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특허 상세정보

Adhesive panels of microvane arrays for reducing effects of wingtip vortices

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06    B64C-021/10   
출원번호 US-0569270 (2014-12-12)
등록번호 US-9868516 (2018-01-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Baker Botts L.L.P.
인용정보 피인용 횟수 : 2  인용 특허 : 16
초록

In one embodiment, a wing includes a low pressure side, a high pressure side opposite the low pressure side, and a drag reducing apparatus coupled to the low pressure using an adhesive. The drag reducing apparatus includes a first side coupled to the low pressure side of the wing, and a second side opposite the first side, the second side comprising a plurality of vortex generators arranged in an array configuration, the array configuration of vortex generators operable to weaken a wingtip vortex generated by the wing by generating one or more vane vorti...

대표
청구항

1. A wing, comprising: a low pressure side and a high pressure side opposite the low pressure side, wherein the low pressure side and high pressure side are configured, when air flows over the wing, to generate a force on the high pressure side; anda drag reducing apparatus coupled to the low pressure side of the wing using an adhesive, the drag reducing apparatus comprising: a first side coupled to the low pressure side of the wing;a second side opposite the first side, the second side comprising a plurality of vortex generators arranged in a plurality ...

이 특허에 인용된 특허 (16)

  1. Schenk Karl M. (Wichita KS) Reynolds Peter T. (Wichita KS) Abla M. H. (Wichita KS) Wattson ; Jr. Robert K. (Wichita KS). Airstream modification device for airfoils. USP1982104354648.
  2. Ireland, Peter. Application of elastomeric vortex generators. USP2014108870124.
  3. Lisy, Frederick J.; Modarreszadah, Mohammed; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.; Prince, Troy. Flow control device and method of controlling flow. USP2005016837465.
  4. Lisy,Frederick J.; Modarreszadah,Mohammed; Patel,Mehul P.; DiCocco,Jack M.; Carver,Reed; Schmidt,Robert N.; Prince,Troy. Flow control device and method of controlling flow. USP2008027334760.
  5. Williams John E. F. (Cambridge GB2) Lang Jack (Cambridge GB2). Low drag surface construction. USP1987094693201.
  6. Wheeler Gary O. (2715 185th Ave. E. Sumner WA 98390). Low drag vortex generators. USP1991105058837.
  7. Miller, Daniel N.; McCallum, Brent N.; Jenkins, Stewart A.; Wells, David M.. Method and system for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation. USP2012088240616.
  8. Smith, Brian R.; Maines, Brant H.; Ma, Edward C.; DiGirolamo, Edward A.; Yagle, Patrick J.. Microvanes for aircraft aft body drag reduction. USP2012078226038.
  9. Miller, Daniel N.; Baruzzini, Dan J.. Prismatic-shaped vortex generators. USP2012078210482.
  10. Fox, Bruce R.; Fox, Stephen J.. Retractable vortex generator for reducing stall speed. USP2014028657238.
  11. Rawlings, Diane C.; McLean, Jr., James D.; Mathews, Mary J.. Structurally designed aerodynamic riblets. USP2013048413928.
  12. Smith Robert A. (Ridgecrest CA) Gutmark Ephraim (Ridgecrest CA) Schadow Klaus C. (Ridgecrest CA) Wilson Kenneth J. (Ridgecrest CA). Suppressor of oscillations in airframe cavities. USP1994085340054.
  13. Miller, Daniel N.; McCallum, Brent N.; Jenkins, Stewart A.; Wells, David M.. System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation. USP2013018353482.
  14. Essenhigh, Katherine Anne; Tao, Fengfeng; Bennett, Grover Andrew; Boespflug, Matthew; Murray, Robert C.; Saddoughi, Seyed Gholani. System, apparatus, program product, and related methods for providing boundary layer flow control. USP2013098523115.
  15. Babinsky, Holger; Loth, Eric; Lee, Sang. Vortex generators to control boundary layer interactions. USP2014028656957.
  16. Choi,Haecheon; Choi,Jin; Lee,Dongkon; Kim,Jeonglae; Jeon,Woo Pyung; Hahn,Seonghyeon; Kim,Jinsung. Wake disturbing apparatus and method for reducing drag. USP2006097100969.