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특허 상세정보

Sealing assembly for reducing gaps between movable control surfaces of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/06   
미국특허분류(USC) 244/131 ; 244/133 ; 342/04
출원번호 US-0074637 (1993-06-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Schruhl
인용정보 피인용 횟수 : 15  인용 특허 : 0
초록

The invention is a sealing assembly for reducing the gap between an aircraft's movable flight control member and adjacent structure thereto, the flight control member and structure having external surfaces and side surfaces facing each other. In detail, the assembly includes first and second flexible bulb seals mounted on the periphery of the side surface of both the flight control member and the adjacent structure forming an extension of the external surface of both. Each of the bulb seals includes a compressible foam bulk absorber core; the core having...

대표
청구항

[ We claim:] [1.] A sealing assembly for reducing the gap between an aircraft's movable flight control member and adjacent structure thereto, the flight control member and structure having external surfaces and side surfaces facing each other, the assembly comprising first and second flexible bulb seals mounted on the periphery of the side surface of both the flight control member and the adjacent structure forming an extension of the external surface of both, each of said bulb seals comprising:a compressible foam bulk absorber core; said core having a b...

이 특허를 인용한 특허 피인용횟수: 15

  1. Stenzel, Volkmar; Kaune, Martin; Lohner, Hubertus; Schramm, Ottmar. Aircraft landing flap. USP2017079694901.
  2. Neal, Matthew A.; Smith, Charles R.. Dynamic conformal aerodynamic seal (CAS) for aircraft control surfaces. USP20180710017239.
  3. Merlo, Emanuele; Brenna, Fabio. Equipment for the reduction of the radar marking for aircrafts. USP2016069362626.
  4. Poppe, Bernd; Auhagen, Kurt. Flap interconnection system for aircraft. USP2009067546984.
  5. Schlipf, Bernhard; Hue, Xavier. High lift component for an aircraft, high lift system, method for adjusting the high lift characteristics of an aircraft and aircraft. USP2017029567064.
  6. Luippold, David Arthur; Brown, Mark David; Tully, John Wilbur. Highly conductive thermoplastic elastomer (TPE) gap filler. USP2004086780921.
  7. Geders Paul Francis ; Wille Robert Henry. Interface seal for an aircraft. USP2000076092764.
  8. Luippold David Arthur ; Brown Mark David ; Tully John Wilbur. Method for reducing reflected radio frequency electromagnetic radiation. USP2001096284175.
  9. Woldanski Greg L.. Normal incidence multi-layer elastomeric radar absorber. USP2001056224982.
  10. Woldanski Greg L.. Process for making a low density foam filled reticulated absorber by means of vacuum. USP2001056231794.
  11. Hodkisson, Mark; Wilson, James; Evans, Samuel. Retractable infill panel for high-lift device. USP2016029254927.
  12. Martin Hernandez, Agustín Mariano. Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser. USP2010127850119.
  13. Conway, Jr., George Louis; Young, Kendall G.; Stroud, Ron L.. Single aperture conformal aircraft bays. USP2003036536711.
  14. Carlson Marvin Lee. Transmission line electromagnetic reflection reduction treatment. USP2001026184815.
  15. Dyckrup, Werner. Wing for an aircraft. USP2015018931733.