Integrated high thermal conductive fiber as cooling fin for SMA actuator with expandable sleeve
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64C-013/28
F03G-007/06
F28F-013/00
F28F-021/02
F28F-021/06
출원번호
US-0593106
(2015-01-09)
등록번호
US-9664183
(2017-05-30)
발명자
/ 주소
Apdalhaliem, Sahrudine
Shome, Moushumi
Meredith, Kimberly D.
Ashmawi, Waeil M.
Safai, Morteza
Calkins, Frederick T.
출원인 / 주소
THE BOEING COMPANY
대리인 / 주소
Patterson + Sheridan, LLP
인용정보
피인용 횟수 :
0인용 특허 :
7
초록▼
Aspects of the present disclosure generally relate to an SMA actuator that includes a cooling device disposed within a torque tube. In one aspect, the cooling device includes a sliding sleeve, an expandable sleeve, and plurality of cooling fins coupled to the expandable sleeve. Axial movement of the
Aspects of the present disclosure generally relate to an SMA actuator that includes a cooling device disposed within a torque tube. In one aspect, the cooling device includes a sliding sleeve, an expandable sleeve, and plurality of cooling fins coupled to the expandable sleeve. Axial movement of the sliding sleeve relative to the expandable sleeve facilitates radial expansion of the expandable sleeve and urges the cooling fins into contact with the torque tube. The cooling fins function as heat sinks when in contact with the torque tube to facilitate the removal of heat from the torque tube to increase the cooling rate of the torque tube. During heating of the torque tube, the cooling fins may be spaced apart from the torque tube to reduce the thermal mass that is heated, thus increasing the heating rate of the torque tube.
대표청구항▼
1. An actuator, comprising: a torque tube; anda cooling device disposed within the torque tube, the cooling device comprising: a radially expandable sleeve;a sliding sleeve disposed within the radially expandable sleeve and axially movable relative to the radially expandable sleeve; andone or more c
1. An actuator, comprising: a torque tube; anda cooling device disposed within the torque tube, the cooling device comprising: a radially expandable sleeve;a sliding sleeve disposed within the radially expandable sleeve and axially movable relative to the radially expandable sleeve; andone or more cooling fins coupled to an outer surface of the radially expandable sleeve, wherein axial movement of the sliding sleeve relative to the radially expandable sleeve causes the radially expandable sleeve and the one or more cooling fins coupled thereto to expand radially outward from a first position to a second position. 2. The actuator of claim 1, wherein the torque tube comprises a shape memory alloy. 3. The actuator of claim 2, wherein the shape memory alloy comprises nickel-titanium alloy, copper-aluminum-nickel alloy, copper-zinc-aluminum alloy, or iron-manganese-silicon alloy. 4. The actuator of claim 1, wherein the radially expandable sleeve, the sliding sleeve, and the one or more cooling fins comprise a composite material. 5. The actuator of claim 4, wherein the composite material comprises polyethylene fiber, epoxy graphite, or thermal pitch fiber. 6. The actuator of claim 4, wherein the composite material has a specific thermal conductivity ratio between about 5000 (W-lb)/(m-Kelvin-in3) and about 9000 (W-lb)/(m-K-in3). 7. The actuator of claim 4, wherein the composite material has a thermal conductivity within range of about 440 Watts/meter-Kelvin to about 700 Watts/meter-Kelvin. 8. The actuator of claim 4, wherein the composite material has a tensile strength of about 280 ksi to about 380 ksi. 9. The actuator of claim 1, further comprising a heating coil disposed around and in contact with the torque tube. 10. The actuator of claim 1, wherein each of the cooling fins comprising a shaft having a contact pad at a radially outward end thereof. 11. The actuator of claim 10, wherein each contact pad has an arcuate shape. 12. The actuator of claim 1, wherein the sliding sleeve and the radially expandable sleeve have complementing tapered surfaces. 13. The actuator of claim 1, wherein the sliding sleeve is a polygonal cone or truncated polygonal cone. 14. The actuator of claim 1, wherein the actuator is coupled to a control surface of an aircraft to actuate the control surface. 15. A method of operating an actuator, the actuator having a torque tube including a shape memory alloy and a cooling device disposed within the torque tube, the method comprising: moving the actuator in a first direction by applying heat to the torque tube, wherein one or more cooling fins of the cooling device are spaced from the torque tube while applying heat;axially actuating a sliding sleeve of the cooling device relative to an expandable sleeve of the cooling device to expand the expandable sleeve and to urge the one or more cooling fins into contact with the torque tube; andmoving the actuator in a second direction opposite the first direction by cooling the torque tube, wherein the cooling the torque tube comprises flowing a cooling fluid adjacent the cooling fins. 16. The method of claim 15, wherein the cooling fluid flows axially through the torque tube. 17. The method of claim 15, further comprising adjusting a cooling rate of the torque tube by adjusting a contact pressure between the torque tube and the one or more cooling fins. 18. The method of claim 15, further comprising axially actuating the sliding sleeve in a direction to contract the expandable sleeve to space the one or more cooling fins from the torque tube. 19. A cooling device, comprising: a radially expandable sleeve;a sliding sleeve disposed within the radially expandable sleeve and axially movable relative to the radially expandable sleeve; andone or more cooling fins coupled to an outer surface of the radially expandable sleeve, wherein axial movement of the sliding sleeve relative to the radially expandable sleeve causes the radially expandable sleeve and the cooling fins coupled thereto to expand radially outward from a first position to a second position. 20. The cooling device of claim 19, wherein the radially expandable sleeve, the sliding sleeve, and the one or more cooling fins comprise a composite material. 21. The cooling device of claim 20, wherein the composite material comprises polyethylene fiber, epoxy graphite, or thermal pitch fiber. 22. The cooling device of claim 20, wherein the composite material has a specific thermal conductivity ratio between about 5000 (W-lb)/(m-Kelvin-in3) and about 9000 (W-lb)/(m-K-in3). 23. The cooling device of claim 20, wherein the composite material has a thermal conductivity within range of about 440 Watts/meter-Kelvin to about 700 Watts/meter-Kelvin. 24. The cooling device of claim 20, wherein the composite material has a tensile strength of about 280 ksi to about 380 ksi. 25. The cooling device of claim 19, wherein each of the cooling fins comprising a shaft having a contact pad at radially outward end thereof. 26. The cooling device of claim 25, wherein each contact pad has an arcuate shape. 27. The cooling device of claim 19, the sliding sleeve and the expandable sleeve have complementing tapered surfaces. 28. The cooling device of claim 19, wherein the sliding sleeve is a polygonal cone or truncated polygonal cone. 29. The cooling device of claim 19, wherein the cooling fins extend radially from the outward surface of the radially expandable sleeve.
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이 특허에 인용된 특허 (7)
Smith, Charles; Chau, Michael M.; Emigh, Roger A.; Dean, Nancy F., Electronic device having fibrous interface.
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