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특허 상세정보

Guided projectile

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00    F42B-010/60    F42B-015/01   
미국특허분류(USC) 244/315 ; 244/322
출원번호 US-0928976 (1978-07-28)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 34  인용 특허 : 0
초록

A guided projectile, especially a propelled or ballistic missile, has its trajectory corrected by gas jets from pulse thrusters disposed in at least on axial plane of the missile symmetrically on opposite sides of the center of gravity thereof and whose thrusts are countered, when no longer needed, by the operation of diametrically opposite pulse thrusters in the same plane and at the same side of the center of gravity. The pulse thrusters are formed as gas generators which can be triggered to feed respective nozzles. The projectile is also roll stabiliz...

대표
청구항

A guided projectile comprising: an elongated axially extending projectile body having a front end, a rear end and a center of gravity located along the axis of said body between said ends; a plurality of pulse thrusters axially spaced along said body and each provided with a pair of diametrically opposite, oppositely opening thrust nozzles lying in a guidance director plane, the nozzles of both said pulse thrusters being disposed symmetrically on opposite sides of said center of gravity in the same guidance director plane; respective triggerable-release ...

이 특허를 인용한 특허 피인용횟수: 34

  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. Blue, Linden S.; Blue, Austin J. N.. Aircraft. USP2018019878788.
  4. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  5. Boone, Donald M.; Gotzmer, Carl; Johnson, Kenneth B.; Lipton, Leonard D.; Scherr, Michael R.. Dipole antenna projectile with sensor. USP2009097581501.
  6. Flynn, Dennis Joseph; Locking, Paul Martin; Johnson, Martin. Drag reduction system. USP20180710030951.
  7. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  8. Schneider, Arthur J.. Guided kinetic penetrator. USP2010097795567.
  9. Linick, James M.. Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like. USP2004046722609.
  10. Arthur J. Schneider ; James G. Small. Impulse radar guidance apparatus and method for use with guided projectiles. USP2002096450442.
  11. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  12. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  13. Sharpin, David; Kolanek, Jim; Cvetnic, Mark A.; Hutchings, Mike; Tennison, James; Nelson, Kent Carl; Hunsberger, Harold Kregg; Baseghi, Behshad. Methods and apparatuses for active protection from aerial threats. USP2015109170070.
  14. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  15. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  16. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  17. Grosse Matthias,DEX. Missile for combatting moving targets. USP1999085931414.
  18. Dryer, Richard. Modular guided projectile. USP2013108546736.
  19. Anderson,Steven E.. Modular projectile system. USP2009037506587.
  20. Teetzel, James W.; Celona, Marc J.; Lemire, Gary M.. Modular rocket system. USP2015119194678.
  21. Biggers James E. ; Finn Kevin P. ; Schwartz ; II Homer H.. Neural network controller for a pulsed rocket motor tactical missile system. USP2000106138945.
  22. Romer Rudolf,DEX ; Wollmann Gerd,DEX. Projectile having an apparatus for flight-path correction. USP1998115836540.
  23. 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.
  24. Silverman, Fredric Scott; Lowe, Gregory Arthur; Little, Jr., Gaybert Barnes. Pyrotechnic electric generator. USP2014078763531.
  25. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  26. Facciano, Andrew B.; Alkema, Michael S.; Moore, Robert T.. Rocket propelled payload with divert control system within nose cone. USP2015049018572.
  27. Mccool, James W.. Steerable spin-stabilized projectile and method. USP2012118319162.
  28. Cesaroni, Anthony Joseph. Surface skimming munition. USP2015018939084.
  29. Cesaroni, Anthony Joseph. Surface skimming munition. USP2016099448049.
  30. Pearce, John Gregory; Brodbeck, Gregory V.. Switch key tool for use in changing switch knob settings on a laser guided bomb. USP2003126666142.
  31. 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.
  32. 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.
  33. Rossi, Rinaldo. System for steering a flying object using pairs of lateral nozzles. USP2015129212880.
  34. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.