Root end assembly configuration for a wind turbine rotor blade and associated forming methods
An assembly configuration between a wind turbine rotor blade and a rotor hub includes a rotor hub having one or more pitch bearings, with each pitch bearing having an outer diameter race and an inner diameter race. Rotor blades are affixed to the respective pitch bearing rings, with the rotor blades having a root end with an outer diameter. An adaptor is configured between the root end and the pitch bearing, with the adaptor affixed to the inner diameter race and the root end affixed to the adaptor. The adaptor defines a mounting surface for the root end radially inward of the pitch bearing such that the root end outer diameter is less than the diameter of the inner diameter race.
1. An assembly configuration between a wind turbine rotor blade and a rotor huh, comprising:
a rotor hub having one or more pitch bearings, said bearings having an outer diameter race and an inner diameter race;
a rotor blade affixed to said pitch bearings, said rotor blades comprising a root end having an outer diameter;
an adaptor configured between said root end and said bearing, said adaptor affixed to said inner diameter race at a first location and said root end affixed to said adaptor;
said adaptor defining a mounting surface for said root end radially inward of said inner diameter race such that said root end outer diameter is less than an inner diameter of said pitch bearing; and
said root end separately bolted directly to said mounting surface radially inward of said first location for attachment of said rotor blade said pitch bearing; and
said adaptor comprising a flat, planar, member so as to lie flush against said inner diameter race, said adaptor and said inner diameter race having the same outer diameter.
2. The assembly configuration as in claim 1 , wherein said adaptor comprises a plate member.
3. The assembly configuration as in claim 2 , wherein said adaptor comprises a ring member.
4. The assembly configuration as in claim 1 , wherein said adaptor is formed from a material the same or a greater stiffness than said rotor blades.
5. The assembly configuration as in claim 4 , wherein said rotor blades are a composite material and said adaptor is a composite or metal.
6. An assembly configuration between a wind turbine rotor blade and a rotor hub, comprising:
a rotor hub having one or more pitch bearings, said bearings having an outer diameter race and an inner diameter race;
a rotor blade affixed to said pitch bearings, said rotor blades comprising a root end having an outer diameter;
an adaptor configured between said root end and said bearing, said adaptor affixed to said inner diameter race at a first location and said root end affixed to said adaptor;
said adaptor defining a mounting surface for said root end radially inward of said inner diameter race such that said root end outer diameter is less than an inner diameter of said pitch bearing;
said root end separately bolted directly to said mounting surface radially inward of said first location for attachment of said rotor blade to said pitch bearing;
wherein said adaptor has a raised spanwise profile relative to said pitch bearing and comprises side walls extending transversely outward at an angle less than 90 degrees from a radially outer ring of said adaptor, said mounting surface defined at an end of said side walls;
wherein the radially outer ring is affixed to said inner diameter race, said mounting surface circumscribed within said outer ring; and
wherein said adaptor comprises a truncated cross-sectional profile.
7. The assembly configuration as in claim 6 , wherein said adaptor comprises a radially outer ring affixed to said inner diameter race, said mounting surface circumscribed within said outer ring.
8. The assembly configuration as in claim 7 , wherein said adaptor is metal and said rotor blade is a composite material.
9. The assembly configuration as in claim 8 , wherein said mounting surface is defined in a non-parallel plane relative to a plane of said inner diameter race such that a centerline axis of said blade is offset relative to a centerline axis of said pitch bearing.