초록 ▼

Tenons can be installed at the ends of turbine blades by applying a solid state bonding procedure such as a friction welding technique to join the tenons to the turbine blades. The tenons can be employed to assemble the turbine blades to one or more covers for the turbine blades. The tenons can be i

Tenons can be installed at the ends of turbine blades by applying a solid state bonding procedure such as a friction welding technique to join the tenons to the turbine blades. The tenons can be employed to assemble the turbine blades to one or more covers for the turbine blades. The tenons can be installed in connection with the restoration of tenons for turbine buckets in steam turbines and in connection with the renovation of rotor assemblies that include turbine blades secured to a common disk, tenons located at one end of respective turbine blades and one or more covers secured to the turbine blades by means of the tenons. In instances in which tenon remnants are present at the ends of the turbine blades, tenon enlargement elements can be joined to the tenon remnants by the solid state bonding procedure. The tenon installations can be carried out in situ.

대표청구항 ▼

1. A method of installing at least one respective tenon at each of one or more turbine blades including: providing one or more turbine blades at which at least one respective tenon is to be installed, each turbine blade including a first end that is configured to be secured to a turbine disk and a s

1. A method of installing at least one respective tenon at each of one or more turbine blades including: providing one or more turbine blades at which at least one respective tenon is to be installed, each turbine blade including a first end that is configured to be secured to a turbine disk and a second end that is located substantially opposite the first end of the turbine blade;orienting the second end of each turbine blade at which at least one respective tenon is to be installed in an attitude that is accommodative to the installation of the at least one respective tenon at the second end of each turbine blade; andinstalling the at least one respective tenon at the second end of each turbine blade at which the at least one respective tenon is to be installed by applying a solid state bonding procedure to join the at least one respective tenon to the second end of each turbine blade;wherein the second end of each turbine blade at which the at least one respective tenon is to be installed includes at least one tenon remnant identified for restoration and the step of installing the at least one respective tenon at the second end of each turbine blade at which the at least one respective tenon is to be installed by applying a solid state bonding procedure to join the at least one respective tenon to the second end of the turbine blade includes bonding a respective tenon enlargement element to each of the at least one tenon remnants identified for restoration. 2. The method of claim 1 wherein the solid state bonding procedure includes a friction welding technique. 3. The method of claim 1 wherein the solid state bonding procedure includes a friction welding technique. 4. The method of claim 1 wherein the method is performed in situ. 5. A method of assembling a plurality of turbine blades and one or more covers for the turbine blades by means of tenons installed at the turbine blades through openings in the one or more covers including: providing a plurality of turbine blades at which at least one respective tenon is to be installed, each turbine blade including a first end that is configured to be secured to a common turbine disk and a second end that is located substantially opposite the first end of the turbine blade;orienting the plurality of turbine blades at which at least one respective tenon is to be installed in an attitude that is accommodative to the installation of at least one respective tenon at the second end of each of the plurality of turbine blades;providing one or more covers for installation at the second ends of the plurality of turbine blades at which at least one respective tenon is to be installed, the one or more covers including openings of a size and located to allow respective tenons to be installed through the openings and bonded to respective second ends of the plurality of turbine blades when the one or more covers are placed at the second ends of the plurality of turbine blades;placing the one or more covers at the second ends of the plurality of turbine blades at which at least one respective tenon is to be installed so that the openings in the one or more covers are positioned at each of the respective second ends of the plurality of turbine blades; andinstalling at least one respective tenon at the second end of each of the plurality of turbine blades at which at least one respective tenon is to be installed through a respective opening in the one or more covers by applying a solid state bonding procedure to join each respective tenon to the second end of a respective one of the plurality of turbine blades. 6. The method of claim 5 wherein the solid state joining procedure includes a friction welding technique. 7. The method of claim 5 wherein at least one of the plurality of turbine blades at which at least one respective tenon is to be installed includes at the second end thereof at least one tenon remnant identified for restoration, and the step of installing at least one respective tenon at the second end of each of the plurality of turbine blades at which at least one respective tenon is to be installed through a respective opening in the one or more covers by applying a solid state bonding procedure to join each tenon to the second end of a respective one of the plurality of turbine blades includes bonding a respective tenon enlargement element to each of the at least one tenon remnant identified for restoration. 8. The method of claim 7 wherein the solid state bonding procedure includes a friction welding technique. 9. The method of claim 5 wherein the method is performed in situ.