F04D29/02 ,  F04D29/32

CPC分类号： F04D29/324 ,  F01D5/282 ,  F04D29/023 ,  F04D29/388 ,  F05D2300/6034 ,  Y10T29/49332 ,  Y10T29/49337 ,  Y10T156/17 ,  Y10T428/24132

摘要： A system for manufacturing a blade (200) is provided. The system includes a mold (304), a plurality of first plies, each of the first plies sized to extend substantially the length of a span of the blade, a plurality of second plies, each of the second plies sized to extend only partially the length of the span of the blade, the plurality of first plies layered with the plurality of second plies in the mold such that the plurality of second plies is interspersed throughout the plurality of first plies to spread apart the plurality of first plies to facilitate increasing a cross-sectional area of the blade.

摘要翻译： 提供一种用于制造叶片（200）的系统。 该系统包括模具（304），多个第一层，每个第一层的尺寸设计成基本上延伸叶片的跨度的长度，多个第二层，每个第二层的尺寸设计成仅部分延伸 叶片的跨度的长度，多个第一层与模具中的多个第二层层叠，使得多个第二层散布在整个多个第一层中，以分散多个第一层，以便于增加 叶片的横截面面积。

公开(公告)号：EP1984244A2

公开(公告)日：2008-10-29

申请号：EP06850525.4

申请日：2006-10-17

申请人： Sikorsky Aircraft Corporation

发明人： OWEN, Stephen, J.

IPC分类号： B64C27/08

CPC分类号： B64C27/467 ,  B64C3/14 ,  Y02T50/12 ,  Y10T29/49332

摘要： An airfoil family for a helicopter rotor blade, designated SC362XX. SC362XX essentially removes the large lower surface suction peak associated with 'drag creep' at moderate lift coefficients while reducing the peak Mach number and shock strength at high lift/Mach number conditions. Another optional airfoil family for use at inboard regions of the helicopter rotor, which is designated SC3252XX airfoil family, is a relatively thicker airfoil section that includes a significant increase in thickness forward of the 30% x/c location to provide a relatively thick and rigid inboard section. The lift coefficient at which the drag divergence Mach number was optimized is the same in both families thereby readily providing application to a single rotor blade.