发明申请
US20120301312A1 CERAMIC MATRIX COMPOSITE AIRFOIL STRUCTURES FOR A GAS TURBINE ENGINE
有权
用于气体涡轮发动机的陶瓷基体复合材料空气结构
- 专利标题: CERAMIC MATRIX COMPOSITE AIRFOIL STRUCTURES FOR A GAS TURBINE ENGINE
- 专利标题(中): 用于气体涡轮发动机的陶瓷基体复合材料空气结构
-
申请号: US13116093申请日: 2011-05-26
-
公开(公告)号: US20120301312A1公开(公告)日: 2012-11-29
- 发明人: Douglas M. Berczik , Gabriel L. Suciu , Brian D. Merry , Alvanos Ioannis , Christopher M. Dye
- 申请人: Douglas M. Berczik , Gabriel L. Suciu , Brian D. Merry , Alvanos Ioannis , Christopher M. Dye
- 主分类号: F01D5/14
- IPC分类号: F01D5/14 ; B21K25/00
摘要:
A Ceramic Matrix Composite (CMC) airfoil segment for a gas turbine engine includes a box-shape fiber geometry which defines a rectilinear pressure side bond line and a rectilinear suction side bond line.