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특허 상세정보

Highly efficient supersonic laminar flow wing structure

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-030/00    B64C-007/00    B64C-009/18    B64C-003/10    B64C-009/24    B64C-001/26    B64C-003/14   
출원번호 US-0068773 (2011-05-18)
등록번호 US-9233755 (2016-01-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Haefliger, William W.
인용정보 피인용 횟수 : 0  인용 특허 : 16
초록

Improved supersonic laminar flow wing structure, on a supersonic aircraft, having strake extending forwardly of the wing inboard extent, and reversed fillet at strake junction with the wing leading edge. Plain and split flap structures may also be provided at each laminar flow wing.

대표
청구항

1. Improved supersonic laminar flow wing structure, on a supersonic aircraft, the wing structure characterized as forwardly sharp, and thin along its chordal extent, and having in combination the following: a) a fuselage,b) reversed fillet at fuselage junction with the wing leading edge, said reversed fillet having a forward edge defining a first edge portion angled forwardly toward the fuselage and a second edge portion angled rearwardly toward the fuselage. 2. Improved supersonic laminar flow wing structure as defined in claim 1 wherein said reversed f...

이 특허에 인용된 특허 (16)

  1. Walters Marvin M. (Lansdale PA) Kern Steven B. (Holland PA). Active vortex control for a high performance wing. USP1994025282591.
  2. Lucchesini, Massimo; Iaia, Pierclaudio. Aircraft configuration with improved aerodynamic performance. USP2009047520470.
  3. Morgenstern, John M.; Arslan, Alan. Aircraft lift device for low sonic boom. USP2005086935592.
  4. Tracy Richard R.. Aircraft wing and fuselage contours. USP2000116149101.
  5. Flaig Axel,DEX ; Schwetzler Detlev,DEX ; Stache ; deceased Ulrich,DEXITX by Ronald Seiler ; legal representative. Apparatus for influencing a wing root airflow in an aircraft. USP2000116152404.
  6. Borzachillo Angelo (Torrance CA). Auxiliary flaperon control for aircraft. USP1979034146200.
  7. Herrick Larry L. ; Bays-Muchmore C. Byram ; Hoffman Michael S. ; LeGrand Louis L. ; Ogg Steven S. ; Paul ; Jr. Bernard P. ; Visser Kenneth D. ; Wells Stephen L.. Blunt-leading-edge raked wingtips. USP2000076089502.
  8. Cole James B. (Mercer Island WA). Extendable aerodynamic fairing. USP1976073968946.
  9. Tracy Richard R. (3000 Old Ranch Rd. Carson City NV 89704). High efficiency, supersonic aircraft. USP1994065322242.
  10. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  11. Tracy Richard R.. High-efficiency, supersonic aircraft. USP1999045897076.
  12. Tracy Richard R. (3000 Old Ranch Rd. Carson City NV 89704). High-efficiency, supersonic aircraft. USP1996055518204.
  13. Rao Dhanvada M. (Yorktown VA). Lift augmentation for highly swept wing aircraft. USP1993105255881.
  14. Staudacher Werner (Zorneding DEX). Method for steering an aircraft. USP1981054267990.
  15. Skow Andrew (Rolling Hills Estates CA). Strakes for landing speed reduction. USP1993105249762.
  16. Rudolph Peter K. C. (Seattle WA). Vortex leading edge flap assembly for supersonic airplanes. USP1997105681013.