公开(公告)号：US4201512A

公开(公告)日：1980-05-06

申请号：US826977

申请日：1977-08-23

申请人： Chester W. Marynowski ,  F. Michael Lewis ,  Charles E. Lapple ,  Robert G. Murray ,  Konrad T. Semrau

发明人： Chester W. Marynowski ,  F. Michael Lewis ,  Charles E. Lapple ,  Robert G. Murray ,  Konrad T. Semrau

IPC分类号： F01D1/08 ,  F01D1/36

CPC分类号： F01D1/36

摘要： The staging or compounding of drag-type turbines having a high energy input is herein accomplished by disposing successive stages of a drag turbine in radially offset relation, i.e., nested relationship with nozzles between radially displaced stages mounted either in fixed spatial position or mounted for rotation with the upstream rotor and providing either like or opposite directions of rotation of successive stages. The successive radial stages of the present invention are separately coupled to coaxial drive shafts which, in turn, may be appropriately coupled to rotary output means in a conventional manner to provide the output power and high efficiency of the multistaged turbine.

摘要翻译： 具有高能量输入的拖曳式涡轮机的分级或复合在此通过将拖拉式涡轮机的连续级设置为径向偏移关系来实现，即，在安装在固定的空间位置或安装成旋转的径向位移的台阶之间与喷嘴的嵌套关系 与上游转子并提供连续级的相同或相反的旋转方向。 本发明的连续的径向级分别联接到同轴驱动轴上，同轴驱动轴又可以以常规方式适当地耦合到旋转输出装置，以提供多级涡轮机的输出功率和高效率。