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특허 상세정보

Anti-icing piccolo tube standoff

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/02   
미국특허분류(USC) 244/134B; 244/134R
출원번호 US-0354557 (2009-01-15)
등록번호 US-8100364 (2012-01-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lathrop & Gage LLP
인용정보 피인용 횟수 : 3  인용 특허 : 21

A standoff structure for an anti-icing piccolo tube wherein a flexible structure is formed from support ribs, a support bar and a diverter bar for supporting the piccolo tube within the slat or other aircraft leading edge, and for diverting hot gas from the piccolo tube across the inner surface of the slat or other aircraft leading edge.


1. A standoff structure for supporting an anti-icing piccolo tube in a leading edge of an aircraft structure comprising: a plurality of flexible support ribs disposed substantially parallel to each other;a support bar and a diverter bar disposed substantially parallel to each other;wherein the support bar and the diverter bar are disposed substantially perpendicular to and in connection with the plurality of support ribs; wherein the plurality of support ribs, the support bar and diverter bar are formed from a continuous sheet of flexible material. 2. Th...

이 특허에 인용된 특허 (21)

  1. Paul Laugt FR. Aircraft airfoil leading edge member equipped with a de-icing device. USP2002106467730.
  2. Cook Leonard J. (Canoga Park CA) Rosenthal Herman A. (San Diego CA). Aircraft anti-icing plenum. USP1976013933327.
  3. DuPont, Henry Morgan. Airfoil anti-icing assembly and method. USP2004036702233.
  4. Swanson ; Everts W. ; Wehrman ; Marvin D.. Boundary layer control system for aircraft. USP1978074099691.
  5. Parente Charles A.. Combined acoustic and anti-ice engine inlet liner. USP1998115841079.
  6. Rauckhorst ; III Richard L. (North Canton OH). Compressible nose dynamic de-icer. USP1994055314145.
  7. Adams Lowell J. (Dayton OH). Deicer assembly utilizing shaped memory metals. USP1996095558304.
  8. Pike Walter E. ; Shafer Jan C.. Double-walled duct assembly for aircraft anti-icing conduit systems. USP1999126003814.
  9. Lardiere ; Jr. Benjamin G. (Milford CT) Goldberg Joshua I. (Woodbridge CT). Electro-expulsive separation apparatus. USP1990014894569.
  10. Al-Khalil, Kamel. Energy-efficient electro-thermal and electro-mechanical ice-protection method. USP2010127854412.
  11. Al-Khalil, Kamel. Energy-efficient electro-thermal ice-protection system. USP2010057708227.
  12. Manda Leo J. (Florissant MO) Lavorando Michael J. (Chesterfield MO). Energy-exchange system incorporating small-diameter tubes. USP1993075228643.
  13. Lardiere ; Jr. Benjamin G. (Milford CT) Goldberg Joshua I. (Woodbridge CT). Expulsive separation apparatus. USP1991014982121.
  14. Porte Alain,FRX. Hot air diffuser for a jet engine air inlet cowl with de-icing circuit. USP2000066079670.
  15. Goldberg Joshua I. (Woodbridge CT). Method of building an expulsive blanket using composite materials and stitched attachment. USP1996075531405.
  16. Kawabe Shun,JPX ; Sato Keiichi,JPX ; Yamashita Daiya,JPX ; Nakayama Haruo,JPX ; Shiraishi Koji,JPX ; Matsumoto Keizo,JPX. Method of maufacturing a leading edge structure for aircraft. USP1998095807454.
  17. Shatz Solomon (P.O. Box 523 Cupertino CA 94015). Movable sheet for laminar flow and deicing. USP1997015590854.
  18. Sternberger, Joe E.. Nacelle inlet thermal anti-icing spray duct support system. USP2011037900872.
  19. Leffel Kevin L. (Akron OH) Rauckhorst ; III Richard L. (North Canton OH). Side flex leading edge ice protector. USP1996025489073.
  20. McLaren Douglas (Seattle WA) Orr William W. (Mercer Island WA). Thermal anti-icing system for aircraft. USP1991045011098.
  21. McArdel Richard C. (Kirkland WA). Wing slat anti-ice air duct system with improved slide bearings and air seal. USP1986084603824.