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특허 상세정보

Stabilizer with structural box and sacrificial surfaces

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/00    B64C-005/02    B64D-027/14    B64C-005/06    B64C-009/02    B64C-019/00    B64D-033/04    F02K-001/56    F02K-001/78    B64C-001/26   
출원번호 US-0440995 (2013-10-17)
등록번호 US-9884674 (2018-02-06)
국제출원번호 PCT/US2013/065417 (2013-10-17)
국제공개번호 WO2014/078006 (2014-05-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 21
초록

An aircraft includes a tail extending from a fuselage. The tail defines a structural box having first and second vertical stabilizers that support a horizontal stabilizer. The tail includes at least one sacrificial control surface and at least one primary control surface. The primary control surfaces maintain aircraft controllability in the event that the sacrificial control surface becomes inoperable.

대표
청구항

1. An aircraft comprising; a fuselage; anda tail extending from the fuselage, the tail defining a structural box having first and second vertical stabilizers and a horizontal stabilizer supported atop the first and second vertical stabilizers, the tail including at least one sacrificial control surface and at least one primary control surface, the at least one sacrificial control surface including a defined frangible connection along which the sacrificial control surface breaks away from the tail responsive to a strike from debris, wherein the primary co...

이 특허에 인용된 특허 (21)

  1. Llamas Sandin, Raul Carlos. Aircraft having a lambda-box wing configuration. USP2012058186617.
  2. Brand, Joseph Horace; Dooley, Kevin; Dowhan, Michael; Youssef, Nashed; Harvey, Richard; Savage, William. Aircraft propulsion system. USP2009067540450.
  3. Krojer Hubert (Bermatingen DEX). Aircraft propulsion system arrangement. USP1985024500055.
  4. Franklin, III, Walter M.; Morgenstern, John M.; Lee, Howard; Quayle, Brian; Hajic, Ken; Scarcello, John; Arslan, Alan E.. Aircraft tail configuration for sonic boom reduction. USP2004116824092.
  5. Gilbert Raymond D. (6501 Inwood Dr. Springfield VA 22150). Aircraft tail surface spoilers. USP1995085445346.
  6. Larson Robert J. (Seattle WA 4). Aircraft vertical fin-fuselage structural integration system. USP1984054448372.
  7. Speelman ; III Ralph J. (Dayton OH). Aircraft windshield system with frangible panel for aircrew emergency escape. USP1994035289996.
  8. Ward, Michael David. Aircraft wings and fuel tanks. USP2009107600717.
  9. Sprenger Wilfried,DEX. Aircraft with a double-T tail assembly. USP2001086273363.
  10. Sigalla Armand (Bellevue WA). Airplane all-moving airfoil with moment reducing apex. USP1981094291853.
  11. Payen, Hervé. Composite anti-crash structure with controlled buckling for an aircraft. USP2010087780116.
  12. El Hamel,Karim; Newton,Arnold C. Engine arrangement. USP2006097107755.
  13. Provost, Michael J. Engine arrangement. USP2003046543718.
  14. Kress Robert W. (Saugerties NY). Four engine VTOL aircraft. USP1992075131605.
  15. Babu, Michael; Domonkos, Richard E.; Shacter, Philip. Gas turbine engine with dual fans driven about a central core axis. USP2011098015796.
  16. Lion Charles E. (253 Euclid Ave. Ridgway PA 15853). Reduced noise monolithic wing-stabilizer aircraft. USP1984054447022.
  17. Zauber, Vonn A.; Gentry, Steven M.. Rugged, removable, electronic device. USP2010087775834.
  18. Saito, Yoshio; Endo, Masanori; Matsuda, Yukio; Sugiyama, Nanahisa; Tagashira, Takeshi. Separated core engine type turbofan engine. USP2004096792746.
  19. Gagliano Christopher ; Boadman Thomas E.. Stabilizer fins-inverted for aircraft. USP1999115979824.
  20. Zimmermann Vincent H. (Olivette MO) DEGarcia ; Jr. Horacio J. (Maryland Heights MO) Pierson Harlan K. (Hazelwood MO). Trifan powered VSTOL aircraft. USP1976083972490.
  21. Guering, Bernard; Teulou, Olivier. Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft. USP2012058167239.