IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0512656
(2010-11-30)
|
등록번호 |
US-9416768
(2016-08-16)
|
우선권정보 |
EP-09177783 (2009-12-02) |
국제출원번호 |
PCT/EP2010/068521
(2010-11-30)
|
§371/§102 date |
20120718
(20120718)
|
국제공개번호 |
WO2011/067248
(2011-06-09)
|
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
0 인용 특허 :
20 |
초록
▼
The present invention relates to an airfoil shaped body with a leading edge and a trailing edge extending along the longitudinal extension of the body and defining a profile chord, the airfoil shaped body comprising an airfoil shaped facing that forms the outer surface of the airfoil shaped body and
The present invention relates to an airfoil shaped body with a leading edge and a trailing edge extending along the longitudinal extension of the body and defining a profile chord, the airfoil shaped body comprising an airfoil shaped facing that forms the outer surface of the airfoil shaped body and surrounds an internal volume of the body, a distance member that is connected to the facing inside the body and extends from the facing and into the internal volume of the body, and at least one reinforcing member that operates in tension for reinforcing the facing against inward deflections and that is connected to the facing inside the internal volume of the body at the same side of the profile chord as the connection of the distance member to the facing and to the distance member at a distance from the facing.
대표청구항
▼
1. An airfoil shaped body with a leading edge and a trailing edge extending along a longitudinal direction of the airfoil shaped body and defining a profile chord, the airfoil shaped body having a suction side and a pressure side, both of which extend between the leading edge and the trailing edge,
1. An airfoil shaped body with a leading edge and a trailing edge extending along a longitudinal direction of the airfoil shaped body and defining a profile chord, the airfoil shaped body having a suction side and a pressure side, both of which extend between the leading edge and the trailing edge, the airfoil shaped body comprising: an airfoil shaped facing that forms an outer surface of the airfoil shaped body and surrounds an internal volume of the airfoil shaped body,at least one reinforcing member that is connected to the airfoil shaped facing with a first connection inside the internal volume only adjacent a first side of the airfoil shaped body, the first side being one of the suction side and the pressure side, and extends transversal to the longitudinal direction of the airfoil shaped body; anda distance member that is in contact with airfoil shaped facing, at a substantially flat part of the airfoil shaped facing inside the internal volume of the airfoil shaped body at a same side of the profile chord as the first connection, and at a lateral distance from the first connection and extends from the airfoil shaped facing and into the internal volume of the body, whereinthe at least one reinforcing member is in contact with the distance member at a second connection at a distance from the airfoil shaped facing inside the internal volume of and only adjacent the first side of the airfoil shaped body and operates in tension for reinforcing the airfoil shaped facing against inward deflections, andthe at least one reinforcing member is further connected to the airfoil shaped facing with a third connection only adjacent the first side of the airfoil shaped body and at a side of the distance member opposite the first connection and on a same side of the profile chord as the connection of the distance member to the airfoil shaped facing. 2. An airfoil shaped body according to claim 1, wherein one of the at least one reinforcing member is connected to the airfoil shaped facing with the first connection and another one of the at least one reinforcing member is connected to the airfoil shaped facing with the third connection and is displaced along the longitudinal direction of the airfoil shaped body with relation to the one of the at least one reinforcing member with the first connection. 3. An airfoil shaped body according to claim 1, wherein the at least one reinforcing member comprises a plurality of elongated reinforcing members extending transversal to the longitudinal direction of the airfoil shaped body and positioned in spaced relationship along the longitudinal extension of the airfoil shaped body. 4. An airfoil shaped body according to claim 1, wherein the at least one reinforcing member is selected from the group of a wire, a rope, a thread, a fiber, and a web of fabric. 5. An airfoil shaped body according to claim 1, wherein the at least one reinforcing member also operates in compression for reinforcing the airfoil shaped facing against inward deflections. 6. An airfoil shaped body according to claim 5, wherein the at least one reinforcing member has the shape of an element selected from the group of a rod, a bar, a plate, a tube. 7. An airfoil shaped body according to claim 1, further comprising a girder extending inside the airfoil shaped body and along the longitudinal direction of the airfoil shaped body and that is connected to the airfoil shaped facing, and wherein the distance member forms part of the girder. 8. An airfoil shaped body according to claim 1, wherein a part of the airfoil shaped facing constitutes the distance member. 9. An airfoil shaped body according to claim 1, further comprising two girders extending inside the airfoil shaped body and along the longitudinal direction of the body and with a mutual distance perpendicular to the longitudinal direction of the body and that are connected to the airfoil shaped facing, and wherein the distance member is located between the two girders, and whereinthe at least one reinforcing member is connected to the airfoil shaped facing proximate respective connections of the girders to the airfoil shaped facing. 10. An airfoil shaped body according to claim 1, wherein the distance member is formed by a plurality of distance members. 11. An airfoil shaped body according to claim 1, wherein a space between the at least one reinforcing member and the airfoil shaped facing is at least partly filled with a filler material. 12. An airfoil shaped body according to claim 1, wherein the at least one reinforcing member and a part of the airfoil shaped facing constitute a cap part. 13. A wind turbine with a blade that is an airfoil shaped body according to claim 1. 14. An aircraft with a wing that is an airfoil shaped body according to claim 1. 15. A method for manufacturing an airfoil shaped body, the airfoil shaped body having a leading edge and a trailing edge extending along a longitudinal direction of the airfoil shaped body and defining a profile chord, the method comprising: providing at least a part of an airfoil shaped facing of the airfoil shaped body,providing a distance member,contacting the distance member to an internal surface of the airfoil shaped facing,providing at least one reinforcing member,connecting the at least one reinforcing member to a first position at the internal surface of the airfoil shaped facing at a distance from the distance member and at the same side of the profile chord as the contact of the distance member with the airfoil shaped facing and only adjacent a first side of the airfoil shaped body, the first side being one of a suction side and a pressure side,contacting the at least one reinforcing member to the distance member at a distance from the airfoil shaped facing only adjacent the first side of the airfoil shaped body, andconnecting the at least one reinforcing member to a second position at the internal surface of the airfoil shaped facing at a distance from the distance member and at a side of the distance member opposite from the first position and at a same side of the profile chord as the contact of the distance member with the airfoil shaped facing and only adjacent the first side of the airfoil shaped body. 16. A method according to claim 15, further comprising: pre-tensioning the at least one reinforcing member with a desired amount of tension. 17. A method according to claim 15, further comprising: providing a filler material in a space between the at least one reinforcing member and the internal surface of the airfoil shaped facing. 18. A method according to claim 15, further comprising: providing at least one girder and connecting the girder to the internal surface of the airfoil shaped facing. 19. A method according to any of claim 15, wherein at least one of providing at least a part of an airfoil shaped facing, providing a distance member, and providing at least one reinforcing member includes building up layers of fiber materials.
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