Compressor blade of a gas turbine
Research output: Intellectual Property › Patent application/Patent
Contributors
Abstract
The present invention relates to a compressor blade of a gas turbine having an airfoil and a blade root, said blade root and airfoil being made in one piece from a fiber-composite material, as well as a leading edge protector made from a sheet metal material, characterized in that the airfoil is provided with a radial groove extending substantially over the entire length of the airfoil and that the leading edge protector is detachably clamped onto the airfoil and is fixed with a sheet metal flange in the radial groove of the airfoil.
Details
The present invention relates to a compressor blade of a gas turbine having an airfoil and a blade root, said blade root and airfoil being made in one piece from a fiber-composite material, as well as a leading edge protector made from a sheet metal material, characterized in that the airfoil is provided with a radial groove extending substantially over the entire length of the airfoil and that the leading edge protector is detachably clamped onto the airfoil and is fixed with a sheet metal flange in the radial groove of the airfoil.
| Original language | English |
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| IPC (International Patent Classification) | F01D 5/14 |
| Patent number | US 9,964,117 |
| Filing date | 17 Dec 2015 |
| Country/Territory | Germany |
| Priority date | 19 Dec 2014 |
| Priority number | DE102014226700 |
| Publication status | Published - 8 May 2018 |
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External IDs
| ORCID | /0000-0003-3813-2933/work/142656674 |
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