$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Rotationally stabilized guidable projectile and method for guiding the same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/06    F42B-010/26    F42B-010/14    F42B-010/54    F42B-010/64   
출원번호 US-0130635 (2012-06-26)
등록번호 US-9360286 (2016-06-07)
우선권정보 SE-1130064 (2011-07-07)
국제출원번호 PCT/SE2012/000098 (2012-06-26)
§371/§102 date 20140314 (20140314)
국제공개번호 WO2013/006106 (2013-01-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Polsinelli PC
인용정보 피인용 횟수 : 0  인용 특허 : 30
초록

The invention relates to a rotationally stabilized projectile (1) for launching from a barrel, which projectile (1) comprises a front projectile part (22), a rear projectile part (20) comprising a rotating band (4), and an intermediate projectile part (21) comprising a freely rotatable middle section (2) arranged with guide wings (3) for improving the gliding capability and guidance capability during the gliding phase and end phase of the projectile. The guide wings (3) are arranged extensibly on the freely rotatable middle section (2), and the intermedi...

대표
청구항

1. A rotationally stabilized projectile which is to be launched from a barrel, and wherein said projectile comprises a front projectile part,a rear projectile part-comprising a rotating band, andan intermediate projectile part comprising a freely rotatable middle section arranged with at least two radially extendable guide wings,wherein the guide wings are arranged extensibly on the freely rotatable middle section and are located in front of the rotating band, and wherein the intermediate projectile part also comprises a regulator device for regulating t...

이 특허에 인용된 특허 (30)

  1. Shai, Mordechai. Air vehicle and method for operating an air vehicle. USP2014118894003.
  2. Banks,Johnny E.; Baker,Brian C.. Apparatus and method for selectivity locking a fin assembly. USP2006087097132.
  3. Metz ; Pierre. Attitude-controlling system and a missile equipped with such a system. USP1978024076187.
  4. Blake, Jesse H.; Murphy, Matthew G.. Bang-bang control using tangentially mounted surfaces. USP2014088816261.
  5. Demarest, Joel; Verdier, Gilles. Centrifugally-cast tube and related method and apparatus for making same. USP2003116644358.
  6. Dunn Albert J. (Bangor ; Co. Down GB5). Control systems for moving bodies. USP1995025393012.
  7. Dunn Albert J. (Bangor GB5) Carson Oliver S. (Belfast GB5). Control systems for moving bodies. USP1995025393011.
  8. Ransom Richard S. (Craigavad ; Co. Down IEX). Control systems for moving bodies. USP1995065423497.
  9. Alford Robert L. (Excelsior MN) Rupert John G. (Mahtomedi MN). Electro-mechanical roll control apparatus and method. USP1995095452864.
  10. Elder, Douglas J.. Electromagnetic railgun projectile. USP2009057526988.
  11. Fraysse, Jr., John W.. Guided fuse with variable incidence panels. USP2011098026465.
  12. Hinsdale, Andrew J.; Dryer, Richard. Hybrid spin/fin stabilized projectile. USP2010127849800.
  13. Chung Sung K. (Dover NJ) Kline Roy W. (Newton NJ). Limited range projectile. USP1995125476045.
  14. Rönn, Torsten; Pettersson, Thomas; Heiche, Ulf. Method of increasing the range of a subcalibre shell and subcalibre shells with a long range. USP2012018097838.
  15. Giesenberg, Peter Joachim Wilhelm; Jakob, Otto-Paul. Missile. USP2003056557798.
  16. Kranz Walter (Taufkirchen DEX). Missile having rotor ring. USP1990104964593.
  17. Ransom, Richard Sutton. Missile system and method of missile guidance. USP2004126832740.
  18. Fieuzal Jean Henri (Rueil Malmaison FR) Bourgine Louis Gaston (Chambourcy FR) Jean Andre Camille (Conflans Sainte Honorine FR) Benzoni Rene Pierre (Paris FR). Missile with cruciform guidance system. USP1976083976266.
  19. Geswender, Chris Eugene; Harline, Shawn Brent; Blaha, George A.. Missile with odd symmetry tail fins. USP2005036869044.
  20. Grosso Vincent A. (Hopkinton MA). Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same. USP1995015379968.
  21. Deckard, Dennis D.; Mulinix, David J.; Stark, Douglas E.. One-piece wrap around fin. USP2004016672537.
  22. Lardellier Alain ; M. J. (Melun FRX) Saillot Patrick W. R. (Vaux le Penil FRX). Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft. USP1993015181675.
  23. Lamorlette,G챕rard. Process to control the trajectory of a spinning projectile. USP2006097105790.
  24. Peller Helmut (Dsseldorf DEX) Schilling Hartmut (Kaarst DEX) Becker Hanjoerg (Dsseldorf DEX) Glotz Gerhard (Dsseldorf DEX). Projectile with rotatable stabilizing device. USP1990024903917.
  25. James M. Garner ; James M. Bender ; Peter Dehmer ; Melissa Klusewitz. Protective device for deployable fins of artillery projectiles. USP2002086435097.
  26. Cole Donald E. (Covina CA). Rolling airframe autopilot. USP1977104054254.
  27. Klestadt Ralph H. (Sherman Oaks CA). Rotationally mounted flexible band wing. USP1995055417393.
  28. Stoy David R. (Woodland Hills CA). Separately banking maneuvering aerodynamic control surfaces, system and method. USP1994065322243.
  29. Kusic, Tom. Spiralling missile--A. USP2003116644587.
  30. Bittle David A.. Wing deployer and locker. USP2001026186442.