ROTOR HUB FOR A WIND POWER INSTALLATION, AND CORRESPONDING ROTOR ARRANGEMENT AND WIND POWER INSTALLATION
20220154687 · 2022-05-19
Inventors
Cpc classification
F05B2220/7066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2250/231
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0608
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0691
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/82
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
F03D1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/80
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A rotor hub for a wind power installation, with at least two flange portions each for receiving a rotor blade, wherein the rotor hub has a housing with a wall which is interrupted by the flange portions, wherein the housing has a wall region between two adjacent flange portions. A rotor arrangement for a wind power installation, and a wind power installation. A surface portion with cylindrical curvature is formed in the wall region.
Claims
1. A rotor hub for a wind power installation, comprising: a plurality of flange portions, each flange portion being configured to receive a rotor blade, a housing having a wall that extends to two of the plurality of the flange portions, wherein the housing has a wall region between two adjacent flange portions, and wherein a surface portion with cylindrical curvature is located in the wall region.
2. The rotor hub according to claim 1, wherein the plurality of flange portions are three flange portions, wherein the surface portion with the cylindrical curvature is located between each two adjacent flange portions of the three flange portions.
3. The rotor hub according to claim 1, wherein the surface portion with the cylindrical curvature is located in the region between two adjacent flange portions, wherein peripheries of the two adjacent flange portions have a smallest mutual distance.
4. The rotor hub according to claim 1, wherein the housing adjacent to the wall region has one or more flat wall regions that are formed from at least one triangular base surface.
5. The rotor hub according to claim 4, wherein the housing of the rotor hub adjacent to the flat wall regions has free-form wall regions.
6. The rotor hub according to claim 5, wherein the free-form wall regions are curved.
7. The rotor hub according to claim 1, wherein adjacent wall regions transform into one another without kinks.
8. The rotor hub according to claim 1, comprising a plurality of surface portions with cylindrical curvature located between all pairs of two adjacent flange portions.
9. The rotor hub according to claim 1, wherein a collar is located on at least one flange portion and extends radially outwardly with respect to a rotational axis of the rotor hub, and wherein the collar is configured to increase the stiffness of the collar against carding moments.
10. The rotor hub according to claim 9, wherein the collar is attached to the rotor hub by a screw connection.
11. The rotor hub according to claim 9, wherein the collar is integrally formed with the rotor hub.
12. A rotor arrangement for a wind power installation, comprising: a rotor hub having: a plurality of flange portions, each flange portion being configured to receive a rotor blade, a housing having a wall that extends to two of the plurality of the flange portions, wherein the housing has a wall region between two adjacent flange portions, and wherein a surface portion with cylindrical curvature is located in the wall region, and a plurality of rotor blades on the rotor hub, wherein each of the plurality of rotor blades have an angle of attack that is configured to be adjusted and are received at a respective flange portion of the plurality of flange portions of the rotor hub by a respective blade bearing.
13. A wind power installation comprising: a tower, a nacelle mounted on the tower by a rotary connection, a generator located in the nacelle, and the rotor arrangement according to claim 12 connected to the generator for driving the generator.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
[0028] The invention is described below with reference to the appended figures showing preferred exemplary embodiments. The drawings show:
[0029]
[0030]
[0031]
[0032]
[0033]
[0034]
DETAILED DESCRIPTION
[0035]
[0036] The rotor hub 114 is illustrated in
[0037] The surface portion 124 with cylindrical curvature 126 is arranged in the region between two adjacent flange portions 116 at which peripheries u.sub.1, u.sub.2, u.sub.3 of the adjacent flange portions 116 have the smallest mutual distance d.sub.u. The housing 118 of the rotor hub 114 has flat wall regions 128 adjacent to the wall region 122. The flat wall regions 128 are formed from at least one triangular base surface 130. The housing 118 of the rotor hub 114 furthermore comprises free-form wall regions 132 adjacent to the flat wall regions 128. The free-form wall regions 132 are configured curved 134. Adjacent wall regions 122, 128, 130 transform into one another without kinks.
[0038] As evident in particular from
[0039]
[0040] During operation, a bending of the flange portion 116 of the rotor hub 114 causes high circumferential hoop stresses in the bearing outer ring 148 of the blade bearing 146. In particular, the bearing bore 156 is exposed to such hoop stresses, whereby the bearing bores 156 are susceptible to the formation of fatigue cracks. Because of the flattening of the rotor hub 114 relative to an ideal spherical geometry as known from the prior art, in the present case the lever arm H between the surface of the housing 118 of the rotor hub 114 and the bearing bore 156 of the bearing outer ring 148 or corresponding bearing fixing bolts 150 is reduced, whereby the occurrence of fatigue cracks in the region of the bearing bores 156 of the bearing outer ring 148 is avoided.
[0041]
LIST OF REFERENCE SIGNS USED
[0042] 100 Wind power installation [0043] 102 Tower [0044] 104 Nacelle [0045] 106 Rotor arrangement [0046] 108 Rotor blade [0047] 110 Spinner [0048] 112 Generator [0049] 114 Rotor hub [0050] 115 Rotary connection [0051] 116 Flange portion [0052] 118 Housing [0053] 120 Wall [0054] 122 Wall region between two adjacent flange portions [0055] 124 Surface portion [0056] 126 Cylindrical curvature [0057] 128 Flat wall regions [0058] 130 Triangular base surfaces [0059] 132 Free-form wall region [0060] 134 Curvature of free-form wall region [0061] 136 Rotational axis of hub [0062] 138 Bulkhead [0063] 140 Receiver for actuator for blade angle of attack [0064] 142 Generator connection flange [0065] 144 Spinner connection flange [0066] 146 Blade bearing [0067] 148 Bearing outer ring [0068] 150 Bearing fixing bolts [0069] 152 Bearing inner ring [0070] 154 Blade flange [0071] 156 Bearing bore of bearing outer ring [0072] 214 Rotor hub [0073] 216 Flange portion [0074] 218 Housing [0075] 220 Wall [0076] 238 Bulkhead [0077] 256 Collar [0078] d.sub.u Distance of peripheries of flange portions [0079] H Lever arm [0080] u.sub.1, u.sub.2, u.sub.3 Peripheries of flange portions
[0081] The various embodiments described above can be combined to provide further embodiments. These and other changes can be made to the embodiments in light of the above-detailed description. In general, in the following claims, the terms used should not be construed to limit the claims to the specific embodiments disclosed in the specification and the claims, but should be construed to include all possible embodiments along with the full scope of equivalents to which such claims are entitled. Accordingly, the claims are not limited by the disclosure.