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Three axis flap control system 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G06E-019/00
  • F42B-010/00
출원번호 US-0714455 (2000-11-17)
발명자 / 주소
  • Teter, Roger D.
  • Kudlick, Dean A.
  • Williams, Richard M.
출원인 / 주소
  • Lockheed Martin Corporation
대리인 / 주소
    Swidler Berlin Shereff Friedman, LLP
인용정보 피인용 횟수 : 21  인용 특허 : 22

초록

A three axis control system employing four flaps is disclosed. The flaps are of uniform design, which decreases machining and manufacturing costs. The flaps are positioned on a vehicle orthogonally, but offset from a vehicle centerline. The system provides not only pitch and yaw control, but also bi

대표청구항

A three axis control system employing four flaps is disclosed. The flaps are of uniform design, which decreases machining and manufacturing costs. The flaps are positioned on a vehicle orthogonally, but offset from a vehicle centerline. The system provides not only pitch and yaw control, but also bi

이 특허에 인용된 특허 (22)

  1. Bagley Cloy J. (Fountain Valley CA), Airfoil deployment system for missile or aircraft.
  2. Trimbath Thomas E. (Bellevue WA), Body spoiler for yaw control of a supersonic airplane.
  3. Topliffe Roger O. (Amherst NH), Canard drive mechanism latch for guided projectile.
  4. Lee Sae D. (Buffalo Grove IL), Cathode ray tube implosion protection system.
  5. Maudal Inge (Claremont CA) Moss John F. (El Toro CA), Directional control of rockets using elastic deformation of structural members.
  6. Frank Stephen J,GBX ; Hawkins David,GBX, Drag-producing aerodynamic device.
  7. Schroeder Wayne K., Dual-control scheme for improved missile maneuverability.
  8. Goltz, Gerhard; Grosswendt, Werner; Peller, Helmut; Seidensticker, Jens, Fin stabilized subammunition body.
  9. Wassom Steven R. (Smithfield UT) Rapp Girard H. (Brigham City UT) Smalley Robert B. (Brigham City UT), Finless aerodynamic control system.
  10. Kayser Lyle D. ; Brown T. Gordon, Fold-out fin.
  11. August Henry (Chatsworth CA), Gapped flap for a missile.
  12. Johansson Sven-Eric (Karlskoga SEX) Melhus Ulf (Karlskoga SEX) Selin Lennart (Kristinehamn SEX), Ignition system.
  13. Voigt Allan A. ; Speicher John M., Integrated missile fin deployment system.
  14. Schroeder Wayne K., Method and apparatus for rapidly turning a vehicle in a fluid medium.
  15. Pinson George T. (Huntsville AL), On-board flight control drag actuator system.
  16. Pinson George T. (Huntsville AL), On-board flight control panel system.
  17. Kastenhuber Manfred (Rednitzhembach DEX) Eckel Alfred (Ireuchtlingen DEX) Bock Erich (Nuremberg DEX), Pivoting guidance mechanism for small-calibered projectiles.
  18. Minnich Violet C. (Huntsville AL), Pop-up fin.
  19. Waymeyer Walter K. (LaVerne CA) Banach Timothy P. (Chino CA), Roll damper for thrust vector controlled missile.
  20. Purcell William O. (Maitland FL), Submunition having terminal trajectory correction.
  21. Thomas E. Harkins ; T. Gordon Brown, System and method for reducing dispersion of small rockets.
  22. Ullrich Hans-Gunter,DEX, Vane control system for a guided missile.

이 특허를 인용한 특허 (21)

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard, 2-D projectile trajectory correction system and method.
  2. August,Henry, Aerodynamic control of a hypersonic entry vehicle.
  3. Alban, III, William H.; Johnston, Karl A.; Eiswirth, Edward A.; Morgan, David E., Aerodynamic re-entry vehicle control with active and passive yaw flaps.
  4. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N., Aircraft and missile forebody flow control device and method of controlling flow.
  5. Prince,Troy; Lisy,Frederick J.; Patel,Mehul P.; DiCocco,Jack M.; Carver,Reed; Schmidt,Robert N., Aircraft and missile forebody flow control device and method of controlling flow.
  6. Trosky, Bernhard; Wich, Harald; Lehmann, Lutz, Artillery rocket.
  7. Pettersson, Thomas, Brake panel for a detonator or a projectile.
  8. Olden, Thomas A.; Wrigglesworth, Walter, Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof.
  9. Fraysse, Jr., John W., Guided fuse with variable incidence panels.
  10. Prince, Troy; Kolacinski, Richard; Patel, Mehul, Hierarchical closed-loop flow control system for aircraft, missiles and munitions.
  11. Schroeder, Wayne K.; Banks, Johnny Edward, Method and apparatus for planar actuation of a flared surface to control a vehicle.
  12. Teter, Roger D.; Dunn, Steven A.; Meyer, J. William, Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy.
  13. Teter,Roger D.; Dunn,Steven A.; Meyer,J. William, Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy.
  14. Teter, Roger D.; Dunn, Steven; Barczi, Kenneth, Methods and apparatus for driving rotational elements of a vehicle.
  15. Teter, Roger D.; Dunn, Steven; Barczi, Kenneth, Methods and apparatus for varying a trim of a vehicle.
  16. Lyman, Ward D.; Koehler, Frederick B.; Sanderson, Terry M., Shape memory alloy micro-aero control surfaces.
  17. Olden, Thomas A.; Cavalleri, Robert; Kinsey, Jr., Lloyd E., Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle.
  18. Tyree, Anthony K., System and method for navigating an object.
  19. Meyer,J. W., System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping.
  20. Olden, Thomas A.; Wrigglesworth, Walter, Systems and methods for composite structures with embedded interconnects.
  21. Rutan,Elbert L., Winged spacecraft.
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