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특허 상세정보

Missile with adjustable flying controls

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/02   
미국특허분류(USC) 244/321 ; 102/208
출원번호 US-0283628 (1988-12-13)
우선권정보 DE-3742836 (1987-12-17)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 17  인용 특허 : 4

A missile with adjustable flight controls capable of altering the missile\s flight path is disclosed. The missile comprises an electric generator and control electronics. The electric generator is used in this invention both to provide electrical power to the control electronics and to regulate the flight controls. A mechanical connection is created between the generators rotor and the flight controls. The generator is electrically coupled to the control electronics through an electrically variable load. The control electronics alters the load which vari...


A missile with target sensor means comprising: adjustable flight control means; electric generator means having a rotor and a stator, the rotor and stator being mounted on two sections of the missile capable of rotary movement relative to one another, the rotor being mechanically coupled to the adjustable flight control means; variable electric load means coupled to the electric generator means for providing variable electric resistance; and control electronic means coupled to the target sensor means and the variable electric load means, the control elec...

이 특허를 인용한 특허 피인용횟수: 17

  1. Mock, M Robert. Eccentric drive control actuation system. USP2010077755012.
  2. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C.. G-hardened flow control systems for extended-range, enhanced-precision gun-fired rounds. USP2015079086258.
  3. Mock,M. Robert; Marshall,John Adams; Sweer,Grant Allen. Guided projectile with power and control mechanism. USP2008107431237.
  4. Zeglar, Frank C.. Integrated vehicle fluids. USP2014118884202.
  5. Zegler, Frank C.. Integrated vehicle fluids. USP2017129850008.
  6. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C.. Methods for extended-range, enhanced-precision gun-fired rounds using g-hardened flow control systems. USP2017059658040.
  7. Rastegar, Jahangir S.; Murray, Richard T.. Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons. USP2014048701558.
  8. Rastegar, Jahangir S.; Murray, Richard T.. Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons. USP2013058443726.
  9. Rastegar, Jahangir S.. Miniature safe and arm mechanisms for fuzing of gravity dropped small weapons. USP2014028646386.
  10. Frank F. Webster. Modular rocket boosted penetrating warhead. USP2002126494140.
  11. Arata,Allen A.. Movable nose cap and control strut assembly for supersonic aircraft. USP2007107278609.
  12. Smith, Brian J.; Kennedy, Kevin D.. On-board power generation system for a guided projectile. USP2005016845714.
  13. Schmacker Bruce E.. Rocket-boosted guided hard target penetrator. USP2001086276277.
  14. Bär, Klaus; Kautzsch, Karl. Spin-stabilized correctible-trajectory artillery shell. USP2009097584922.
  15. Phillips, Craig A.. Targeting augmentation for short-range munitions. USP2013088513580.
  16. Harnoy, Amir. Techniques for articulating a nose member of a guidable projectile. USP2010047696459.
  17. Harnoy, Amir. Techniques for providing surface control to a guidable projectile. USP2010097791007.