IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0813505
(2015-07-30)
|
등록번호 |
US-9951750
(2018-04-24)
|
발명자
/ 주소 |
- Caruso, Christopher Daniel
- Yarbrough, Aaron A.
- Hynum, Daniel Alan
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
0 인용 특허 :
5 |
초록
▼
A rotor blade may generally include a shell forming an outer skin of the blade, with the shell defining a chordwise curvature. The rotor blade may also include a spar cap extending within the shell along a spanwise direction of the blade. The spar cap may be formed from an assembly of pre-cured lami
A rotor blade may generally include a shell forming an outer skin of the blade, with the shell defining a chordwise curvature. The rotor blade may also include a spar cap extending within the shell along a spanwise direction of the blade. The spar cap may be formed from an assembly of pre-cured laminate plates. In addition, the rotor blade may include an interior shelf positioned directly between the shell and the spar cap. The interior shelf may include an outer surface extending adjacent to the shell and an inner surface opposite the outer surface. The outer surface may define a curved profile generally corresponding to a portion of the chordwise curvature of the shell and the inner surface may define a planar surface along which the spar cap extends in a chordwise direction of the blade. The interior shelf may correspond to a pre-fabricated insert for the blade.
대표청구항
▼
1. A rotor blade for a wind turbine, the rotor blade comprising: a shell forming an outer skin of the rotor blade, the shell defining a pressure side and a suction side extending between leading and trailing edges of the rotor blade, the shell including a leading edge segment and a trailing edge seg
1. A rotor blade for a wind turbine, the rotor blade comprising: a shell forming an outer skin of the rotor blade, the shell defining a pressure side and a suction side extending between leading and trailing edges of the rotor blade, the shell including a leading edge segment and a trailing edge segment, the leading and trailing edge segments being joined together at pressure and suction side joints defined along the pressure and suction sides of the rotor blade, respectively, the shell defining a chordwise curvature extending adjacent to the locations of the pressure and suction side joints;a spar cap extending within the shell along a spanwise direction of the rotor blade and being aligned with the pressure and suction side joints between the pressure and suction sides of the rotor blade, the spar cap being formed from an assembly of pre-cured laminate plates; andan interior shelf positioned directly between the shell and the spar cap at the location of one of the pressure side joint or the suction side joint, the interior shelf including an outer surface extending adjacent to the shell and an inner surface opposite the outer surface, the outer surface defining a curved profile generally corresponding to a portion of the chordwise curvature of the shell, the inner surface defining a planar surface along which the spar cap extends in a chordwise direction of the rotor blade,wherein the interior shelf corresponds to a pre-fabricated insert for the rotor blade. 2. The rotor blade of claim 1, wherein the pre-cured laminate plates are stacked one on top of the other directly onto the inner surface of the interior shelf. 3. The rotor blade of claim 1, wherein the interior shelf is formed from a low-density material. 4. The rotor blade of claim 3, wherein the low-density material corresponds to a low-density foam material. 5. The rotor blade of claim 1, wherein the planar surface defined by the inner surface of the interior shelf extends generally parallel to the chordwise direction of the rotor blade. 6. The rotor blade of claim 1, wherein the spar cap defines a rectangular cross-sectional shape. 7. The rotor blade of claim 1, wherein each pre-cured laminate plate forms a single layer of the spar cap. 8. The rotor blade of claim 1, wherein the pre-cured laminate plates correspond to pultruded plates. 9. The rotor blade of claim 1, wherein the interior shelf corresponds to a first interior shelf extending directly between the spar cap and the leading edge segment, further comprising a second interior shaft extending directly between the spar cap and the trailing edge segment. 10. The rotor blade of claim 9, wherein the first and second interior shelves terminate within the rotor blade at the location of the one of the pressure side joint or the suction side joint. 11. The rotor blade of claim 10, wherein a joint is defined between the first and second interior shelves at the location of the one of the pressure side joint or the suction side joint. 12. A rotor blade for a wind turbine, the rotor blade comprising: a shell forming an outer skin of the rotor blade, the shell defining a pressure side and a suction side extending between leading and trailing edges of the rotor blade, the shell including a leading edge segment and a trailing edge segment, the leading and trailing edge segments being joined together at pressure and suction side joints defined along the pressure and suction sides of the rotor blade, respectively, the shell defining a chordwise curvature extending adjacent to the locations of the pressure and suction side joints;a spar cap extending within the shell along a spanwise direction of the rotor blade and being aligned with the pressure and suction side joints between the pressure and suction sides of the rotor blade, the spar cap being formed from an assembly of pre-cured laminate plates; anda first interior shelf positioned directly between the leading edge segment and the spar cap, the first interior shelf including a first outer surface extending adjacent to the leading edge segment and a first inner surface opposite the first outer surface, the first outer surface defining a curved profile generally corresponding to a portion of the chordwise curvature of the shell defined by the leading edge segment, the first inner surface defining a first planar surface along which the spar cap extends in a chordwise direction of the rotor blade;a second interior shelf positioned directly between the trailing edge segment and the spar cap, the second interior shelf including a second outer surface extending adjacent to the trailing edge segment and a second inner surface opposite the second outer surface, the second outer surface defining a curved profile generally corresponding to a portion of the chordwise curvature of the shell defined by the trailing edge segment, the second inner surface defining a second planar surface along which the spar cap extends in the chordwise direction of the rotor blade. 13. The rotor blade of claim 12, wherein the first and second interior shelves terminate within the rotor blade at the location of one of the pressure side joint or the suction side joint. 14. The rotor blade of claim 13, wherein a joint is defined between the first and second interior shelves at the location of the one of the pressure side joint or the suction side joint. 15. The rotor blade of claim 12, wherein the first and second interior shelves correspond to pre-fabricated inserts for the rotor blade. 16. The rotor blade of claim 12, wherein the first and second interior shelves are formed from a low-density material. 17. The rotor blade of claim 12, wherein the first and second planar surfaces are aligned when the leading and trailing edge segments are coupled together at the pressure and suctions side joints such that a substantially continuous planar surface is defined across the first and second interior shelves along which the spar cap extends.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.