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특허 상세정보

Missile, chemical plasm steering system, and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66    F42B-010/00   
출원번호 US-0358079 (2016-11-21)
등록번호 US-10113844 (2018-10-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sanks, Esq., Terry M.
인용정보 피인용 횟수 : 0  인용 특허 : 26
초록

Embodiments disclosed include a system comprising a missile segment having an external surface conforming to a portion of an external surface of a missile body. The missile segment comprising a plurality of chemical plasma dispensing units (CPDUs) having a chemical plasma reactant (CPR). Each CPDU is addressable so that a group of selected CPDUs in an area is ignited simultaneously to cause a first reaction to push CPR particles into a flow stream surrounding the missile body. The CPR particles to complete a second reaction in the flow stream over a reac...

대표
청구항

1. A system comprising: a missile segment having an external surface conforming to an external surface of a portion of a missile body, the missile segment comprising: a plurality of shallow cavities arranged in the external surface of the portion of the missile body and each cavity having an opening; anda plurality of chemical plasma dispensing units (CPDUs) having a chemical plasma reactant (CPR), each respective CPDU being coupled in a respective cavity and being individually addressable so that a group of selected CPDUs in an area is ignited simultane...

이 특허에 인용된 특허 (26)

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  2. Osborne, Bradley Alan; Wilson, Christopher Daniel. Airfoil trailing edge plasma flow control apparatus and method. USP2011087988101.
  3. Luu, Thu-Van T.; Boka, Jeffrey B.; Harcourt, Michael J.; Mookerjee, Purusottam. Burnout time estimation and early thrust termination determination for a boosting target. USP2012038134103.
  4. Duphorne, Darin H.. Convertible downhole devices and method of performing downhole operations using convertible downhole devices. USP2010087775286.
  5. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP200108RE37331.
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  8. Prince, Troy S.; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop control system for aircraft, missiles and munitions. USP2012058190305.
  9. Sheridan,Edward W.; Jones,John. Hydride based nano-structured energy dense energetic materials. USP2009027494705.
  10. Bagley Cloy J. (Fountain Valley CA). Lateral thruster for missiles. USP1990114967982.
  11. Gnemmi, Patrick; Rey, Christian. Low voltage device for the generation of plasma discharge to operate a supersonic or hypersonic apparatus. USP2010017645969.
  12. Sisk David S.. Mass producible launch system. USP2000036036144.
  13. Patel, Mehul; Corke, Thomas C.. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2012098267355.
  14. Patel, Mehul; Corke, Thomas C.. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2011067954768.
  15. Patel, Mehul; Corke, Tom. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2009127624941.
  16. Patel, Mehul; Corke, Tom. Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2017129834301.
  17. Schwimley, Scott L.; Drouin, Jr., Donald V.. Plasma actuator system and method for use with a weapons bay on a high speed mobile platform. USP2011098016246.
  18. Patel, Mehul; Corke, Thomas; Cain, Alan B.. Plasma optimized aerostructures for efficient flow control. USP2017019541106.
  19. Nikic, Dejan. Plasma-assisted synthetic jets for active air flow control. USP2017059637224.
  20. Gnemmi,Patrick; Charon,Romain; Samirant,Michel. Projectile steering by plasma discharge. USP2006027002126.
  21. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  22. Janson, Siegfried W.. Propulsion systems and methods utilizing smart propellant. USP2012128336826.
  23. Campbell John G. (Northridge CA) Ruttle Daniel W. (Panorama City CA). Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same. USP1996075533331.
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  26. Martinez-Tovar Bernardo ; Foster Martin C. ; Novotney David B.. Voltage-protected semiconductor bridge igniter elements. USP2001036199484.