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특허 상세정보

Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/003.21; 244/003.22; 244/003.1
출원번호 US-0023118 (1998-02-13)
발명자 / 주소
대리인 / 주소
    Hunton & Williams LLP
인용정보 피인용 횟수 : 2  인용 특허 : 15
초록

An device for correcting the in-flight trajectory of a munition consists of an impulse motor assembly body. The slug or multiple slugs and propellant(s) are located within the impulse motor assembly body. When a trajectory correction is desired and required, the individual impulse motor propellants are activated and fired, and the slug or multiple slugs are propelled out of the in-flight munition at a specific time and a specific angle on or near the gravimetric center of gravity of the in-flight munition. The reactive forces created by the explosion of ...

대표
청구항

An device for correcting the in-flight trajectory of a munition consists of an impulse motor assembly body. The slug or multiple slugs and propellant(s) are located within the impulse motor assembly body. When a trajectory correction is desired and required, the individual impulse motor propellants are activated and fired, and the slug or multiple slugs are propelled out of the in-flight munition at a specific time and a specific angle on or near the gravimetric center of gravity of the in-flight munition. The reactive forces created by the explosion of ...

이 특허에 인용된 특허 (15)

  1. Linick James M. (P.O. Box 1512 La Quinta CA 92253). Apparatus and method for remote guidance of cannon-launched projectiles. USP1992075131602.
  2. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  3. Linick James (Naples FL). Method and apparatus for radial thrust trajectory correction of a ballistic projectile. USP1997075647558.
  4. Grosso Vincent A. (Hopkinton MA). Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same. USP1995065425514.
  5. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  6. Labroche Jean-Paul (St. Aubin FRX) Tonnerre Guy-Andr (Olivet FRX) Wisshaupt Daniel (Orleans FRX). Projectile and process for its use. USP1992065123612.
  7. Cover John H. (5724 N. Camino del Conde Tucson AZ 85718). Projectile propellant apparatus and method. USP1992015078117.
  8. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  9. Sturm Richard (Ottobrunn DEX). Remote control system for a rolling flying body. USP1990054928906.
  10. Waddington John F. (Tonbridge GB2). Rocket projectiles. USP1988084762293.
  11. Dunne Brian B. (La Jolla CA). Spin-stabilized projectile with pulse receiver and method of use. USP1990084951901.
  12. Purcell William O. (Maitland FL). Submunition having terminal trajectory correction. USP1985014492166.
  13. Levy Benjamin (Gedera ILX). System for correcting flight trajectory of a projectile. USP1997125695152.
  14. Couderc Georges (Bures Sur Yvette FRX) Meyzonnette Jean-Louis (Jouy-en-Josas FRX) Pepin Christian (Gif-Sur-Yvette FRX) Pressiat Robert (Ville D\Avray FRX). System to correct the trajectory of a projectile. USP1992045102065.
  15. Albrektsson Kjell A. (Karlskoga SEX) Eriksson Bertil T. (Karlskoga SEX) Eriksson Sven W. (Karlskoga SEX) Franzen Hans A. E. (Karlskoga SEX) Sandlin Rolf H. (Karlskoga SEX). Terminally corrected projectile. USP1979124176814.