Multiple piece turbine rotor blade
A spar and shell turbine rotor blade with a spar and a tip cap formed as a single piece, the spar includes a bottom end with dovetail or fir tree slots that engage with slots on a top end of a root section, and a platform includes an opening on a top surface for insertion of the spar in which a shell made from an exotic high temperature resistant material is secured between the tip cap and the platform. The spar is tapered to form thinner walls at the tip end to further reduce the weight and therefore a pulling force due to blade rotation. The spar and tip cap piece is made from a NiAL material to further reduce the weight and the pulling force.
1. A multiple piece turbine rotor blade comprising:
a single piece spar and tip cap;
a dovetail or fir tree configuration on a bottom end of the spar;
a root having a top end with a dovetail or fir tree configuration to engage the spar to prevent radial displacement of the spar with respect to the root;
the root having a fir tree configuration on the bottom end for engagement with a slot formed within a rotor disk;
a platform with an opening to receive the spar;
the platform having two legs each with a similar shaped fir tree of the root; and,
a shell secured between the tip cap and the platform.
2. The multiple piece turbine rotor blade of claim 1 , and further comprising:
the spar is tapered such that walls of the spar are thinner at the tip end than at the platform end.
3. The multiple piece turbine rotor blade of claim 1 , and further comprising:
the shell is a single piece shell formed from an exotic high temperature resistant material that cannot be cast or machined.
4. The multiple piece turbine rotor blade of claim 1 , and further comprising:
the spar and tip cap are formed from a Nickel Aluminide material.
5. The multiple piece turbine rotor blade of claim 1 , and further comprising:
the spar includes a rib extending from a pressure side to a suction side of the spar.