• 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

Ordnance system having a warhead with secondary elements as a payload

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-013/24    F42B-013/50    F42B-025/16   
미국특허분류(USC) 102/489 ; 102/350 ; 102/374 ; 102/393
출원번호 US-0330850 (1981-12-15)
우선권정보 DE-3048617 (1980-12-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 18  인용 특허 : 0

An ordnance system which includes a warhead accommodating a number of secondary elements, especially explosive elements as a payload, with the secondary elements adapted to be distributed over a target area. The warhead includes a coaxially arranged rotation-producing propulsion unit such as a rocket engine.


An ordnance system including a wing-stabilized warhead accommodating a plurality of secondary elements forming a payload, characterized in that propulsion means are coaxially disposed in the warhead for producing a high speed rotation of the warhead about a longitudinal axis thereof, the propulsion means being enabled at a time subsequent to launching of the warhead along a portion of the flight path for producing the high speed rotation of the warhead so as to enable distribution of the secondary elements, the propulsion means producing the high speed r...

이 특허를 인용한 특허 피인용횟수: 18

  1. Brooks, George W.; Gagnier, Mike S.. Apparatus and method for dispersing munitions from a projectile. USP2004016672220.
  2. Warner,Brad H.; Gebhard,Thomas J.. Apparatus for expelling a payload from a warhead. USP2007017168368.
  3. Lusk, Kenneth P.. Control and digital telemetry arrangement for an aerial missile. USP199402H001288.
  4. Duparc, Jean-paul; Vives, Michel; Silvain, Patrick. Device for neutralizing a payload. USP2004046718883.
  5. Adimari,Louis J.. Grenade dispense mechanism for non-spin dual purpose improved conventional munitions. USP2006016981450.
  6. Spivak, Timothy L.; Sewell, Mark W.; Fridley, Jr., Perry L.; Canaday, Michael M.. Mission responsive ordnance. USP2004076766746.
  7. Spivak, Timothy; Sewell, Mark W.; Fridley, Jr., Perry L.; Canaday, Michael M.. Mission responsive ordnance. USP2003116640723.
  8. Garcia Jose G. (Vizcaya ESX). Mortar carrier projectile. USP1989034815390.
  9. Mikhail Ameer G. (Bel Air MD). Multistage kinetic energy penetrator. USP1989114878432.
  10. Engelhardt, Johnnie Paul; Ritterhouse, Scott David. Payload deployment system with an internal cargo unit. USP2004086776375.
  11. Doughty, James L.. Projectile carrying sub-munitions. USP2005046874425.
  12. King,Hartley Hughes; Menna,Thomas Louis; Romero,Lawrence Steven. Segmented rod projectile. USP2008117448324.
  13. Budris George J. ; McGrath ; II Peter A. ; Toulouse Tony L. ; Catalano Richard J. ; Diverde Michael B.. Spacecraft dispensing system. USP2000106138951.
  14. Huber ; Jr. Joseph C. (Cuyahoga Falls OH) Nagabhushan Bellur L. (North Canton OH). Spin dispensing method and apparatus. USP1987064676167.
  15. Ettmuller Peter,CHX. Spin stabilized projectile with a payload. USP1999015864086.
  16. Ettmuller Peter,CHX. Spin-stabilized projectile with payload. USP1998105817969.
  17. Manole, Leon; Young, Mark. Stackable collaborative engagement munition. USP2018049939239.
  18. Ronn, Torsten; Johansson, Nils. Unit of ammunition with one or more warhead casings. USP2005116966265.