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특허 상세정보

Remote control system for a rolling flying body

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/033   
미국특허분류(USC) 244/322
출원번호 US-0300960 (1989-01-23)
우선권정보 DE-3801795 (1988-01-22)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 13  인용 특허 : 3

A remote control for a rolling flying body enables that body to also perform pitching movements about its pitch axis and yawing movements about its yaw axis. For this purpose the flying body is equipped with a plurality of control nozzles distributed about the circumference of the flying body. These control nozzles or rather the fluid flow through the control nozzles is so controlled by control valves that two nozzles forming a pair are simultaneously activated for causing the desired pitching and yawing movements. The duration of the control impulse sig...


A remote control system for controlling pitching and yawing movements of a rolling flying body, comprising a plurality of radially arranged fluid flow control nozzles located around the circumference of said flying body, said control nozzles providing control forces for influencing movements of said flying body, a control valve operatively connected to each control nozzle for individually controlling fluid flow through the respective control nozzle, impulse signal control circuit means for providing control impulse signals to each of said control valves ...

이 특허를 인용한 특허 피인용횟수: 13

  1. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  2. Hibma Richard A. ; Hilscher Richard W. ; Miralles Carlos T. ; Ward Jerry D. ; Wright Blaine G.. Apparatus for defending a vehicle against an approaching threat. USP2001056231003.
  3. Linick, James M.. Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like. USP2004046722609.
  4. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  5. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  6. Joseph R. Mayersak. Precision guidance system for aircraft launched bombs. USP2002106460801.
  7. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  8. Baker, Mark H.; Abel, Steve; Woessner, George. Solid propellant gas control system and method. USP2013098528316.
  9. 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.
  10. 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.
  11. Hibma Richard A. ; Hilscher Richard W. ; Yim Kitae ; Park Edward C.. System and method for defending a vehicle. USP2001056231002.
  12. Mazenq, Lionel. System for steering, about its axes of rotation, a moving body propelled by jet reaction, particularly a missile. USP2015079080843.
  13. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.