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특허 상세정보

Multi-caliber fuze kit and methods for same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/003.24; 102/385
출원번호 US-0469443 (2009-05-20)
등록번호 US-8513581 (2013-08-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Schwegman Lundberg & Woessner, P.A.
인용정보 피인용 횟수 : 2  인용 특허 : 23
초록

A multi-caliber fuze kit includes a fuze housing configured for coupling with multiple projectiles. One or more canards are moveably coupled with the fuze housing. The one or more canards are adjustable between two or more canard configurations. In a first canard configuration, the one or more canards are at a first canard angle relative to a bore sight of the fuze housing, and the first canard angle is configured for use with a first projectile. In a second canard configuration, the one or more canards are at a second canard angle relative to the bore s...

대표
청구항

1. A multi-caliber fuze kit for use with projectiles comprising: a fuze housing configured for coupling with multiple projectiles; andone or more canards moveably coupled with the fuze housing, the one or more canards moveable to two or more canard configurations, wherein: a first canard configuration is at a first canard angle relative to a bore sight of the fuze housing, and the first canard includes a first canard shape in the first canard configuration, the first canard angle and the first canard shape are configured for use with a first projectile, ...

이 특허에 인용된 특허 (23)

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard. 2-D projectile trajectory correction system and method. USP2007017163176.
  2. Rupert, John G.; Siewart, Jeff. 2-D projectile trajectory corrector. USP2003016502786.
  3. Rupert, John G.; Siewart, Jeff. 2-D projectile trajectory corrector. USP2003126666402.
  4. Kusic,Tom. Aircraft spiralling mechanism-B. USP2007017165742.
  5. Sebestyen George (Weston MA) Sinclair Ronald R. (Moultonboro NH) Smith John A. (Bedford MA) Sands Timothy B. (Acton MA) Nussdorfer Theodore J. (Lexington MA). Canard control assembly for a projectile. USP1985044512537.
  6. Pellegri, Mauro; Schino, Angelo. Control group for directional fins on missiles and/or shells. USP2003086604705.
  7. Washington William D. (Arab AL) Killough Thomas L. (Huntsville AL) Booth Pamela F. (Huntsville AL) Walker Billy J. (Madison AL). Curved grid fin. USP1991095048773.
  8. Mikhail Ameer G. (Bel Air MD). Detached and attached thermal spoilers for kinetic energy projectile fins. USP1991115062585.
  9. Field,John. Fin attachment system. USP2007047198532.
  10. Clancy,John A.; Bybee,Thomas D.; Friedrich,William A.. Fixed canard 2-D guidance of artillery projectiles. USP2006016981672.
  11. Geswender, Chris E.; Zamora, Matthew A.; Sanchez, Cesar. Fuze guidance system with multiple caliber capability. USP2012068203108.
  12. Abbott Anthony Steven. GPS guided munition. USP2001056237496.
  13. Fraysse, Jr., John W.. Guided fuse with variable incidence panels. USP2011098026465.
  14. Leininger,J체rgen. Method for correcting the flight path of ballistically fired spin-stabilised artillery ammunition. USP2007097267298.
  15. Geswender, Chris E.; Bennett, Stephen E.. Methods and apparatus for guidance of ordnance delivery device. USP2012028124921.
  16. Ishimitsu Kichio K. (Mercer Island WA). Minimum drag wing configuration for aircraft operating at transonic speeds. USP1980064205810.
  17. Janik, Richard; Dryer, Richard. Multi-mode modular projectile. USP2011037905182.
  18. Dasa Madhava (P.O. Box 461 Kula HI 96790-0461). Multiple configuration model aircraft. USP1991045007875.
  19. Driver, Franklin Thomas. Pressurized bladder canister for installation of cured in place pipe. USP2005116969216.
  20. Morris,Joseph P.; Smith,Douglas L.. Projectile trajectory control system. USP2008047354017.
  21. Buckland Roy W. (Croydon GB2). Spin-damped training round with selectable safety trace. USP1990034905602.
  22. Bär, Klaus; Kautzsch, Karl. Spin-stabilized correctible-trajectory artillery shell. USP2009097584922.
  23. Thomas Larry James. Universal warhead adapter, and missile and method incorporating same. USP2001056227096.