Blades having coolant channels lined with a shape memory alloy and an associated fabrication method
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-005/16
F01D-005/18
출원번호
US-0080208
(2002-02-19)
발명자
/ 주소
Villhard, Robert L.
출원인 / 주소
The Boeing Company
대리인 / 주소
Alston & Bird LLP
인용정보
피인용 횟수 :
10인용 특허 :
41
초록▼
A damped blade is provided that includes a blade structural member defining at least one coolant channel and a liner formed of a shape memory alloy extending at least partially along the at least one coolant channel defined by the blade structural member. The shape memory alloy that forms the liner
A damped blade is provided that includes a blade structural member defining at least one coolant channel and a liner formed of a shape memory alloy extending at least partially along the at least one coolant channel defined by the blade structural member. The shape memory alloy that forms the liner is maintained generally at its transition temperature by means of coolant circulated through the coolant channel. The shape memory alloy that forms the liner will resist the onset of vibrations within the blade, thereby effectively damping blade vibrations. A method of fabricating a damped blade is also provided.
대표청구항▼
A damped blade is provided that includes a blade structural member defining at least one coolant channel and a liner formed of a shape memory alloy extending at least partially along the at least one coolant channel defined by the blade structural member. The shape memory alloy that forms the liner
A damped blade is provided that includes a blade structural member defining at least one coolant channel and a liner formed of a shape memory alloy extending at least partially along the at least one coolant channel defined by the blade structural member. The shape memory alloy that forms the liner is maintained generally at its transition temperature by means of coolant circulated through the coolant channel. The shape memory alloy that forms the liner will resist the onset of vibrations within the blade, thereby effectively damping blade vibrations. A method of fabricating a damped blade is also provided. in the inducer or impeller rotatable blades have a leading edge and said at least one diffuser slot inlet has a longitudinal center-line that intersects the flow channel at a point along the sidewalls, the distance from said point to the leading edge being up to 70% of the radial height of said impeller or inducer blades. 7. A device as in claim 1, wherein said at least one diffuser slot is sized so that the flow through said at least one diffuser slot is from about 1/2%-15% of an overall flow through said flow channel at the best operating point within the channel. 8. A device as in claim 1, wherein said at least one diffuser slot is positioned to capture a part-span vortex in the fluid thereby at least partially collapsing the vortex. 9. A device as in claim 1, wherein said at least one diffuser slot does not have a constant width. 10. A device as in claim 1, wherein the fluid flow is under a static pressure and said at least one diffuser slot is configured such that the static pressure in the fluid flow is sufficient to move the fluid flow from said at least one diffuser slot to said at least one passage. 11. A device as in claim 1, wherein said at least one diffuser slot is oriented so that it is no more than 65 degrees from radial with respect to said axis. 12. A device as in claim 1, wherein said at least one diffuser slot is oriented so that it is no more than 10 degrees from radial with respect to said axis. 13. A device as in claim 1, wherein said device includes at least two diffuser slots. 14. A device as in claim 13, wherein at least one of said diffuser slots is located adjacent a leading edge of the blades. 15. A device as in claim 13, wherein at least one of said diffuser slots is located adjacent the housing exit. 16. A device as in claim 13, wherein at least one of said diffuser slots is located adjacent the blades downstream of a leading edge of said blades. 17. A device as in claim 1, further comprising: a) a particle capture slot in fluid communication with said at least one diffuser slot; and b) a particle trap in fluid communication with said particle capture slot. 18. A device as in claim 1, wherein the device includes a means for maintaining or increasing the static pressure in the fluid flow as the fluid flow flows through the device. 19. A device as in claim 1, wherein the device includes a means for directing fluid from said at least one diffuser slot to multiple areas within or outside of the housing. 20. A device for at least partially stabilizing an unstable fluid flow within a flow channel, the device including an inducer or impeller residing at least partially within the flow channel, the inducer or impeller having rotatable blades for drawing the flow into, or being driven by the flow in, the flow channel, the inducer or impeller rotatable about an axis, the flow channel defined by interior sidewalls of a housing, the housing at least partially surrounded by an inlet plenum, the housing including an exit, said device comprising: a) at least one diffuser slot, said at least one diffuser slot including an inlet and an exit, said inlet in fluid communication with the flow channel, said at least one diffuser slot being substantially radial with respect to the axis; b) a re-entry slot in fluid communication with said at least one diffuser slot and the flow channel; and c) a return slot in fluid communication with said at least one diffuser slot and at least one of (i) the inlet plenum and (ii) the housing exit; wherein said at least one diffuser slot is free of vanes and said at least one diffuser slot has a width of about (0.05 to 0.50)×(the radial height of said impeller or inducer blades at said at least one diffuser slot inlet). 21. A device as in claim 20, wherein said at least one diffuser slot has a radius ratio greater than 1.03. 22. A device as in claim 20, wherein said at least one diffuser slot has a radius ratio of about 1.07 to about 2.00. 23. A device as in claim 19, whe rein the inducer or impeller rotatable blades have a leading edge and said at least one diffuser slot inlet has a longitudinal center-line that intersects the flow channel at a point along the sidewalls, the distance from said point to the leading edge being up to 70% of the radial height of said impeller or inducer blades. 24. A device as in claim 19, wherein said at least one diffuser slot is sized so that the flow through said at least one diffuser slot is from about 1/2%-15% of an overall flow through said flow channel at the best operating point within the channel. 25. A device for at least partially stabilizing an unstable fluid flow within a flow channel, the device including an inducer or impeller residing at least partially within the flow channel, the inducer or impeller having rotatable blades for drawing the flow into, or being driven by the flow in, the flow channel, the inducer or impeller rotatable about an axis, the flow channel defined by interior sidewalls of a housing, the housing at least partially surrounded by an inlet plenum, the housing including an exit, said device comprising: a) at least two diffuser slots, said at least two diffuser slots including an inlet and an exit, said inlet in fluid communication with the flow channel, said at least two diffuser slots being substantially radial with respect to the axis; and b) at least one passage in fluid communication with said exit of said at least two diffuser slots and; wherein said at least one passage is in fluid communication with at least one of the inlet plenum, the housing exit, an area downstream of the housing exit, and the flow channel and each of said at least two diffuser slots is free of vanes and each of said at least two diffuser slots has a radius ratio greater than 1.03. 26. A device as in claim 25, wherein said at least one diffuser slot has a radius ratio of about 1.07 to about 2.00. 27. A device for at least partially stabilizing an unstable fluid flow within a flow channel, the device including an inducer or impeller residing at least partially within the flow channel, the inducer or impeller having rotatable blades for drawing the flow into, or being driven by the flow in, the flow channel, the inducer or impeller rotatable about an axis, the flow channel defined by interior sidewalls of a housing, the housing at least partially surrounded by an inlet plenum, the housing including an exit, said device comprising: a) at least one diffuser slot, said at least one diffuser slot including an inlet and an exit, said inlet in fluid communication with the flow channel, said at least one diffuser slot being substantially radial with respect to the axis; and b) at least one passage in fluid communication with said exit of said at least one diffuser slot and said at least one passage in fluid communication with at least one of the inlet plenum, the housing exit, an area downstream of the housing exit, and the flow channel; wherein said at least one diffuser slot has a radius ratio greater than or equal to 1.03, at least one of said at least one diffuser slots is adjacent the housing exit, and said at least one diffuser slot is free of vanes. 28. A device as in claim 27, wherein said at least one passage adjacent the housing exit includes a return slot in fluid communication with the housing exit. 29. A device as in claim 27, wherein said at least one passage adjacent the housing exit is in fluid communication with the inlet plenum. 30. A device for at least partially stabilizing an unstable fluid flow within a flow channel, the device including an inducer or impeller residing at least partially within the flow channel, the inducer or impeller having rotatable blades for drawing the flow into, or being driven by the flow in, the flow channel, the inducer or impeller rotatable about an axis, the flow channel defined by interior sidewalls of a housing, the housing at least partially surrounded by an inlet plenum, the housing includi
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이 특허에 인용된 특허 (41)
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Nitzsche Fred,CAX ITX K1N 6A1 ; Grewal Anant,CAX ITX K1T 3P1 ; Zimcik David,CAX ITX K2L 2G5, Structural component having means for actively varying its stiffness to control vibrations.
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