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특허 상세정보

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Control of a projectile by multi-chamber and single-nozzle impeller

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66   
미국특허분류(USC) 244/322 ; 102/381
출원번호 US-0590905 (1996-01-24)
우선권정보 FR-0001268 (1995-02-03)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 6  인용 특허 : 8
초록
▼

The disclosure pertains to a projectile guided by successive lateral gas jets by way of pairs of impellers. The impellers of one pair are fired so as to exert opposite moments of rotation. According to the disclosure, the impellers are brought together in two groups. Of the impellers of one pair, one is in one group and the other is in the other group. The impellers of each of the groups are separated by diode bulkheads that withstand the pressure of the impeller that is located on one side of the bulkhead and is fired first, but does not withstand the f...

대표
청구항
▼

A projectile comprising: a longitudinal axis, a center of gravity, a first group of guidance impellers having first impellers, and a second group of guidance impellers having second impellers; wherein: a first one of said first impellers leads into a first nozzle located in front of the center of gravity of the projectile, and a first one of said second impellers leads into a second nozzle located behind the center of gravity of the projectile; each of said first impellers of said first group of guidance impellers and said second impellers of said second...

이 특허에 인용된 특허 (8)

  1. Becker Wilfried (Duesseldorf DEX) Grosswendt Werner (Ratingen DEX) Schwenzer Michael (Hermannsburg DEX). Device for guiding a missile. USP1995075433399.
  2. Bchele-Buecher Sigfrid (Meerbusch-Strmp DEX). Device for the limitation of gas pressure in a combustion chamber provided inside a projectile. USP1989024803925.
  3. Ryan William F. (Phoenix AZ). Fluidic thruster control and method. USP1983114413795.
  4. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  5. Crepin Roger (Ville D\Avray FRX). Lateral gas jet piloting device. USP1986124632336.
  6. Bagley Cloy J. (Fountain Valley CA). Lateral thrust assembly for missiles. USP1992075129604.
  7. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  8. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.

이 특허를 인용한 특허 피인용횟수: 6

  1. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  2. Hamamatsu, Masanori; Kohno, Yukinobu; Higashi, Masaaki; Nakashima, Kenichi; Saito, Yasuo; Ohnishi, Hiroshi. Method and device for allocating thrust. USP2005096941195.
  3. Hamamatsu,Masanori; Kohno,Yukinobu; Higashi,Masaaki; Nakashima,Kenichi; Saito,Yasuo; Ohnishi,Hiroshi. Method and device for allocating thrust. USP2006027006905.
  4. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  5. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  6. Elwell, Jr., John M.. Systems and methods for targeting a projectile payload. USP2013108563910.

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