-
1.发明授权AXIALTURBINE FÜR EINE GASTURBINE MIT GERINGEM SPIEL ZWISCHEN SCHAUFELN UND GEHÄUSE 有权轴流涡轮机具有叶片与壳体之间的小游的燃气涡轮机
公开(公告)号：EP2297430B1
公开(公告)日：2013-08-28
申请号：EP09797468.7
申请日：2009-07-08
-
2.发明公开AXIALTURBINE FÜR EINE GASTURBINE MIT GERINGEM SPIEL ZWISCHEN SCHAUFELN UN GEHÄUSE 有权轴流涡轮机具有叶片与壳体之间的小游的燃气涡轮机
公开(公告)号：EP2297430A1
公开(公告)日：2011-03-23
申请号：EP09797468.7
申请日：2009-07-08
发明人： BRAUN, Stefan , CORNELIUS, Christian , HEILOS, Andreas , HEIN, Olaf , HOFBAUER, Thomas , EMDE, Annika , LERNER, Christian , MARTIN, Silvio-Ulrich , MATTHEIS, Thorsten , MÜSGEN, Ralf , SCHUMANN, Eckart , TETERUK, Rostislav , ZIMMERMANN, Adam
摘要： The invention relates to an axial turbine (1) for a gas turbine comprising a rotor blade cascade that is formed from rotor blades (2) having, respectively, a front edge (3) and a radially outer, free-standing (13) blade tip, and an annular space wall (11) that surrounds the rotor blade cascade and that has an annular space inner side (12), enabling the annular space wall to be arranged directly adjacent to the blade tip forming a radial gap between the covering of the blade tip and the annular space inner side. The invention is characterised in that the blade tips are designed aerodynamically such that when the axial turbine is in operation, the area of the blade tip with the highest pressure load is disposed in the region of the front edges, and the rotor blades in the region of their front edges have a radial elevation (16) and the annular space wall comprises, on the annular space inner side, a peripheral radial recess (15) that interacts with the radial elevations such that a gap width minimum is established in the direction of the main through flow of the axial turbine when seen in the region of the front edge.
-
搜索结果
2 条记录 (耗时 0.008 秒)
