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특허 상세정보

Drag control module for stabilized projectiles

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/00   
미국특허분류(USC) 244/032.4 ; 244/032.5 ; 244/032.7 ; 244/032.1
출원번호 US-0924515 (1997-09-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Clohan
인용정보 피인용 횟수 : 17  인용 특허 : 15
초록

A trajectory (range) control device which is designed to fit behind the f of a fin stabilized ballistic projectile for correcting range error. The trajectory (range) control device is a self-contained, add-on module, which will screw into the forward portion of the projectile. The fuze will then screw into the trajectory (range) control module, which has a small through hole that will coincide with the center of the fuze and the center of the projectile. This through hole is intended to provide a channel in which the fuze can detonate the intended booste...

대표
청구항

[ What is claimed is:] [1.] A device to control the range of trajectory of a fin stabilized projectile having a fuze located in the nose of the projectile comprising:an add-on drag producing module removably located in the forward portion of said projectile between the body of said projectile and the fuze of said projectile; said module having attachment means on either end designed to mate with said fuze and said projectile such that said module can be attached to said projectile at a time Prior to launch of said projectile by removing the fuze from sai...

이 특허에 인용된 특허 (15)

  1. Klestadt Ralph H. (Tucson AZ). Aerodynamic lifting and control surface and control system using same. USP1997075642867.
  2. Steuer Raimar (Leinburg DEX) Kraus Werner (Neumarkt DEX). Airborne submunition member. USP1991075031856.
  3. Linick James M. (P.O. Box 1512 La Quinta CA 92253). Apparatus and method for remote guidance of cannon-launched projectiles. USP1992075131602.
  4. Topliffe Roger O. (Amherst NH). Automatically deployed shell fins. USP1982064332360.
  5. Washington William D. (Arab AL) Killough Thomas L. (Huntsville AL) Booth Pamela F. (Huntsville AL) Walker Billy J. (Madison AL). Curved grid fin. USP1991095048773.
  6. Goulding Kenneth (Stevenage GB2). Deployment and actuation mechanisms. USP1987124709877.
  7. Malloy James C. (Ferndale MI). Descaling/deglassing salt composition and method. USP1993065221358.
  8. Wedertz Larry D. (Mira Loma CA). Double swing wing self-erecting missile wing structure. USP1987054667899.
  9. Wedertz Larry D. (Alta Loma CA) Vazquez Jose R. (Rancho Cucamonga CA) Schoneman Scott R. (Ontario CA). Expandable telescoped missile airframe. USP1990074944226.
  10. Brieseck Bernd (Henfenfeld DEX) Kreuzer Peter (Zirndorf-Weiherhof DEX). Foldable wing, especially for a projectile. USP1987014635881.
  11. Bains William R. (Lake Elsinore CA). Guided projectile flight control fin system. USP1986014565340.
  12. Spiroff Carl M. (Granite City IL). Low height fin control actuator. USP1987044655420.
  13. Geis Norman P. (Kensington NH) Chambers Edward A. (Acton MA). Mortar system with improved round. USP1985084533094.
  14. Kastenhuber Manfred (Rednitzhembach DEX) Eckel Alfred (Ireuchtlingen DEX) Bock Erich (Nuremberg DEX). Pivoting guidance mechanism for small-calibered projectiles. USP1986074600167.
  15. Madderra, Jimmy M.. Rocket fin hold down spring. USP1983054384691.

이 특허를 인용한 특허 피인용횟수: 17

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard. 2-D projectile trajectory correction system and method. USP2007017163176.
  2. Rupert, John G.; Siewart, Jeff. 2-D projectile trajectory corrector. USP2003016502786.
  3. Rupert, John G.; Siewart, Jeff. 2-D projectile trajectory corrector. USP2003126666402.
  4. Zemany, Paul D.; Carlson, Mark A.; Maynard, John A.. Ballistic guidance control for munitions. USP2010117834300.
  5. Johnson Mark W.. Competent munitions using range correction with auto-registration. USP2000056069584.
  6. Hickey, Dennis J. Device for exerting drag. USP2004016682014.
  7. Bonnet Alain,FRX ; Padiolleau Bertrand,FRX ; Cros Anne-Laure,FRX. Device for translational braking of a projectile on its trajectory. USP2001126325325.
  8. Thomas E. Harkins ; Bradford S. Davis. Drag-brake deployment method and apparatus for range error correction of spinning, gun-launched artillery projectiles. USP2002026345785.
  9. Malejko, Gregory; Fulton, Keith; Nguyen, Ductri. Extendable stabilizer for projectile. USP2014058735789.
  10. Ginetto, Stephen; Moramarco, Andrew; Mohla, Leanne. Frangible tail boom for projectile. USP2016109470491.
  11. Axford, Richard Desmond Joseph; Beggs, Kevin William. Guidance device. USP2014038674277.
  12. August,Henry. Mortar shell ring tail and associated method. USP2007087262394.
  13. Ginetto, Stephen; Moramarco, Andrew; Mohla, Leanne. Projectile tail boom with self-locking fin. USP2017079702673.
  14. Olden, Thomas A.; Cavalleri, Robert; Kinsey, Jr., Lloyd E.. Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle. USP2012068193476.
  15. Bar, Klaus; Bohl, Jurgen; Kautzsch, Karl. Spin-stabilized projectile with a braking device. USP2003016511016.
  16. Cohe, Patrick; Dubois, Bertrand; Moreau, Fabien. Steering section for guided munition. USP2014118890043.
  17. Bonnet Alain,FRX ; Cros Anne-Laure,FRX. Translational braking device for a projectile during its trajectory. USP2001106310335.