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A turbine blade having a root and a tip and an airfoil with a core section made of composite material and a protective sheath or layer joined to the composite core at a location or locations exposed to erosion is described with the composite core of the airfoil being continuous from a location in vi

A turbine blade having a root and a tip and an airfoil with a core section made of composite material and a protective sheath or layer joined to the composite core at a location or locations exposed to erosion is described with the composite core of the airfoil being continuous from a location in vicinity of the root to a location in vicinity of the tip of the blade and including a section which widens with distance from the rotational axis along the length of the airfoil and which ends at the location in vicinity of the tip of the blade. The protective sheath or layer is secured by interference fit with widening section of the core.

대표청구항 ▼

1. A turbine blade, comprising: a root;a tip;an airfoil extending therebetween with a core section made of composite material;a protective sheath including a leading edge cover, a suction side cover, a trailing edge cover and a pressure side cover, the leading edge cover and the trailing edge cover

1. A turbine blade, comprising: a root;a tip;an airfoil extending therebetween with a core section made of composite material;a protective sheath including a leading edge cover, a suction side cover, a trailing edge cover and a pressure side cover, the leading edge cover and the trailing edge cover each having recesses;an adhesive layer between the protective sheath and the core section;wherein the protective sheath is joined to the core section at least in an area of the airfoil exposed to erosion, the core section of the airfoil is continuous from a location in a vicinity of the root to a location in a vicinity of the tip of the blade and comprises a section which widens from the rotational axis along the length of the airfoil and which ends at the location in the vicinity of the tip of the blade;welding seams arranged in the respective recesses of the leading edge cover and the trailing edge cover and offset from the adhesive layer for avoiding thermal damage to the adhesive layer during a welding process; andan interference fit provided for the protective sheath by the widening section of the core section configured for preventing movement of the protective sheath along the core section in a radially outward direction. 2. The turbine blade of claim 1 wherein the widening is continuous or step-wise. 3. The turbine blade of claim 1 wherein the widening includes a lengthening of the airfoil's chord length towards the tip. 4. The turbine blade of claim 3 wherein the airfoil has a section where the chord length decreases as a function of the radial distance followed by a section where the chord length increases as a function of the radial distance. 5. The turbine blade of claim 3 wherein chord length increases continuously as a function of the radial distance from the location in vicinity of the root to the location in vicinity of the tip of the blade. 6. The turbine blade of claim 1 being a blade for a steam turbine. 7. The turbine blade of claim 1 being a last stage blade for a steam turbine. 8. A method of manufacturing a blade for a steam turbine comprising: providing a core of composite material continuously extending from a location in a vicinity of a root section of the blade to a location in a vicinity of a tip section of the blade;surrounding the core with a protective sheath of a different material, the protective sheath including a leading edge cover, a suction side cover, a trailing edge cover and a pressure side cover, the leading edge cover and the trailing edge cover each having recesses;increasing the width of the core of composite material at least at the vicinity of the tip end of the blade;providing an adhesive layer between the protective sheath and the core;providing welding seams in the respective recesses of the leading edge cover and the trailing edge cover offset from the adhesive layer for avoiding thermal damage to the adhesive layer during a welding process; andproviding an interference fit for the protective sheath by the widening section of the composite core configured for preventing movement of the protective sheath along the core in a radially outward direction.