发明名称 |
GAS TURBINE ENGINE AIR SEPARATOR |
摘要 |
PROBLEM TO BE SOLVED: To improve an air separator to more appropriately contact the air separator with turbine first-sequence discs in a gas turbine.SOLUTION: An air separator includes: a cylindrical member 22; and a seal flange 28 including a flange body 36 extending radially in a rear end portion of the cylindrical member 22. A head section 42 includes an axial flange arranged in a radially outward free end portion 66 of the flange body 28, arranged axially backward of the flange body 36, and defining a rear seal surface 60 for engagement with a front surface of a blade disc; and a front cantilever head bulk portion 64 extending axially forward from the flange body 36. An axial distance dof the head bulk portion 64 from a connected portion of the head bulk portion 64 connected to a front side of the flange body 36 to an axial front surface of the head bulk portion 64 is larger than a maximum radial dimension dof the head bulk portion 64 from a radially inward side to a radially outermost side of the bulk portion 64. |
申请公布号 |
JP2015098870(A) |
申请公布日期 |
2015.05.28 |
申请号 |
JP20140233655 |
申请日期 |
2014.11.18 |
申请人 |
SIEMENS ENERGY INC |
发明人 |
MAHESH JANARTHANAN;DIEGO L CASO JR;RYAN J MAJKUT |
分类号 |
F02C7/18;F01D25/00;F01D25/12;F01D25/24;F02C7/00;F02C7/28 |
主分类号 |
F02C7/18 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|