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Deployable fin projectile with outflow device

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-013/32   
미국특허분류(USC) 244/003.28; 244/049
출원번호 US-0246082 (2002-09-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle & Sklar, LLP
인용정보 피인용 횟수 : 11  인용 특허 : 3
초록
▼

A missile or projectile tail section includes an outflow device and a number of deployable fins. The outflow device may be a base bleed device that includes a slow-burning propellant which fills the vacuum created by the projectile's motion through the air. Use of the outflow device may allow the projectile range to be extended by up to 20%. The fins are stowed canted relative to planes that include the axis of the tail section. By canting or tilting the fins relative to the axis of the tail section, increased space is made in the tail section for the ou...

대표
청구항
▼

A missile or projectile tail section includes an outflow device and a number of deployable fins. The outflow device may be a base bleed device that includes a slow-burning propellant which fills the vacuum created by the projectile's motion through the air. Use of the outflow device may allow the projectile range to be extended by up to 20%. The fins are stowed canted relative to planes that include the axis of the tail section. By canting or tilting the fins relative to the axis of the tail section, increased space is made in the tail section for the ou...

이 특허에 인용된 특허 (3)

  1. Montet Evelyne (Bourges FRX) Masson Bernard (Bourges FRX) Chotet Eric (Vignoux FRX) Dauvergne Patrick A. G. (Levet FRX) Blin Andr (Mehun Sur Yevre FRX) Bonnet Alain (Bourges FRX) Crepin Roger C. (Vil. Deployment mechanism of a projectile fin. USP1992045108051.
  2. Kayser Lyle D. ; Brown T. Gordon. Fold-out fin. USP2001016168111.
  3. Jones ; Jr. Allen (5028 Lauderdale Ave. Virginia Beach VA 23455). Steering and stabilization apparatus for aerial missile. USP1980064209147.

이 특허를 인용한 특허 피인용횟수: 11

  1. Cleveland, Kenneth D.; Pietrzak, Amy; Butland, Adam G.; Steenson, Jr., James H.; Schorr, David J.; Borysthen-Tkacz, Joseph. Apparatus for deploying stowed control surfaces of a projectile. USP2015129207051.
  2. Cleveland, Kenneth; Pietrzak, Amy; Butland, Adam; Steenson, Jr., James H.; Schorr, David; Borysthen-Tkacz, Joseph. Apparatus for deploying stowed control surfaces of a projectile. USP2015079086259.
  3. Byrne,James Patrick; Thompson,Andrew. Method and apparatus for stowing and deploying control surfaces of a guided air vehicle. USP2006097100865.
  4. Geswender, Chris Eugene; Harline, Shawn Brent; Blaha, George A.. Missile with odd symmetry tail fins. USP2005036869044.
  5. Decker, Ryan; Yakimenko, Oleg; Hollis, Michael; Chesnulovitch, Douglas; Chaplin, Raymond; Dundon, Gary; Farbanish, Gregory. Mortar projectile with guided deceleration system for delivering a payload. USP2016119500454.
  6. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2012128338769.
  7. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2013128610042.
  8. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2012058183508.
  9. Lutzenberger, Joerg; Kaebitz, Bernd; Kroyer, Robert. Rudder system. USP20180610006748.
  10. Nitenson,Edward; Cumings,Robert. Self-propelled projectile. USP2006087083141.
  11. Rogers, Thomas R.. Techniques for controlling access through a slot on a projectile. USP2010117829830.

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