公开(公告)号：US06786695B2

公开(公告)日：2004-09-07

申请号：US10293333

申请日：2002-11-14

Applicant: Andrew John Tomko ,  Brian Patrick Marks

Inventor： Andrew John Tomko ,  Brian Patrick Marks

IPC: F01D1100

CPC classification number: F01D5/147 ,  F05D2230/13 ,  F05D2230/23

Abstract: To accurately axially position and/or seal between axially facing turbine parts, a groove having a cylindrical cross-section is formed in one surface with a centerline offset toward the one surface, the groove opening through the one surface. Rod segments having corresponding cylindrical cross-sections are inserted in the groove. The rod segments have flat surfaces coextensive therewith projecting a predetermined measured distance from the one surface, thereby accurately axially locating the turbine parts relative to one another and forming a seal therebetween. The rod segments have ends abutting one another to seal the segments one to the other.

Abstract translation: 为了准确地轴向地定位和/或密封在轴向面对的涡轮机部件之间，具有圆柱形横截面的凹槽形成在一个表面中，该中心线朝向一个表面偏移，该凹槽通过该一个表面开口。 具有相应圆柱形横截面的杆段插入槽中。 杆段具有共同延伸的平坦表面，其从一个表面突出预定的测量距离，从而相对于彼此精确地轴向定位涡轮机部件并在其间形成密封。 杆段具有彼此邻接的端部，以将片段彼此密封。