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A rotor wheel assembly includes a rotor wheel having a plurality of dovetail slots spaced circumferentially about a peripheral surface of the rotor wheel. The rotor wheel also has a plurality of notches formed in the peripheral surface. The rotor wheel assembly includes at least one bucket having an

A rotor wheel assembly includes a rotor wheel having a plurality of dovetail slots spaced circumferentially about a peripheral surface of the rotor wheel. The rotor wheel also has a plurality of notches formed in the peripheral surface. The rotor wheel assembly includes at least one bucket having an integral cover, an airfoil, a dovetail, and a platform having a first surface and an opposite second surface. The first surface of the platform includes a keyway. The keyway has an opposing tapered surface oriented at a first angle relative to the first surface of the platform. Furthermore, the rotor wheel assembly includes a wedge key having first face that is oriented substantially parallel to the first surface of the platform and an opposite second face that is oriented at the first angle relative to the first face, such that the second face is substantially parallel to the taper surface.

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1. A rotor wheel assembly comprising: a rotor wheel comprising a plurality of dovetail slots spaced circumferentially about a peripheral surface of said rotor wheel, and a plurality of notches formed in said peripheral surface;a first bucket coupled to said rotor wheel, said first bucket comprising

1. A rotor wheel assembly comprising: a rotor wheel comprising a plurality of dovetail slots spaced circumferentially about a peripheral surface of said rotor wheel, and a plurality of notches formed in said peripheral surface;a first bucket coupled to said rotor wheel, said first bucket comprising an integral cover, an airfoil, a dovetail, and a platform comprising a first circumferential surface and an opposite second circumferential surface, said first circumferential surface comprising a keyway defined therein, said keyway defining a cavity in said first circumferential surface, said keyway comprising a forward surface, a rearward surface, and an opposing circumferential tapered surface oriented at a first angle relative to said platform first circumferential surface;a second bucket coupled to said rotor wheel adjacent said first bucket, said second bucket comprising a platform comprising a third circumferential surface facing said first circumferential surface; anda wedge key comprising a first face oriented substantially parallel to said platform first circumferential surface and an opposite second face oriented at said first angle relative to said first face, said second face is substantially parallel to said circumferential tapered surface, said wedge key disposed in said keyway and positionable between a first position in which said wedge key does not contact said second bucket, and a second position in which said wedge key is in face-to-face contact with said keyway circumferential tapered surface and said second bucket third circumferential surface, wherein said wedge key couples said first bucket to said second bucket, and wherein a frictional contact force is generated between said first bucket and said wedge key, and said second bucket and said wedge key. 2. A rotor wheel assembly in accordance with claim 1, wherein each of said plurality of notches has an axial length that is approximately the same as an axial length of said keyway. 3. A rotor wheel assembly in accordance with claim 1, wherein said rotor wheel has an axis of rotation, said plurality of dovetail slots comprise axial entry dovetail slots, such that each said dovetail slot extends substantially parallel to the axis of rotation. 4. A rotor wheel assembly in accordance with claim 1, wherein said wedge key has an axial width sized to enable said wedge key to slidably engage said keyway. 5. A rotor wheel assembly in accordance with claim 4, wherein said wedge key is configured to simultaneously slidably engage said keyway and one of said plurality of notches. 6. A rotor wheel assembly in accordance with claim 1, wherein a value of said first angle is between about 1° to about 15°. 7. A turbine engine comprising: a rotatable shaft having an axis of rotation;a casing extending circumferentially about said rotatable shaft, said casing defining at least one passage configured to channel a working fluid along a length of said rotatable shaft;a rotor wheel assembly coupled to a portion of said rotatable shaft for rotation therewith, said rotor wheel assembly configured to expand the working fluid, said rotor wheel assembly comprising: a rotor wheel comprising a plurality of dovetail slots spaced circumferentially about a peripheral surface of said rotor wheel, and a plurality of notches formed in said peripheral surface;a plurality of buckets arranged in a circumferential array about said axis of rotation, each respective bucket of said plurality of buckets comprising a dovetail configured to couple to a respective one of said plurality of dovetail slots, an airfoil, an integral cover formed integrally with said respective bucket, and a platform comprising a first circumferential surface and an opposite second circumferential surface, said first circumferential surface comprising a keyway defined therein, said keyway defining a cavity in said first circumferential surface, said keyway comprising a forward surface, a rearward surface, and an opposing tapered circumferential surface oriented at a first angle relative to said platform first circumferential surface; andat least one wedge key comprising a first face oriented substantially parallel to said platform first circumferential surface and an opposite second face oriented at said first angle relative to said first face, said second face is substantially parallel to said tapered circumferential surface, said at least one wedge key disposed between adjacent buckets of said plurality of buckets and in said keyway, said at least one wedge key configured to generate a frictional contact force between said adjacent buckets to couple said adjacent buckets to each other. 8. A turbine engine in accordance with claim 7, wherein said plurality of dovetail slots are oriented at a second angle relative to said axis of rotation. 9. A turbine engine in accordance with claim 8, wherein said plurality of dovetail slots comprise axial entry dovetail slots, such that said second angle is approximately 0°. 10. A turbine engine in accordance with claim 7, wherein said wedge key second face is configured to engage said tapered circumferential surface of a respective one of said plurality of buckets, and a bottom surface of said wedge key is configured to engage a bottom surface of a respective one of said plurality of notches simultaneously, such that an adjacent bucket of said plurality of buckets can couple to an adjacent respective one of said plurality of dovetail slots. 11. A turbine engine in accordance with claim 7, wherein said wedge key second face is configured to engage said tapered circumferential surface of a first bucket of said adjacent buckets, and said wedge key first face is configured to mate against said second circumferential surface of a second bucket of said adjacent buckets. 12. A turbine engine in accordance with claim 11, wherein said first angle is configured to enable a locking taper between said wedge key and a respective one of said plurality of buckets, such that said platform of a respective one of said plurality of buckets is coupled to said platform of an adjacent respective one of said plurality of buckets to facilitate increasing a natural frequency of said respective buckets. 13. A turbine engine in accordance with claim 12, wherein a value of said first angle is between about 1° to about 15°. 14. A turbine engine in accordance with claim 7, wherein said at least one wedge key is configured to simultaneously slidably engage one of said keyways and one of said plurality of notches. 15. A method of assembling a rotor wheel assembly having a plurality of buckets and a rotor wheel having a plurality of dovetail slots spaced circumferentially about a periphery of the rotor wheel, wherein each bucket of the plurality of buckets includes a dovetail, a platform, an airfoil, and an integral cover, said method comprising: coupling a first bucket to the rotor wheel comprising inserting the dovetail of the first bucket into a first dovetail slot;securing the first bucket to the rotor wheel using a wedge key;coupling a second bucket to the rotor wheel comprising inserting the dovetail of the second bucket into a second dovetail slot adjacent the first dovetail slot proximate the wedge key;rotating the rotor wheel assembly up to an operating speed; andcoupling the first bucket to the second bucket using the wedge key, wherein a frictional contact force is generated between the first bucket and the wedge key, and the second bucket and the wedge key. 16. The method in accordance with claim 15, wherein securing the first bucket to the rotor wheel using a wedge key comprises inserting the wedge key into a keyway formed in the platform of the first bucket. 17. The method in accordance with claim 16, wherein the platform of the first bucket includes a first surface, the first surface having the keyway formed therein, wherein the keyway includes an opposing tapered surface oriented at a first angle relative to the first surface. 18. The method in accordance with claim 17, wherein coupling the first bucket to the second bucket comprises using a wedge key having first face substantially parallel to the platform first surface and a second face substantially parallel to the opposing tapered surface. 19. The method in accordance with claim 15, wherein coupling the first bucket to the second bucket comprises coupling the first bucket platform to the second bucket platform to facilitate increasing a natural frequency of the first bucket and the second bucket. 20. The method in accordance with claim 15, further comprising reducing the rotor wheel assembly from the operating speed to a resting condition and acquiring standing vibration test data of the rotor wheel assembly for use in tuning and frequency validation.