$\require{mediawiki-texvc}$
  • 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

Mortar round glide kit

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/00    F42B-010/38   
미국특허분류(USC) 244/003.25; 102/384
출원번호 US-0806742 (2010-08-19)
등록번호 US-8237096 (2012-08-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Knobbe Martens Olson & Bear LLP
인용정보 피인용 횟수 : 2  인용 특허 : 16
초록

Apparatus and methods provide a kit for converting a conventional mortar round into a glide bomb. Mortar rounds are readily available to combat personnel and are small and light enough to be carried by relatively small unmanned aerial vehicles (UAVs) such as the RQ-7 Shadow. Advantageously, the kit provides both guidance and relatively good standoff range for the UAV such that the kit-equipped mortar round can be dropped a safe distance away from the intended target so that the UAV is not easily observed near the intended target.

대표
청구항

1. An apparatus comprising a kit for equipping a mortar round with the ability to glide when dropped from altitude, the apparatus comprising: a housing configured to be attached to a rear portion of a mortar round;a threaded joint configured to attach the housing to a rear portion of a mortar round, wherein the threaded joint is configured to engage with threads of a mortar round originally intended to engage with a tail section;at least one wing configured to provide lift and two or more movable control surfaces configured to permit flight control, wher...

이 특허에 인용된 특허 (16)

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard. 2-D projectile trajectory correction system and method. USP2007017163176.
  2. Nowakowski Michael V. (Los Angeles CA). Autonomous precision weapon delivery using synthetic array radar. USP1993115260709.
  3. Clancy,John A.; Bybee,Thomas D.; Friedrich,William A.. Fixed canard 2-D guidance of artillery projectiles. USP2006016981672.
  4. Abbott Anthony Steven. GPS guided munition. USP2001056237496.
  5. Abbott Anthony Steven. GPS guided munition. USP1999085943009.
  6. Yaacov Frucht IL. Method and system for guiding submunitions. USP2002116481666.
  7. McKendree,Thomas L.; Britigan,John D.; Habereder,Hans L.. Munition with integrity gated go/no-go decision. USP2008057367525.
  8. McKendree,Thomas L.; Britigan,John D.; Habereder,Hans L.. Munition with integrity gated go/no-go decision. USP2007047207517.
  9. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  10. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP1999025866838.
  11. Mayersak Joseph R. (Ashburn VA). Precision guidance system for aircraft launched bombs. USP1996045507452.
  12. Mayersak Joseph R. (Ashburn VA). Precision guidance system for aircraft launched bombs. USP1997085657947.
  13. Ratkovic, Joseph A.. Projectile guidance with accelerometers and a GPS receiver. USP2004086779752.
  14. Ratkovic, Joseph A.; Fersht, Samuel N.; Curby, Robert D.; Brockstein, Allan J.; Hsu, David Y.. Projectile guidance with accelerometers and a GPS receiver. USP2003066573486.
  15. Morris,Joseph P.; Smith,Douglas L.. Projectile trajectory control system. USP2008047354017.
  16. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.