公开(公告)号：US07134842B2

公开(公告)日：2006-11-14

申请号：US11022121

申请日：2004-12-24

申请人： Anna Tam ,  Ching-Pang Lee ,  Kevin Richard Kirtley ,  Ronald Scott Bunker ,  Scott Henry Lamson ,  Scott Michael Carson

发明人： Anna Tam ,  Ching-Pang Lee ,  Kevin Richard Kirtley ,  Ronald Scott Bunker ,  Scott Henry Lamson ,  Scott Michael Carson

IPC分类号： F01D5/22

CPC分类号： F01D5/145 ,  F01D5/143 ,  F05D2240/80 ,  F05D2250/70 ,  F05D2250/711 ,  F05D2250/712 ,  Y02T50/673

摘要： A turbine stage includes a row of airfoils joined to corresponding platforms to define flow passages therebetween. Each airfoil includes opposite pressure and suction sides and extends in chord between opposite leading and trailing edges. Each platform has a scalloped flow surface including a bulge adjoining the pressure side adjacent the leading edge, and a bowl adjoining the suction side aft of the leading edge.

摘要翻译： 涡轮级包括连接到相应平台的一排翼型件，以限定它们之间的流动通道。 每个翼型件包括相对的压力和吸力侧面，并且在相对的前缘和后缘之间延伸成弦。 每个平台具有扇形流动表面，包括邻近前缘的压力侧的凸起，以及与前缘的后侧的吸入侧邻接的碗。

公开(公告)号：US07249928B2

公开(公告)日：2007-07-31

申请号：US10907476

申请日：2005-04-01

申请人： Kevin Samuel Klasing ,  Scott Michael Carson

发明人： Kevin Samuel Klasing ,  Scott Michael Carson

IPC分类号： F01D25/12

CPC分类号： F01D5/145 ,  F01D5/143 ,  F01D9/041 ,  F01D11/001 ,  Y02T50/672 ,  Y02T50/673

摘要： A turbine nozzle for a gas turbine engine includes a nozzle segment having an airfoil-shaped vane with a root, a tip, a leading edge, a trailing edge and opposed curved pressure and suction sides. An arcuate inner band segment is attached to the root of the vane. The inner band segment includes an inner flowpath surface bounded at forward and aft ends thereof by a forward-facing surface and an aft-facing surface, respectively. A convex curved blended corner is formed between the inner flowpath surface and the aft-facing surface.

摘要翻译： 用于燃气涡轮发动机的涡轮喷嘴包括具有叶形翼片的喷嘴段，其具有根部，尖端，前缘，后缘和相对的弯曲压力和吸力侧。 弧形内带段连接到叶片的根部。 内带段包括在其前端和后端分别由前向表面和后向表面限定的内部流路表面。 内侧流路面与后方面之间形成有凸曲面的混合角。