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특허 상세정보

Tip fence for reduction of lift-generated airframe noise

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/58    B64C-009/00   
미국특허분류(USC) 244/01N ; 244/091 ; 244/199 ; 244/213
출원번호 US-0482459 (1995-06-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Warsh
인용정보 피인용 횟수 : 19  인용 특허 : 10
초록

In addition to reducing airframe noise, the tip fence tends to decrease drag and to increase lift, thus improving the overall aerodynamic performance of the aircraft. Another advantage presented by the tip fence lies in the simplicity of its design, its elegance, and its ready ability to fit on the wing components, such as the flaps and the slats. Furthermore, it does not require non-standard materials or fabrication techniques, and it can be readily, easily and inexpensively retrofited on most of the existing aircraft, with minimal design changes.

대표
청구항

[ What is claimed is:] [1.] An aircraft wing comprising in combination:a high-lift system formed of a plurality of flaps, at least some of which having an outboard tip and an inboard tip; anda lift-generated noise reduction tip fence secured to at least one of said outboard tip and inboard tip of at least one of said flaps, and said tip fence moving with said at least one of said flaps, for reducing airframe aerodynamic noise generated at said one of said outboard tip and inboard tip.

이 특허를 인용한 특허 피인용횟수: 19

  1. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Aircraft. USP201008D622653.
  2. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Aircraft configuration. USP2011098016233.
  3. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.; Lan, Justin. Aircraft configuration. USP2014018628040.
  4. Trichês, Jr., Mário; Valle do Carmo, Micael Gianini; Caldeira da Silva, Bruno Arantes; Franca Barboza, Marcus Vinicius; Losada Gouveia, Vinicius. Aircraft provided with aerodynamic seal for reduction of noise generated by aircraft control surfaces. USP2014028657236.
  5. Jeffrey W. Moe. Aircraft wing and method for reducing airframe-generated noise. USP2002096454219.
  6. Wright, Philip; Kay, Edmund. Aircraft wing with slotted high lift system. USP2016119481447.
  7. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Airplane configuration. USP2012018087607.
  8. Larssen, Jon V.; Calkins, Frederick T.. Deployable flap edge fence. USP2010077753316.
  9. Larssen, Jon V.; Calkins, Frederick T.. Deployable flap edge fence. USP2013068469315.
  10. Ferrari, Marcello do Areal Souto. Devices and methods to improve wing aerodynamics at low airspeeds. USP2012028118265.
  11. Bielek, Craig Allen. Gas turbine nozzle with a flow fence. USP2015028944774.
  12. Bielek, Craig Allen. Gas turbine nozzle with a flow groove. USP2015069062554.
  13. Isotani, Kazuhide; Hayama, Kenji. High-lift device of air vehicle. USP2017079714079.
  14. Isotani, Kazuhide; Hayama, Kenji. High-lift device of air vehicle. USP2017109789955.
  15. Hirai, Makoto; Takenaka, Keizo; Imamura, Taro; Yamamoto, Kazuomi; Yokokawa, Yuzuru. High-lift-device, wing, and noise reduction device for high-lift-device. USP2016099440729.
  16. Hieu T. Ngo ; Lisa E. Barlow. Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith. USP2002056394397.
  17. Isotani, Kazuhide; Hayama, Kenji; Kumada, Toshiyuki; Ono, Masaru. Method of attenuating noise in aircraft landing gear and structure. USP2016059327829.
  18. Konings, Christopher A.. Nacelle chine installation for drag reduction. USP2005116964397.
  19. Winter, Michael. Systems and methods for altering inlet airflow of gas turbine engines. USP2015109169779.