Powertrain assembly for a wind turbine
A wind turbine nacelle including an outer cover defining an interior volume within which is housed a powertrain assembly comprising: a gearbox including an input shaft and an output shaft which are aligned on a common rotational axis, an electrical power generator connected to the output shaft of the gearbox. The power generator includes a generator cabinet that encloses, in an internal chamber, a stator at a radially outward position and a rotor in a radially inward position, the rotor being rotatable about the common rotational axis. The rotor comprises: a cylindrical field structure coupled to a rotor support frame; a gearbox connection flange that couples to the gearbox output shaft by a first fixing array; wherein the generator cabinet is provided with an opening that permits maintenance personal to gain access fully inside the internal chamber, and wherein the internal chamber is configured to allow maintenance personnel to access at least the first fixing array that couples the gearbox output shaft to the gearbox connection flange from a position fully inside the internal chamber.
1. A wind turbine nacelle including an outer cover defining an interior volume within which is housed a powertrain assembly comprising:
a gearbox including an input shaft and an output shaft which are aligned on a common rotational axis (R), an electrical power generator connected to the output shaft of the gearbox,
wherein the power generator includes a generator cabinet that encloses, in an internal chamber, a stator at a radially outward position and a rotor in a radially inward position, the rotor being rotatable about the common rotational axis, wherein the rotor comprises:
a cylindrical field structure coupled to a rotor support frame;
a gearbox connection flange that couples to the gearbox output shaft by a first fixing array;
wherein the generator cabinet is provided with an opening that permits maintenance personnel to gain access fully inside the internal chamber, and wherein the internal chamber is configured to allow maintenance personnel to access at least the first fixing array that couples the gearbox output shaft to the gearbox connection flange from a position fully inside the internal chamber.
2. The wind turbine nacelle of claim 1 , wherein the rotor further comprises a second fixing array that couples the gearbox connection flange to the rotor support frame, and wherein the internal chamber is configured to allow maintenance personnel to access the second fixing array from inside the internal chamber.
3. The wind turbine nacelle of claim 2 , wherein the first fixing array has an associated pitch circle diameter (D 1 ) and
wherein the second fixing array has an associated pitch circle diameter (D 3 ) and,
wherein the pitch circle diameter (D 1 ) of the first fixing array is smaller than the pitch circle diameter (D 3 ) of the second fixing array.
4. The wind turbine nacelle of claim 1 , wherein the rotor support frame is coupled to the cylindrical field structure at a rotor connection flange by a tie rod system including a plurality of tie rod tensioners configured to tension the tie rod system, and
wherein the internal chamber is configured to allow maintenance personnel to access the tie rod tensioners from inside the internal chamber.
5. The wind turbine nacelle of claim 4 , wherein the tie rod system includes a plurality of balancing adjustment masses configured to provide rotational balance to the cylindrical field structure and,
wherein the internal chamber is configured to allow maintenance personnel to access the balancing adjustment masses from inside the internal chamber.
6. The wind turbine nacelle of claim 1 , wherein the rotor further comprises a drive ring gear, and where the internal chamber is configured to allow maintenance personnel to access the drive ring gear from inside the internal chamber.
7. The wind turbine nacelle of claim 1 , wherein the cylindrical field structure defines a rotor internal diameter that is greater than 2 m.
8. The wind turbine nacelle of claim 1 , wherein the gearbox is a planetary gearbox with at least two stages.
9. The wind turbine nacelle of claim 1 , wherein the gearbox connection flange defines a first diameter (D 1 ) and wherein the tie-rod system defines a diameter (D 2 ), and wherein the first diameter (D 1 ) is less than the second diameter (D 2 ).
10. The wind turbine nacelle of claim 9 , wherein the first diameter (D 1 ) is less than 0.7 m and wherein the second diameter (D 2 ) is greater than 2 m.
11. The wind turbine nacelle of claim 1 , wherein the rotor connection flange of the rotor support frame is spaced from the gearbox connection flange along the rotational axis by a distance that is at least 25% of the maximum outer diameter of the rotor support frame.
12. The wind turbine nacelle of claim 11 , wherein the rotor connection flange of the rotor support frame is spaced from the gearbox connection flange along the rotational axis by a distance less than 0.7 m.
13. The wind turbine nacelle of claim 1 , wherein the rotor connection flange of the rotor support frame is spaced from the gearbox connection flange along the rotational axis (R) by a distance that is between 20% and 60% of the internal diameter of the rotor connection flange.
14. The wind turbine nacelle of claim 1 , wherein the rotor connection flange and the gearbox connection flange extend in mutually parallel planes.
15. The wind turbine nacelle of claim 1 , wherein the rotor support frame further includes a transition section extending between the rotor connection flange and the gearbox connection flange.
16. The wind turbine nacelle of claim 15 , wherein the transition section includes a generally frustoconical portion that defines a cone angle (B) of less than 30 degrees.
17. The wind turbine nacelle of claim 1 , wherein the rotor support frame includes a plurality of access apertures.
18. The wind turbine nacelle of claim 17 , wherein the access apertures define an opening of at least 100 cm 2 .
19. The wind turbine nacelle of claim 17 , wherein the access apertures are defined in an axially-facing end surface portion of the transition section.
20. The wind turbine nacelle of claim 17 , wherein the access apertures provide access therethrough to at least one of the following generator features:
i) a stray current protection system,
ii) one or more rotary sensor components associated with the gearbox output shaft,
iii) accelerometer systems,
iv) temperature sensors,
v) pitch tube sealing components.
21. The wind turbine nacelle of claim 1 , further comprising a closure which covers the opening in the generator cabinet, the closure being openable by maintenance personnel to gain access fully inside the internal chamber through the opening.
22. A wind turbine comprising a tower and a wind turbine nacelle according to claim 1 supported on top of the tower.
23. A method of servicing a wind turbine powertrain in a nacelle of a wind turbine, wherein the powertrain comprises a gearbox including an input shaft and an output shaft which are aligned on a common rotational axis (R), and an electrical power generator connected to the output shaft of the gearbox,
wherein the power generator includes a generator cabinet that defines an internal chamber which permits access to maintenance personnel inside the generator cabinet, the generator cabinet enclosing a stator at a radially outward position and a rotor in a radially inward position, the rotor being rotatable about the common rotational axis,
wherein the rotor comprises a cylindrical field structure coupled to a rotor support frame, and a gearbox connection flange that couples to the gearbox output shaft by a first fixing array;
wherein the method comprises: gaining access to the internal chamber of the electrical power generator through an opening defined by the generator cabinet; and, carrying out service operations from a position fully inside the internal chamber.
24. The method of claim 23 , wherein the service operations includes servicing at least one of the following items by maintenance personnel from a position fully inside the internal chamber:
i) a second fixing array that couples the gearbox connection flange to the rotor support frame;
ii) a tie rod system that couples the rotor support frame to the cylindrical field structure;
iii) a plurality of balancing adjustment masses configured to provide rotational balance to the cylindrical field structure;
iv) a drive ring gear.
25. The method of claim 23 , wherein the step of gaining access to the internal chamber of the electrical power generator includes releasing a closure that covers the opening of the generator cabinet thereby to reveal the opening for accessing the internal chamber.
26. The wind turbine nacelle of claim 1 , wherein the rotor connection flange of the rotor support frame is spaced from the gearbox connection flange along the rotational axis (R) by a distance that is between 20% and 40% of the internal diameter of the rotor connection flange.
27. The wind turbine nacelle of claim 17 , wherein the access apertures define an opening of at least 200 cm 2 .