$\require{mediawiki-texvc}$
  • 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

Device for guiding a missile

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/322 ; 244/321
출원번호 US-0253036 (1994-06-02)
우선권정보 DE-4408085 (1994-03-10)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 0
초록

The invention relates to a device for guiding a missile (1; 30) with a missile tip (2) and a cylindrical section (3) adjoining the tip of the missile; the device is provided with at least one control block (4; 31, 32) with exhaust openings (13-15) of corresponding nozzle bodies (10-12) arranged perpendicularly in relation to the missile\s surface. In order to accomplish effective guidance, particularly of high-speed missiles (1; 30), in a simple and cost-effective manner it is proposed that the control block (4; 31, 32) be constructed with a plurality of...

대표
청구항

In a device for guiding a missile having a missile tip and a cylindrical section adjoining the tip of the missile, said device having at least one control block with exhaust openings for corresponding nozzle bodies arranged perpendicularly in relation to the missile\s surface; the improvement wherein: the at least one control block contains a plurality of small, fast-burning rocket motors which are arranged radially on the periphery of the missile and which are ignitable in a predeterminable sequence and number; and two said control blocks that can rotat...

이 특허를 인용한 특허 피인용횟수: 21

  1. Rastegar, Jahangir S.; Spinelli, Thomas. Actuators for gun-fired projectiles and mortars. USP2015109151581.
  2. Rastegar, Jahangir S.; Spinelli, Thomas. Actuators for gun-fired projectiles and mortars. USP2010097800031.
  3. Shpund, Zalman Shlomo; Sahar, David. Airborne guided shell. USP2012108278611.
  4. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  5. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  6. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004076766979.
  7. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004116817569.
  8. Heitmann,Thomas; Schwenzer,Michael. Lateral thrust control. USP2006107118065.
  9. Banks, Johnny E.; Baker, Brian C.. Method and apparatus for controlling a trajectory of a projectile. USP2003106637699.
  10. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  11. Facciano, Andrew B.; Ebel, James A.; Alkema, Michael; Travis, Robert D.; Saxton, Mike J.. Projectile and method that include speed adjusting guidance and propulsion systems. USP2014058729443.
  12. Folsom,Mark; Piper, III,Charles; Fahey,Wm. David; McGowan,Jared M.. Projectile diverter. USP2006027004423.
  13. Horwath Tibor G.. Reticle for use in a guidance seeker for a spinning projectile. USP2000066076765.
  14. Tibor G. Horwath. Reticle for use in a guidance seeker for a spinning projectile. USP2002036357695.
  15. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  16. Facciano, Andrew B.; Alkema, Michael S.; Moore, Robert T.. Rocket propelled payload with divert control system within nose cone. USP2015049018572.
  17. Kim, Won Hoon; Cho, Won Man; Lee, Bang Eop; Moon, Soon Il; Son, Young Il. Side thruster module. USP2009117610747.
  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. USP2010127851732.
  19. 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.
  20. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.
  21. Elwell, Jr., John M.. Systems and methods for targeting a projectile payload. USP2013108563910.