公开(公告)号：US20060138150A1

公开(公告)日：2006-06-29

申请号：US10545329

申请日：2004-02-07

申请人： Dirk Buechler ,  Gerhard Buttkewitz ,  Georg Harzfeld

发明人： Dirk Buechler ,  Gerhard Buttkewitz ,  Georg Harzfeld

IPC分类号： F17C1/00

CPC分类号： F17C1/06 ,  F17C1/08 ,  F17C2201/0119 ,  F17C2201/0147 ,  F17C2201/054 ,  F17C2201/056 ,  F17C2203/012 ,  F17C2203/013 ,  F17C2203/0604 ,  F17C2203/0619 ,  F17C2203/0665 ,  F17C2203/0668 ,  F17C2203/067 ,  F17C2203/0673 ,  F17C2209/2154 ,  F17C2223/0123 ,  F17C2223/035 ,  F17C2260/011 ,  F17C2260/013

摘要： The invention can be used for the pressurized storage of gases. The aim of the invention is to provide a pressurized container consisting of fibre-reinforced plastic with flat or practically flat lids. To achieve this, wound axially aligned reinforcement structures run through the interior of the body and absorb the major part of the required forces on their plane of alignment. The invention is characterized in that fibre strands are distributed uniformly over the cross-sectional surface of the cylindrical pressurized container, are aligned axially and fixed to flat or practically flat lids. In one advantageous embodiment of the invention, a container is formed by the spiral winding of an essentially unidirectional fibre-layer, which is thicker at its edges. Reinforcement layers, which are arranged in a circumferential direction and exert a radial action, cover the reinforcement strands or the spirally wound unidirectional fibre-layer, said layers forming the casing of the pressurized container.

摘要翻译： 本发明可用于气体的加压储存。 本发明的目的是提供一种由具有扁平或几乎平坦的盖的纤维增强塑料组成的加压容器。 为了实现这一点，缠绕轴向对齐的加强结构穿过主体的内部并吸收其对准平面上所需力的主要部分。 本发明的特征在于，纤维束均匀分布在圆柱形加压容器的横截面上，轴向对齐并固定在平坦或实际上平坦的盖子上。 在本发明的一个有利的实施例中，容器由基本上单向纤维层的螺旋绕组形成，其在其边缘处较厚。 沿圆周方向布置并施加径向作用的增强层覆盖加强股或螺旋卷绕的单向纤维层，所述层形成加压容器的壳体。

公开(公告)号：US20130192231A1

公开(公告)日：2013-08-01

申请号：US13879189

申请日：2011-10-04

申请人： Dirk Buchler ,  Gerhard Buttkewitz

发明人： Dirk Buchler ,  Gerhard Buttkewitz

IPC分类号： F01D1/04

CPC分类号： F01D1/04 ,  F01D1/24 ,  F01D15/10 ,  F02C3/04 ,  F02C3/067 ,  F02C3/08 ,  F02C3/09 ,  F02C3/14 ,  F02C3/16 ,  F02C3/165

摘要： The invention relates to a turbine wheel arrangement for a gas turbine comprising two successive turbine wheels (18, 20) rotating in opposite directions, wherein the first turbine wheel (18) comprises flow channels (42) of a Laval cross-sectional shape, distributed over the circumference and having radially inner gas inlets (43) and radially further out gas outlets (45), in each case with a substantially tangential flow direction component, wherein the gas outlets (45) act an the second axially or radially acting turbine wheel (20) in the direction of flow. This has the effect that the thermal energy and compressive energy of the gas at the nozzle inlet is largely converted into flow energy at the outlet of the turbine stage. The rotational speeds of the two rotors coupled to the turbine wheels can be set as desired, allowing the operational states of the two systems to be optimally set without adjusting systems.

摘要翻译： 本发明涉及一种用于燃气轮机的涡轮机叶轮装置，其包括沿相反方向旋转的两个相继的涡轮机叶轮（18,20），其中第一涡轮机叶轮（18）包括拉瓦尔截面形状的流动通道（42） 在圆周上并且具有径向内部气体入口（43）和径向进一步排出气体出口（45），在每种情况下具有基本切向的流动方向分量，其中气体出口（45）作用于第二轴向或径向作用的涡轮机叶轮 （20）沿流动方向。 这具有以下效果：喷嘴入口处的气体的热能和压缩能量在涡轮级的出口处被大部分转化为流动能。 耦合到涡轮机叶轮的两个转子的转速可以根据需要设定，从而允许在不调整系统的情况下最佳地设定两个系统的操作状态。