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특허 상세정보

Joint construction between components of military projectile and releasable by melting of fusible eutectic helical membe

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/16   
미국특허분류(USC) 60/223 ; 60/253
출원번호 US-0239037 (1994-05-06)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 0
초록

The joint construction is employed between a military rocket motor and a warhead adapted to be propelled by the motor. The motor includes a motor tube with a cylindrical front portion having an internal cylindrical surface therein. The warhead comprises an adapter ring having a cylindrical rear portion with an external cylindrical surface which is telescopically receivable within the internal cylindrical surface. The internal and external cylindrical surfaces are formed with respective confronting aligned internal and external helical screw thread groove...

대표
청구항

A joint construction for use between a military rocket motor and a warhead adapted to be propelled by combustion of a propellent in said motor, said joint construction comprising a generally cylindrical motor tube having a connection to the front end of said rocket motor, said motor tube having a substantially cylindrical front component, a generally cylindrical adapter ring having means thereon for securing said adapter ring to said warhead, said adapter ring having a substantially cylindrical rear component, said components having respective substantia...

이 특허를 인용한 특허 피인용횟수: 22

  1. Redeker, Hendrik; Luebbers, Willi. Cartridge with safety fuse in the drive system, and method for producing it. USP2018069995563.
  2. Diehl, Matthew D.; Schneck, Eric Michael; Bogan, Gregory Norman. Decoupling assembly for a plumbing network. USP2017129851188.
  3. Singer Victor ; Solberg Mark A.. Design for a gun-launched rocket. USP2000086094906.
  4. Warner, Paul; Rothwell, Elizabeth; Ryan, Christopher. Dual-side unfoldable building modules. USP2015028943759.
  5. Michaud, Dennis; Rothwell, Elizabeth; Morton, Everett; Eason, Steven; Kassabian, Paul. Foldable building units. USP2014068739475.
  6. Devenyi, Gabor. Mechanical device having cylindrical components locked together by a retainer having an organic plastic retainer outer surface. USP2004116819510.
  7. Roach, Eric E.. Method and apparatus for releasably attaching a closure plate to a casing. USP2004066752085.
  8. Olander Donald E. ; Campbell James. Method for making a case for combustible materials. USP1999115976293.
  9. Devenyi Gabor,CAX. Preloaded device having components with an axially aligned movement. USP2001096288855.
  10. Kotefski, Stojan; Reda, Eugene R. Pressure discharge mechanism for closed vessels. USP2015048997773.
  11. Kotefski, Stojan; Reda, Eugene R; Kotefski, Nikola. Pressure discharge valve. USP2015048997774.
  12. Sullivan, Kevin Michael; Martinez, Marcelo Edgardo; Bruno, Nicolas Horacio; Desmarais, Brian. Pressure relief system for gun fired cannon cartridges. USP2015018925463.
  13. Diehl, Matthew D.; Schneck, Eric Michael; Bogan, Gregory Norman. Pressure vessel with safety features. USP2014128919254.
  14. Sneddon, Kirk; Anselmo, Estelle. Pressure-relief vent. USP2016119505532.
  15. Cesaroni Anthony J.,CAXITX L3R 8J1 ; Bartel Scott ; Kline Korey R.. Reloadable/modular solid propellant rocket motor. USP2000066079202.
  16. Woo, Timothy; Moy, Leon; Elmasri, Bishara; Morales, Christina; Cohen, Alan N.; Prillaman, Daniel Lee. Riveted cartridge venting. USP2013108550004.
  17. Diehl, Matthew D.; Schneck, Eric Michael; Bogan, Gregory Norman. Rocket motor tube with safety features. USP2013118578855.
  18. Solberg, Mark A.; Black, Robert E.. Rocket motors with insensitive munitions systems. USP2003096619029.
  19. Solberg, Mark A.; Black, Robert E.. Rocket motors with insensitive munitions systems and projectiles including same. USP2005116966264.
  20. Pitre, Sylvain; Goulet, André. Systems and methods for reducing munition sensitivity. USP20181010113846.
  21. Savage, Jr.,John M.. Threaded lens coupling to LED apparatus with compressible locking ring. USP2006016985313.
  22. Steven S. Kim ; John R. Luense. Vented MK 66 rocket motor tube with a thermoplastic warhead adapter. USP2002016338242.