• 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

Munition guidance system and method of assembling the same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/20    F41G-007/22    F42B-015/01    F42B-033/00    F41G-007/00    F42B-015/00   
출원번호 US-0233761 (2012-07-18)
등록번호 US-9157702 (2015-10-13)
우선권정보 IL-214191 (2011-07-19)
국제출원번호 PCT/IL2012/050255 (2012-07-18)
§371/§102 date 20140120 (20140120)
국제공개번호 WO2013/011510 (2013-01-24)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 21

A munition guidance system is disclosed. The system comprises a generally tubular enclosure, having an internal cavity adapted for receiving a munition, wherein an outer diameter of the enclosure is at most the largest outer diameter of the munition; and a processing and control unit enclosed within the enclosure and being configured for controlling guidance wings so as to maneuver the munition while flying.


1. A munition guidance system, comprising: a generally tubular enclosure, having an internal cavity adapted for receiving a munition, wherein an outer diameter of said enclosure is at most the largest outer diameter of said munition;a plurality of guidance wings enclosed within said enclosure and configured for being erected outwardly from said enclosure;a target identification unit for identifying a target; anda processing and control unit enclosed within said enclosure and being configured for erecting said wings based on at least one criterion, and fo...

이 특허에 인용된 특허 (21)

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard. 2-D projectile trajectory correction system and method. USP2007017163176.
  2. Brieseck Bernd (Henfenfeld DEX) Nagler Josef (Rothenbach/Pegn. DEX). Airborne body with over-caliber sized guidance mechanism. USP1988034728058.
  3. Schroppel Werner (Wendelstein DEX) Leidenberger Thomas (Nurnberg DEX). Arrangement for the unlatching and extension of the stabilizing fins of a projectile. USP1992055114095.
  4. Buckland, Roy William; Smith, Stephen George Gladwell. Control of projectiles or the like. USP2014038674278.
  5. Perry, Craig; Schroeder, Richard W.; Voigt, Allan A.. Cover ejection and fin deployment system for a gun-launched projectile. USP2005046880780.
  6. Goulding Kenneth (Stevenage GB2). Deployment and actuation mechanisms. USP1987124709877.
  7. Dodu,Ren?; Dion,Dominique. Deployment and drive device for projectile control surfaces. USP2007027175131.
  8. Okada,Shinichi; Okawa,Sadao; Shinomiya,Masato; Mochizuki,Makoto. Flying body for firing from a tube with over-caliber stabilizers. USP2006027004425.
  9. Manole, Leon R.; Logsdon, Jr., Ernest L.; Palathingal, Mohan J.; Sebasto, Anthony J.. Gun launched hybrid projectile. USP2012028115149.
  10. Voigt Allan A. ; Speicher John M.. Integrated missile fin deployment system. USP2000066073880.
  11. Geis Norman P. (Kensington NH) Chambers Edward A. (Acton MA). Mortar system with improved round. USP1985084533094.
  12. Zemany, Paul D.; Carlson, Mark A.; Maynard, John A.. Optically guided munition. USP2009057533849.
  13. Arnaud Philippe (Orleans la Source FRX) Bernard Marc (Marcilly en Villette FRX) Boubault Herv (Olivet FRX) Thouron Ren (La Ferte St Aubin FRX). Peripheral casing for a guided munition fired with a cannon effect. USP1992045103734.
  14. Kuhnle Joachim,DEX ; Heitmann Thomas,DEX ; Niemeyer Torsten,DEX ; Arendt Norbert,DEX. Projectile to be fired from a weapon barrel and stabilized by a guide assembly. USP2001116314886.
  15. Craig W. Dale (King George VA). Retainer/release mechanism for use on fin stabilized gun fired projectiles. USP1979114175720.
  16. Martinez, Marcelo Edgardo. Rolling projectile with extending and retracting canards. USP2012118319164.
  17. Woodland Richard L. K.,CAXITX V8Z 6N2. Sonotube compatible unmanned aerial vehicle and system. USP2000056056237.
  18. Jeffrey C. Callahan. Submarine horizontal launch tactom capsule. USP2002086427574.
  19. Palmer Miles R.. Transformable gun launched aero vehicle. USP2001076260797.
  20. Thomas Larry James. Universal warhead adapter, and missile and method incorporating same. USP2001056227096.
  21. Hppner Heinz-Jochen (Bremen DEX) Sgarz Hugo (Bremen-Lesum DEX) Sadowski Herbert (Delmenhorst DEX). Unmanned aircraft. USP1984094471923.