发明授权
US08790082B2 Gas turbine blade with intra-span snubber 有权
带跨度缓冲器的燃气轮机叶片

Gas turbine blade with intra-span snubber
摘要:
A gas turbine blade (10) including a hollow mid-span snubber (16). The snubber is affixed to the airfoil portion (14) of the blade by a fastener (20) passing through an opening (24) cast into the surface (22) of the blade. The opening is defined during an investment casting process by a ceramic pedestal (38) which is positioned between a ceramic core (32) and a surrounding ceramic casting shell (48). The pedestal provides mechanical support for the ceramic core during both wax and molten metal injection steps of the investment casting process.
信息查询
0/0