[특허]Rotor blade for a rotary wing aircraft

Eurocopter Deutschland GmbH

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Rotor blade for a rotary wing aircraft

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-027/615
미국특허분류(USC)	416/023;
출원번호	US-0158928 (2006-12-08)
등록번호	US-8162607 (2012-04-24)
우선권정보	DE-10 2005 061 751 (2005-12-21)
국제출원번호	PCT/EP2006/011812 (2006-12-08)
§371/§102 date	20081121 (20081121)
국제공개번호	WO2007/079855 (2007-07-19)
발명자 / 주소	Grohmann, Boris Maucher, Christoph Altmikus, Andree Mangelsdorf, Stephan
출원인 / 주소	Eurocopter Deutschland GmbH
대리인 / 주소	Brooks Kushman P.C.
인용정보	피인용 횟수 : 5 인용 특허 : 16

초록
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A rotor blade including a rotor blade profile including a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core. A covering skin including an upper skin and a lower skin encase the profile core. A reversibly bendable flexural actuator including a first actuator end disposed at the trailing edge region of the rotor blade profile and a second actuator end projecting past the profile body toward the trailing edge. The second actuator end forms part of the trailing edge region and forms a movabl...

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1. A rotor blade comprising: a rotor blade profile having a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core and a covering skin including an upper skin and a lower skin, the covering skin encasing the profile core; anda reversibly bendable flexural actuator including a first actuator end to be fastened at an end region of the profile body, the end region pointing towards the trailing edge, and a second actuator end projecting past the profile body toward the trailing edge;wherein the projecting second actuator end forms part of the profile trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon bending of the reversibly bendable flexural actuator,wherein the reversibly bendable flexural actuator includes a planar shape and at least one of a plate shape and a ribbon shape,wherein the reversibly bendable flexural actuator is disposed on at least one support layer wherein the at least one support layer is plate-shaped and reversibly bendable. 2. The rotor blade as recited in claim 1, wherein the reversibly bendable flexural actuator further includes a shape-memory alloy. 3. The rotor blade as recited in claim 1, wherein the reversibly bendable flexural actuator includes a piezoelectric element so that the reversibly bendable flexural actuator is a piezoelectric flexural actuator thereby being deformable by delivery of an electric current. 4. The rotor blade as recited in claim 1, wherein the reversibly bendable flexural actuator includes a piezoelectric flexural actuator and wherein at least one of the piezoelectric flexural actuator and the at least one support layer includes a varying thickness. 5. The rotor blade as recited in claim 1, wherein the at least one support layer includes a fiber composite. 6. The rotor blade as recited in claim 5, wherein the fiber composite includes a plastic material reinforced with a glass fiber. 7. The rotor blade as recited in claim 1, wherein the reversibly bendable flexural actuator is disposed on both sides of the at least one support layer. 8. The rotor blade as recited in claim 1, wherein the reversibly bendable flexural actuator is disposed on one side of the at least one support layer. 9. The rotor blade as recited in claim 1, wherein the at least one support layer includes a return device. 10. A rotor blade comprising: a rotor blade profile having a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core and a covering skin including an upper skin and a lower skin, the covering skin encasing the profile core; anda reversibly bendable flexural actuator including a first actuator end to be fastened at an end region of the profile body, the end region pointing towards the trailing edge, and a second actuator end projecting past the profile body toward the trailing edge;wherein the projecting second actuator end forms part of the profile trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon bending of the reversibly bendable flexural actuator,wherein the reversibly bendable flexural actuator includes a planar shape and at least one of a plate shape and a ribbon shape, andwherein the movable rotor blade flap is covered with a first filler material being flexible and flexurally elastic and the first filler material forming an outer profile of the movable rotor blade flap. 11. The rotor blade as recited in claim 10, wherein the first filler material further extends along the profile body. 12. The rotor blade as recited in claim 10, wherein the first filler material is a homogenous material. 13. The rotor blade as recited in claim 12, wherein the first filler material includes at least one of a silicone material and a foam material. 14. The rotor blade as recited in claim 10, wherein the first filler material is an inhomogeneous material. 15. The rotor blade as recited in claim 14, wherein the inhomogeneous material includes at least one of a rib-like, a framework-like and a skeleton-like, filler material. 16. The rotor blade as recited in claim 10, wherein the first filler material includes a protective skin, the protective skin being flexible and flexurally elastic and including an outer contour of the rotor blade profile in at least a rotor blade flap region. 17. The rotor blade as recited in claim 16, wherein first filler material is integrated with the protective skin. 18. The rotor blade as recited in claim 16, wherein the protective skin includes a protective layer applied on the first filler material. 19. A rotor blade comprising: a rotor blade profile having a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core and a covering skin including an upper skin and a lower skin, the covering skin encasing the profile core; anda reversibly bendable flexural actuator including a first actuator end to be fastened at an end region of the profile body, the end region pointing towards the trailing edge, and a second actuator end projecting past the profile body toward the trailing edge;wherein the projecting second actuator end forms part of the profile trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon bending of the reversibly bendable flexural actuator,wherein the reversibly bendable flexural actuator includes a planar shape and at least one of a plate shape and a ribbon shape, andwherein the upper skin and the lower skin extend to the first actuator end and are configured so as to retain the reversibly bendable flexural actuator and wherein the second actuator end freely projects between the upper skin and the lower skin. 20. A rotor blade comprising: a rotor blade profile having a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core and a covering skin including an upper skin and a lower skin, the covering skin encasing the profile core; anda reversibly bendable flexural actuator including a first actuator end to be fastened at an end region of the profile body, the end region pointing towards the trailing edge, and a second actuator end projecting past the profile body toward the trailing edge;wherein the projecting second actuator end forms part of the profile trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon bending of the reversibly bendable flexural actuator,wherein the reversibly bendable flexural actuator includes a planar shape and at least one of a plate shape and a ribbon shape, andwherein the covering skin extends to the reversibly bendable flexural actuator and wherein the covering skin in a region that extends to the reversibly bendable flexural actuator has a reduced thickness compared to the covering skin in a region that does not extend to the reversibly bendable flexural actuator. 21. A rotor blade comprising: a rotor blade profile having a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core and a covering skin including an upper skin and a lower skin, the covering skin encasing the profile core; anda reversibly bendable flexural actuator including a first actuator end to be fastened at an end region of the profile body, the end region pointing towards the trailing edge, and a second actuator end projecting past the profile body toward the trailing edge;wherein the projecting second actuator end forms part of the profile trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon bending of the reversibly bendable flexural actuator,wherein the reversibly bendable flexural actuator includes a planar shape and at least one of a plate shape and a ribbon shape, andwherein the covering skin extends to the reversibly bendable flexural actuator and includes a local discontinuity in reversibly bendable flexural strength wherein the local discontinuity includes a virtual rotor blade flap articulation configured to allow the profile trailing edge region to be deformable so as to include the arc-shaped movable rotor blade flap deflection. 22. A rotor blade comprising: a rotor blade profile having a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core and a covering skin including an upper skin and a lower skin, the covering skin encasing the profile core; anda reversibly bendable flexural actuator including a first actuator end to be fastened at an end region of the profile body, the end region pointing towards the trailing edge, and a second actuator end projecting past the profile body toward the trailing edge;wherein the projecting second actuator end forms part of the profile trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon bending of the reversibly bendable flexural actuator,wherein the reversibly bendable flexural actuator includes a planar shape and at least one of a plate shape and a ribbon shape; anda mounting device disposed in the end region of the profile body for mounting the reversibly bendable flexural actuator and wherein at least one of the reversibly bendable flexural actuator and the profile trailing edge region is configured to detachably mount on the mounting device. 23. The rotor blade as recited in claim 22, wherein the mounting device includes a terminating profile structure connectable to the profile trailing edge region of the profile body, wherein the terminating profile structure includes at least one of an insertion opening configured to allow an insertion of the first actuator end and a mounting projection configured to allow a mounting of the first actuator end. 24. The rotor blade as recited in claim 23, wherein the first actuator end includes a connector region slidable onto the mounting projection. 25. The rotor blade as recited in claim 23, wherein the first actuator end includes a ribbon shape and is configured to be disposed planar and securable to the mounting projection. 26. The rotor blade as recited in claim 23, wherein the terminating profile structure includes a first U-shaped profile having an open side facing the profile tip region and including a limb connectable directly or indirectly to the upper and lower covering skin. 27. The rotor blade as recited in claim 26, wherein the first U-shaped profile includes a profile region disposed on a side facing the trailing edge, wherein the profile region includes the mounting projection. 28. The rotor blade as recited in claim 26, wherein the first U-shaped profile includes at least one profile element configured to mount on the U-shaped profile, the at least one profile element configured to fit around the U-shaped profile and including a first profile region directly or indirectly connectable to at least one of the upper skin and the lower skin and including a second profile region facing the trailing edge, wherein the second profile region includes the mounting projection. 29. The rotor blade as recited in claim 26, wherein the first U-shaped profile includes a loop-shaped profile region, the loop-shaped profile region extending toward the profile tip region and toward the profile core and wherein the loop-shaped profile region includes an indentation open toward the trailing edge, the indentation including the insertion opening and wherein the loop-shaped profile region is enclosable from a side of the profile core and wherein the loop-shaped profile includes a second substantially U-shaped profile including an open side facing the trailing edge. 30. The rotor blade as recited in claim 26, wherein the first U-shaped profile is partially fillable with a second filler material including a stiffness greater than a stiffness of a material of the profile core. 31. The rotor blade as recited in claim 22, wherein the mounting device includes at least one of an electric interface and an electrical connector configured to at least one of supply energy to and control the flexural actuator.

이 특허에 인용된 특허 (16)

이 특허를 인용한 특허 피인용횟수: 5

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Rotor blade for a rotary wing aircraft

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Rotor blade for a rotary wing aircraft

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이 특허에 인용된 특허 (16)

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