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특허 상세정보

Pylon for suspending a turboengine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/00   
미국특허분류(USC) 244/198;
출원번호 US-0426805 (2009-04-20)
등록번호 US-8146868 (2012-04-03)
우선권정보 FR-08 02211 (2008-04-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Dickinson Wright PLLC
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

Disclosed is a mast for the suspension of a bypass turbine engine beneath a wing of an aircraft in which the wing has at least one flap. The mast includes a rear fairing that protrudes rearward of a trailing edge of the wing and is mounted so as to tilt in a deployed downward position as the flap is deployed in a downward position. The rear fairing is positioned to enter a cold flow of the turbine engine, when deployed in the downward position. The rear fairing further supports at least one aerodynamic element that generates vortices that reduce, if not ...

대표
청구항

1. A mast for the suspension of a bypass turbine engine beneath a wing of an aircraft, said wing being furnished with at least one flap and said mast comprising a rear fairing which protrudes rearward relative to a trailing edge of said wing and which is mounted so as to tilt in a deployed downward position as said flap is deployed in a downward position, said rear fairing entering a cold flow of said turbine engine when in the deployed position, and is subjected to vibrations, wherein said rear fairing supports at least one aerodynamic element that gene...

이 특허에 인용된 특허 (13)

  1. Lam Lawrence Y. ; Lam Michael. Aileron for fixed wing aircraft. USP2000066079672.
  2. Johnstone Edmund H. (82 Salzburg Blvd. Apt. G Columbus IN 47201). Aircraft wing vortex deflector. USP1976083974986.
  3. Jones, Kelly T.. Apparatus and methods for actuating rotatable members. USP2004036698688.
  4. Bliesner Wayne T. (Snohomish WA). Contoured wing/flap assembly and method. USP1993015178348.
  5. Atinault, Olivier. Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface. USP2011017866608.
  6. Sankrithi Mithra M. K. V. (417 Bellevue Way SE. #400 Bellevue WA 98004). Flexible flap for an airfoil. USP1984074460138.
  7. Munoz Saiz Manuel,ESXITX 28017. Flight controls with automatic balance. USP2000086109567.
  8. Wheeler Gary O. (2715 185th Ave. E. Sumner WA 98390). Low drag vortex generators. USP1991105058837.
  9. Ingo Borchers DE; Roger Drobietz DE; Michael Gruenewald DE; Knut Mau DE; Johann Reichenberger DE. Noise reducing vortex generators on aircraft wing control surfaces. USP2002126491260.
  10. Vijgen Paul M. H. W. (Hampton VA) Howard Floyd G. (Hampton VA) Bushnell Dennis M. (Wicomico VA) Holmes Bruce J. (Newport News VA). Serrated trailing edges for improving lift and drag characteristics of lifting surfaces. USP1992025088665.
  11. Boyd, James A.. Trailing edge device for an airfoil. USP1985094542868.
  12. Stephenson Martin F. (Issaquah WA). Wing trailing edge flap mechanism. USP1991024995575.
  13. Perez Sanchez,Juan. Wing with extendable aerodynamic pivoted flaps. USP2009037510151.