子分类：
| 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 | 控制壳体模块和制造方法 | CN201280041197.2 | 2012-07-17 | CN103764984A | 2014-04-30 | E·里斯; G·佐尔 |
| 本发明提供了一种用于内燃机的控制壳体模块（1），包含用于附件设备（2、3、4、5、6、7、8）的容纳结构和/或连接结构和/或集成结构以及筋结构，其中控制壳体模块（1）由纤维-塑料复合材料构成，所述纤维-塑料复合材料具有至少一个嵌入物（10），所述嵌入物由热塑性塑料基体中的平的纤维织物构成，其中筋结构由注塑形成的热塑性塑料加强筋（11、11a）构成，所述热塑性塑料包含体积含量最低为30%的、由加强材料构成的短纤维，其中，加强部（11、11a）包含符合受力分布的筋结构（11a）以及规则成型的、相交的纵向加强筋、横向加强筋和/或斜向加强筋（11），且在由筋（11、11a）界定出的筋间隔空间（13）中设置泡沫材料。 | ||||||
| 2 | 风力涡轮机 | CN201080021661.2 | 2010-04-19 | CN102428267A | 2012-04-25 | 杰拉尔德·L·巴伯 |
| 一种风力涡轮机(20)，其包括涡轮机叶轮(22)。径向延伸的帆翼组件(30)支撑在涡轮机叶轮的轮轴结构(28)和周界轨道(26)之间。所述帆翼组件包括帆端部支撑件(52、53)；帆支撑缆线(54、55)，所述帆支撑缆线(54、55)在所述帆端部支撑件之间延伸；以及帆翼(58)，其被所述帆支撑缆线支撑并且在所述涡轮机叶轮的轮轴结构(28)和周界轨道(26)之间延伸。所述帆端部支撑件(52、53)可以枢转以在所述帆翼(58)中形成节距并且彼此相对枢转以在所述帆翼中形成扭转，并且帆展开器杆(70)可以安装在帆翼中并且连接到所述帆支撑缆线(54、55)以调整帆翼的有效宽度和跃层。 | ||||||
| 3 | 用于往复式变容压缩机的环形吸入阀和装备有这种阀的压缩机 | CN01143700.6 | 2001-12-19 | CN1364982A | 2002-08-21 | 莫科·卡路曼尼 |
| 在带有一个或者多个环形或者圆环状阀的往复式变容压缩机中,尤其是用于致冷设备的压缩机中,至少一个弹簧偏压的环形阀由这样的一张薄板(64)制成,即该薄板(64)包括有若干层由浸渍有树脂基质(66)的碳纤维形成的织物层,并且还可能包括有位于其表面边缘处的一个或者多个纤维玻璃和/或陶瓷和/或芳族聚酰胺纤维层。根据需要,可以替代性地用相同方式构造一个排放阀,或者同时以相同的方式构造一个排放阀。 | ||||||
| 4 | 控制壳体模块和制造方法 | CN201280041197.2 | 2012-07-17 | CN103764984B | 2016-06-29 | E·里斯; G·佐尔 |
| 本发明提供了一种用于内燃机的控制壳体模块（1），包含用于附件设备（2、3、4、5、6、7、8）的容纳结构和/或连接结构和/或集成结构以及筋结构，其中控制壳体模块（1）由纤维-塑料复合材料构成，所述纤维-塑料复合材料具有至少一个嵌入物（10），所述嵌入物由热塑性塑料基体中的平的纤维织物构成，其中筋结构由注塑形成的热塑性塑料加强筋（11、11a）构成，所述热塑性塑料包含体积含量最低为30%的、由加强材料构成的短纤维，其中，加强部（11、11a）包含符合受力分布的筋结构（11a）以及规则成型的、相交的纵向加强筋、横向加强筋和/或斜向加强筋（11），且在由筋（11、11a）界定出的筋间隔空间（13）中设置泡沫材料。 | ||||||
| 5 | 风力涡轮机 | CN201080021661.2 | 2010-04-19 | CN102428267B | 2014-06-25 | 杰拉尔德·L·巴伯 |
| 一种风力涡轮机(20)，其包括涡轮机叶轮(22)。径向延伸的帆翼组件(30)支撑在涡轮机叶轮的轮轴结构(28)和周界轨道(26)之间。所述帆翼组件包括帆端部支撑件(52、53)；帆支撑缆线(54、55)，所述帆支撑缆线(54、55)在所述帆端部支撑件之间延伸；以及帆翼(58)，其被所述帆支撑缆线支撑并且在所述涡轮机叶轮的轮轴结构(28)和周界轨道(26)之间延伸。所述帆端部支撑件(52、53)可以枢转以在所述帆翼(58)中形成节距并且彼此相对枢转以在所述帆翼中形成扭转，并且帆展开器杆(70)可以安装在帆翼中并且连接到所述帆支撑缆线(54、55)以调整帆翼的有效宽度和跃层。 | ||||||
| 6 | 垂直轴风轮机 | CN201080011206.4 | 2010-03-09 | CN102348890A | 2012-02-08 | 罗伯特·佛拉瑟·莫里斯 |
| 一种轮机头，包括：一可转动件；多个层叠桨叶，每个桨叶都包括一表面，桨叶可旋转地安装于可转动件上，以使得每个桨叶都能够相对可转动件从一第一位置转动至一第二位置，该第一位置与该第二位置间的夹角小于180度；其中，每个桨叶都围绕一轴可旋转地安装于可转动件上，该轴位于这样的靠近桨叶的中心的位置，即如果一力从垂直于该表面的方向施加于轮叶上，则施加于该轴的一侧的该表面的部分上的力与施加于该轴的另一侧的该表面的部分上的力之差足以驱动桨叶从该第一位置旋转至该第二位置。 | ||||||
| 7 | Vertical shaft type wind mill used with sail wing | JP11409181 | 1981-07-21 | JPS5815766A | 1983-01-29 | MURAI HITOSHI |
| PURPOSE:To obtain a wind mill with high efficiency of energy conversion, by protrusively providing plural L-shaped arms radially from upper and lower parts of a vertical shaft, connecting a wing spar shaft to folded parts of the arms, extensibly providing a tension wire to ends of the L-shaped arms, spreading a flexible film between the wing spar shaft and the tension wire, surrounding the wing spar shaft and a pat of the flexible film and forming flexible profile spars. CONSTITUTION:Plural L-shaped arms 3 are protrusively provided radially from upper and lower bosses 2 of a vertical shaft 1, and a wing spar shaft 4 is rotatably mounted between folded parts 3a, and a tension wire 7 of steel wire and the like is extensibly provided between external ends of folded parts 36 through springs 8, while a flexible film 5 of cloth or the like is spread between the tension wire 7 and the wing spar shaft 4, further profile spars 6 consisting of flexible material like rubber and the like, are formed by surrounding the periphery of the wing spar shaft 4 and a part of the flexible film 5. Since the profile spar 6 and the flexible film 5 are suitably curved and deformed in accordance with the direction or velocity of a wind, a vertical shaft type wind mill of good energy efficiency can be obtained by simple construction. | ||||||
| 8 | Vertical shaft type wind mill employing sail wing | JP10102081 | 1981-06-29 | JPS582475A | 1983-01-08 | MURAI HITOSHI |
| PURPOSE:To improve the energy conversion efficiency of the wind mill by applying the sail wing to the vertical shaft type wind mill. CONSTITUTION:When feeding the wind to the vertical shaft type wind mill, the front edge board 5 supported rotatably against L-shaped arm 3 will rotate in accordance to the direction of the wind thereby the sail wing will change the angle automatically to maintain the proper direction against the combined speed of the wind and the wind mill. Furthermore the angle of attack of the sail wing will be varied automatically by the flexure of the stretched wire at the rear edge section of the wing or the expansion of the spring 8 fixed to it, thereby the flexible film 6 will flex to form the wing shape suitable for the flow. Consequently, the sail wing will rotate efficiently around the vertical axis 1. | ||||||
| 9 | Centrifugal impeller and turbomachinery | JP2012541139 | 2010-11-22 | JP2013527358A | 2013-06-27 | ガイノッチ，マッシモ; ジョヴァネッティ，イアコポ; マッシーニ，アンドレア; アクセル，ビューレント; ラナウド，クリストフ; オフリン，ジュリアン; フィン，スコット |
| 各々が、ファブリック要素（１Ａ、１Ｂ、１Ｃ、４、５、６、７、３７）が関連づけられる内壁を有する、複数の空気力学的ベーン（１３）を備えることを特徴とする、ターボ機械用の遠心羽根車。
【選択図】図１Ａ |
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| 10 | Energy converter, flag-type energy conversion device | JP2006543042 | 2005-10-19 | JP4590641B2 | 2010-12-01 | 宏允 河井 |
| 11 | Automatically adjusting sail wing | JP10101981 | 1981-06-29 | JPS582474A | 1983-01-08 | MURAI HITOSHI |
| PURPOSE:To provide the sufficient strength and the rigidity and to improve the hydrodynamic performance by employing the automatically adjustable sail wing. CONSTITUTION:Upon the application of the hydrodynamic force the wing board at the front edge section will rotate around the wing beam shaft 2 thus to change the direction automatically in accordance to the change of the speed or the direction of the flow. In other word when the angle of attack of the flow against the sail wing will vary by same degree in + or - direction the shape of the wing board 3 is made symmetrical up and down, while when the flow is in one direction and only the angle of attack will vary the wing board is made asymmetrical up and down. Consequently in any case the excellent hydrodynamic performance can be exhibited in the full range in accordance to the varying range of the angle of attack. | ||||||
| 12 | CENTRIFUGAL IMPELLER AND TURBOMACHINE | EP10787952.0 | 2010-11-22 | EP2504581B1 | 2016-06-22 | GAINNOZZI, Massimo; GIOVANNETTI, Iacopo; MASSINI, Andrea; AKSEL, Bulent; LANAUD, Christophe; O'FLYNN, Julian; FINN, Scott |
| A centrifugal impeller for a turbomachine is provided. The centrifugal impeller comprises a plurality of aerodynamic vanes, each of the aerodynamic vanes having internal walls on which is associated a fabric element. | ||||||
| 13 | Kraftfahrzeugkühlwasserschlauch | EP94116381.8 | 1994-10-18 | EP0652396B1 | 1997-06-11 | Keuper, Dieter, Dr.; Mroz, Michael |
| 14 | Gekapselte Windkraftmaschine mit aussermittiger Rotorachse und definierter Windführung | EP93250326.1 | 1993-11-25 | EP0599441B1 | 1996-08-28 | MRASEK, Wilhelm |
| 15 | Vertical axis wind turbine | JP2011553431 | 2010-03-09 | JP2012519802A | 2012-08-30 | モリス・ロバート・フレイザー |
| 【課題】簡単な構造でありながら効率的である垂直軸風力タービンを提供する。
【解決手段】回転部材（１２）と、表面を有する複数の薄板状のブレード（１８，２０，２２，２４）とを備えるタービンヘッドにおいて、各ブレードが回転部材に対して第１の位置から第２の位置まで回転できるように、ブレードが回転部材に回転可能に取り付けられており、前記第１および第２の位置の間の角度は１８０度未満であり、各ブレードが、ブレードの中心に近い軸を中心にして回転部材へと回転可能に取り付けられており、力がブレードの前記表面に垂直な方向に加えられる場合に、前記表面のうちの前記軸の一方の側に位置する部分に加わる力と前記表面のうちの前記軸心に対して他方の側に延びる部分に加わる力との間の差が、前記第１の位置から前記第２の位置に向かうブレードの回転を生じさせる。 【選択図】図２ |
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| 16 | エネルギ変換器、旗型エネルギ変換装置 | JP2006543042 | 2005-10-19 | JPWO2006043600A1 | 2008-05-22 | 宏允 河井 |
| 風等の流体の流れにさらされる位置に配されるとともに前記流れによって周縁部の少なくとも一部がほぼ自由にはためき得る可撓性平面体1と、振動エネルギを電気エネルギに変換するエネルギ変換部31と、前記可撓性平面体1に連結されるとともに前記流れにより可撓性平面体1に生じる振動を前記エネルギ変換部に伝達する伝達部2とを具備するようにした。 | ||||||
| 17 | Automatically adjusted sail wing | JP11409081 | 1981-07-21 | JPS5815765A | 1983-01-29 | MURAI HITOSHI |
| PURPOSE:To efficiently adjust a wing correspondingly to a change of wind direction and wind velocity, by constituting the captioned said wing from a wing spar shaft, connecting leading edge parts of ribs provided to both ends of the wing, tension wires, extensibly provided between rear end parts of the ribs, and flexible films, extensibly spread between the wing spar shaft and the tension wires. CONSTITUTION:Wing end ribs 1, consisting of a plate member in length almost equal to the wing spar, are arranged to both end positions of a wing, and a wing spar shaft 2, extended through leading edge parts of the ribs, is rotatably provided, while tension wires 3 of a steel wire and the like are extensibly provided between rear end parts 1a of the ribs, and flexible films 4 of cloth, film, etc. are spread between the wing spar shaft 2 and the tension wires 3, further airfoil spars 6 are formed around the wing spar shaft 2 by using a flexible material of rubber or the like. This sail wing can be utilized for wind mills, curved, deformed and automatically changed to adequately sectional shape by the airfoil spar 6 and the flexible film 4 in accordance with the direction or velocity of a wind. | ||||||
| 18 | Windmill generator equipping sail | JP95281 | 1981-01-06 | JPS57119177A | 1982-07-24 | MUNETOU RIYOUJI |
| PURPOSE:To lightly perform electric power generator with small wind power, by preparing a sail with nylon or vinyl and expanding a semi-circular sagging groove in the right side while contracting flatly the groove in the left side. CONSTITUTION:A sail k of this machine is prepared by nylon or vinyl. Along a direction of the wind, a right side sail k fills with a large amount of the wind even without a wind collector by expanding a groove of its semi-circular sag d like a globefish, and a strong turning effect is produced to obtain large torque rotating a shaft rod e, further a left side sail k is flatly contracted like a flatfish and the wind slips to produce very small torque of derotation, then large torque is generated, thus electric power generation can be lightly performed by small wind power. | ||||||
| 19 | WIND TURBINE | EP10767574 | 2010-04-19 | EP2422078A4 | 2014-12-17 | BARBER GERALD L |
| 20 | CENTRIFUGAL IMPELLER AND TURBOMACHINE | EP10787952.0 | 2010-11-22 | EP2504581A1 | 2012-10-03 | GAINNOZZI, Massimo; GIOVANNETTI, Iacopo; MASSINI, Andrea; AKSEL, Bulent; LANAUD, Christophe; O'FLYNN, Julian; FINN, Scott |
| A centrifugal impeller for a turbomachine is provided. The centrifugal impeller comprises a plurality of aerodynamic vanes, each of the aerodynamic vanes having internal walls on which is associated a fabric element. | ||||||
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