$\require{mediawiki-texvc}$
  • 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

Projectile with correctable trajectory

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/18   
미국특허분류(USC) 244/322 ; 102/202 ; 102/381
출원번호 US-0580333 (1990-09-10)
우선권정보 DE-3931173 (1989-09-19)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 0
초록

A spin-stabilized projectile with a correctable trajectory, wherein the projectile possesses lateral or transverse thrust-propulsion devices which are distributed about the circumference thereof, each incorporating an impulse-generating charge inclusive an electrically-activatable detonator arranged beneath a cover which is radially ejectable relative to the longitudinal axis of the projectile. The detonator, with the presence of a connecting cable which initially extends coaxially with the cover and then thereafter extends at an angle relative thereto, ...

대표
청구항

A spin-stabilized projectile having a correctable trajectory; including propulsion devices for producing a lateral thrust being distributed about the circumference of said projectile, each said propulsion device having an impulse-generating charge including an electrical-actuatable detonator arranged below a cover which is radially outwardly expellable relative to the longitudinal axis of the projectile, said detonator having a connecting cable which initially extends coaxially with the cover and then at an angle relative thereto and being arranged in a ...

이 특허를 인용한 특허 피인용횟수: 19

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  3. Shpund, Zalman Shlomo; Sahar, David. Airborne guided shell. USP2012108278611.
  4. Linick, James M.. Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like. USP2004046722609.
  5. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  6. Schroeder Wayne K.. Method and apparatus for rapidly turning a vehicle in a fluid medium. USP2001106308911.
  7. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  8. Blackburn, Thomas R.. Methods and apparatus for guiding a projectile. USP2011017872215.
  9. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  10. Romer Rudolf,DEX ; Wollmann Gerd,DEX. Projectile having an apparatus for flight-path correction. USP1998115836540.
  11. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  12. Horwath Tibor G.. Reticle for use in a guidance seeker for a spinning projectile. USP2000066076765.
  13. Tibor G. Horwath. Reticle for use in a guidance seeker for a spinning projectile. USP2002036357695.
  14. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  15. Facciano, Andrew B.; Alkema, Michael S.; Moore, Robert T.. Rocket propelled payload with divert control system within nose cone. USP2015049018572.
  16. Kautzsch,Karl; Reindler,Albrecht. Spin-stabilized artillery projectile. USP2008047360490.
  17. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  18. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  19. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.