Process and device for accelerating the destruction of at least two vortices in the wake of a moving body, particularly an aircraft
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0080407
(2002-02-25)
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우선권정보 |
FR-0002804 (2001-03-01) |
발명자
/ 주소 |
- Corjon, Alexandre
- Leweke, Thomas
- Laporte, Florent
|
출원인 / 주소 |
|
대리인 / 주소 |
Stevens, Davis, Miller & Mosher, LLP.
|
인용정보 |
피인용 횟수 :
5 인용 특허 :
10 |
초록
▼
A device for accelerating the destruction of contra-rotating vortices formed at the rear of wings of a moving body by the merging of at least two co-rotating eddies includes, on each of the wings, at least one perturbator which is positioned in the vicinity of the area of creation of one of the co-r
A device for accelerating the destruction of contra-rotating vortices formed at the rear of wings of a moving body by the merging of at least two co-rotating eddies includes, on each of the wings, at least one perturbator which is positioned in the vicinity of the area of creation of one of the co-rotating eddies associated with the wing. Each of the perturbators generates a periodic perturbation of the flow, which has a wavelength capable of exciting at least one of the instability modes of the corresponding eddy in such a way as to increase the core of the contra-rotating vortex which is created from this eddy, in such a way that the diameter of the core becomes greater than a predetermined proportion of the inter-vortex distance.
대표청구항
▼
A device for accelerating the destruction of contra-rotating vortices formed at the rear of wings of a moving body by the merging of at least two co-rotating eddies includes, on each of the wings, at least one perturbator which is positioned in the vicinity of the area of creation of one of the co-r
A device for accelerating the destruction of contra-rotating vortices formed at the rear of wings of a moving body by the merging of at least two co-rotating eddies includes, on each of the wings, at least one perturbator which is positioned in the vicinity of the area of creation of one of the co-rotating eddies associated with the wing. Each of the perturbators generates a periodic perturbation of the flow, which has a wavelength capable of exciting at least one of the instability modes of the corresponding eddy in such a way as to increase the core of the contra-rotating vortex which is created from this eddy, in such a way that the diameter of the core becomes greater than a predetermined proportion of the inter-vortex distance. ing a linear load (LKPrimNip) in the new winding nip by a corresponding displacement and tightening of the reeling drum; separating the material web by at least one separator device to form a new web leader; winding the new web leader onto the new reel spool; removing the old wound reel from the reeling drum, thereby opening the winding nip; and moving the new reel spool in a primary transport device while maintaining the new winding nip until the position of the new winding nip corresponds to the position where the winding nip was located. 2. The process in accordance with claim 1, wherein the material web comprises one of a paper or cardboard web. 3. The process in accordance with claim 1, wherein the moving of the new reel spool comprises moving the new reel spool over the reeling drum via the primary transport device until the new reel spool is taken over by the secondary transport device. 4. The process in accordance with claim 1, wherein the removing of the old wound reel comprises moving the old wound reel via the secondary transport device. 5. The process in accordance with claim 1, wherein during the joint displacement of the reeling drum and the old wound reel, the process further comprises adjusting, controlling, or regulating the linear load (LKSekNip) in the old winding nip by a corresponding displacement and tightening of the old wound reel. 6. The process in accordance with claim 1, wherein the reeling drum is acted on by a force (KTT) generating the linear load (LKSekNip), and the force (KTT) is greater than a force (KSekSchl) acting on the old wound reel and causes the joint displacement of the reeling drum and the old wound reel while maintaining the old winding nip. 7. The process in accordance with claim 1, wherein the old wound reel is acted on by a pressure system generating the linear load (LKSekNip) and the pressure system comprises at least two pressure units arranged such that each of the pressure units are acted on by a respective force (KSekSchl,KSekSchl-II) to generate the linear load (LKSekNip). 8. The process in accordance with claim 7, wherein the at least two pressure units are independent of one another. 9. The process in accordance with claim 7, wherein the old wound reel is acted on by a force (KSekSchl) generating the linear load (LKSekNip), and the force (KSekSchl) is smaller than a force (KTT) acting on the reeling drum and causes the joint displacement of the reeling drum and the old wound reel while maintaining the old winding nip. 10. The process in accordance with claim 7, wherein the old wound reel is acted on by a force (KSekSchl-II) generating the linear load (LKSekNip) and the force (KSekSchl-II) is smaller than a force (KTT) acting can the reeling drum and causes the joint displacement of the reeling drum and the old wound reel while maintaining the old winding nip. 11. The process in accordance with claim 7, wherein the diameter of the old wound reel increases during the joint displacement of the reeling drum and the old wound reel, while maintaining the old winding nip, is compensated for by a corresponding displacement of at least one pressure unit. 12. The process in accordance with claim 7, wherein the at least two pressure units comprises a first and second pressure unit, and wherein the old wound reel is supported by a displaceable movement device acted on by the second pressure unit in the secondary transport device, and the secondary transport device is acted on by the first pressure unit, and the old wound reel is acted on by the force (KSekSchl-II) during a main winding phase in which it is supported in the secondary transport device in a stationary manner. 13. The process in accordance with claim 1, wherein a force (KTT) acting on the reelin
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Cox Ronald A. (Norman OK), Concealable flap-actuated vortex generator.
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Thombi Layukallo JP, Control of flow separation and related phenomena on aerodynamic surfaces.
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Doria Iriarte JosJ. (Rodrguez Arias ; 61-10 48013 Bilbao (Vizcaya) ESX), Fairing for obtaining steady stabilization effects.
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Nosenchuck Daniel M. (Mercerville NJ) Brown Garry L. (Princeton NJ), Lifting body with reduced-strength trailing vortices.
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Wygnanski Israel (4559 N. Placita de las Charcras Tucson AZ 85718), Method and apparatus for delaying the separation of flow from a solid surface.
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Huenecke, Klaus, Method and apparatus for reducing trailing vortices in the wake of an aircraft.
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Ito Hideo (Hitachi JA) Tanaka Mizuho (Hitachi JA) Sato Harumasa (Hitachi JA), Object disposed in a fluid flow and having a selected configuration to minimize generation of Karman\s vortex street.
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Gilbert Raymond D. (6501 Inwood Dr. Springfield VA 22150), Segmented spoilers.
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Headley Jack W. (Rancho Palos Verdes CA) Skow Andrew M. (Hermosa Beach CA) Titiriga ; Jr. Andrew (Torrance CA), Shark nose for aircraft.
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Bilanin Alan J. ; Quackenbush Todd R., System and method of vortex wake control using vortex leveraging.
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Journade, Jerome, Method and device for reducing the induced speeds in vortices in the wake of an aircraft.
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Laporte, Florent; Hansen, Heinz, Method of controlling an aircraft in flight, especially to reduce wake vortices.
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Laporte, Florent; Hansen, Heinz, Method of controlling an aircraft in flight, especially to reduce wake vortices.
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Eaton, John K.; Matalanis, Claude, Translating active Gurney flap to alleviate aircraft wake vortex hazard.
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Loth,John L., Vorticity cancellation at trailing edge for induced drag elimination.
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