$\require{mediawiki-texvc}$
  • 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"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Mortar projectile with guided deceleration system for delivering a payload

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/56    F42B-030/10    F42B-010/00    F42B-030/00   
출원번호 US-0596767 (2015-01-14)
등록번호 US-9500454 (2016-11-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sachs, Michael C.
인용정보 피인용 횟수 : 1  인용 특허 : 22
초록

A new mortar projectile for use to resupply various payloads to distant troops. The mortar projectile has the capability of rapidly and accurately transporting the payloads to forward disposed combatants without interference of terrain or enemy action. The mortar projectile includes a shell body for housing the payload to be delivered, and a GPS-guided parafoil for delivering the payload to the designated remote target location.

대표
청구항

1. A tube-launched projectile used in a flight to deliver a payload to a distant target, the projectile comprising: a payload deployment section; anda tail section that is secured to the payload deployment section, and;wherein the payload deployment section includes a deployment mechanism that is housed within the tail section, and wherein the payload deployment section also includes a guidance decelerator system and a guided deceleration container therein, and wherein the guidance decelerator system further includes a guidance and navigation system, and...

이 특허에 인용된 특허 (22)

  1. Humphrey,John Morgan. Ballistic target defense system and methods. USP2006117137588.
  2. Bland, Geoffrey A.; Weedon, II, Larry Stephen. Conical dart sub-munitions for cargo round. USP2011128074572.
  3. Dryer, Richard. Deployable fin projectile with outflow device. USP2004026695252.
  4. Richard T. Martorana ; Jamie Anderson ; Simon Mark Spearing ; Seth Kessler ; Brent Appleby ; Edward Bergmann ; Sean George ; Steven Jacobson ; Donald Fyler ; Mark Drela ; Gregory Kirkos ; . Flyer assembly. USP2002056392213.
  5. Abbott Anthony Steven. GPS guided munition. USP2001056237496.
  6. Duchesneau Jerome G. (Andover CT). Missile fin deployment device. USP1988104778127.
  7. Inglis Ronald T. (Laguna Beach CA). Missile tail fin assembly. USP1986054588145.
  8. Inglis Ronald T. (Laguna Beach CA). Missile tail fin assembly. USP1987064673146.
  9. Alexander, Steven B.; Redhead, Richard. Mortar round glide kit. USP2012088237096.
  10. Bootes,Thomas H.; Waddell,Jesse T.. Multi-mission payload system. USP2008097418905.
  11. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  12. Mayersak Joseph R. (Ashburn VA). Precision guidance system for aircraft launched bombs. USP1997085657947.
  13. Moore, James L.; Johnson, Gary H.; Peterson, William S.; Shah, Rajesh H.; Dryer, Richard; Quortrup, Conlee O.. Precision guided extended range artillery projectile tactical base. USP2003076588700.
  14. Doughty, James L.. Projectile carrying sub-munitions. USP2005046874425.
  15. Wallow Peter (Langenfeld DEX). Projectile equipped with guide fins. USP1991024995573.
  16. Dryer,Richard; Hinsdale,Andrew J.. Projectile with propelling charge holder. USP2006047024998.
  17. Craig W. Dale (King George VA). Retainer/release mechanism for use on fin stabilized gun fired projectiles. USP1979114175720.
  18. Michel,Matthew Alan. System for dispensing projectiles and submunitions. USP2006027004073.
  19. Lloyd, Richard M.. Tandem warhead. USP2005086931994.
  20. Barson George F. ; Weber Richard M.. Unlocking tail fin assembly for guided projectiles. USP2000106126109.
  21. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Variable-force payload ejecting system. USP2008077395761.
  22. Gustafsson, Lennart; Rönn, Torsten. Warhead. USP2012068196514.

이 특허를 인용한 특허 피인용횟수: 1

  1. Huang, Jian-Lin. Rocket structure. USP2017059664142.