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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/40    B64G-001/26    F42B-010/66    F02K-009/34   
미국특허분류(USC) 060/253; 060/255; 060/256; 244/003.21; 244/003.22
출원번호 US-0945440 (2010-11-12)
등록번호 US-8826640 (2014-09-09)
발명자 / 주소
  • Olden, Thomas A.
  • Wrigglesworth, Walter
출원인 / 주소
  • Raytheon Company
대리인 / 주소
    Cantor Colburn LLP
인용정보 피인용 횟수 : 2  인용 특허 : 57
초록
▼

Embodiments of a flight vehicle are provided, as are embodiments of a method for manufacturing a flight vehicle. In one embodiment, the flight vehicle includes a solid-propellant rocket motor, control circuitry, and an electrically-interconnective support structure. The electrically-interconnective support structure includes a load-bearing frame and a plurality of electrical conductors embedded within the load-bearing frame. The solid-propellant rocket motor is mounted to the load-bearing frame, and the plurality of electrical conductors embedded within ...

대표
청구항
▼

1. A flight vehicle, comprising: a solid-propellant rocket motor;control circuitry; andan electrically-interconnective support structure, comprising:a singular load-bearing frame to which the rocket motor and the control circuitry are mounted such that the rocket motor and the control circuitry are non-rotatable relative to one another, the load bearing frame comprising first, second and third woven layers; anda plurality of electrical conductors embedded within the load-bearing frame and electrically coupling the rocket motor to the control circuitry,a ...

인용문헌 (57)

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  2. Bagley Cloy J. (Fountain Valley CA), Airfoil deployment system for missile or aircraft.
  3. Rotkopf, Menachem, Armor piercing projectile.
  4. Knoski Jerry L. (9001 E. Calle Bogota Tucson AZ 85715), Attachable airfoil with movable control surface.
  5. Koorey Alfred J. (Maitland FL), Boost-sustain-boost rocket.
  6. Kokufu, Shinobu; Suzuki, Takeshi; Echigo, Fumio; Andoh, Daizo; Ogawa, Tatsuo; Kawakita, Yoshihiro; Tomekawa, Satoru, Circuit board and its manufacture method.
  7. Hayward, James L., Circuit module and method.
  8. Das,Rabindra N.; Lauffer,John M.; Magnuson,Roy H.; Markovich,Voya R., Circuitized substrate with solder-coated microparticle paste connections, multilayered substrate assembly, electrical assembly and information handling system utilizing same and method of making said substrate.
  9. Katoh Masayoshi (Kawagoe JPX) Ishii Takashi (Tokyo JPX) Nagaoka Tadahiko (Sayama JPX), Combusting device for generation of a combustion gas.
  10. Granger Charles C. (1203 Chestnut St. Henderson NC 27536), Combustion gas pressure generator.
  11. Kranz Walter (Taufkrichen DEX), Control propulsion unit, especially for exerting transverse forces on a missile.
  12. Zheng,Rong; Rho,Hongsang; Yamarte,Luis; Kovacik,Gary J.; Sarkar,Partha, Controlling solid oxide fuel cell operation.
  13. Becker Wilfried (Duesseldorf DEX) Grosswendt Werner (Ratingen DEX) Schwenzer Michael (Hermannsburg DEX), Device for guiding a missile.
  14. Wagstaff Douglas C.,GBX, Fire mitigation device.
  15. Kline, Korey R.; Smith, Kevin W.; Cesaroni, Anthony Joseph, Flame holder for a hybrid rocket motor.
  16. Tsukada,Kiyotaka; Ninomaru,Terumasa; Kizaki,Masaki, Flexible printed wiring board.
  17. Barnes Michael W. (Brigham City UT) Taylor Robert D. (Hyrum UT), Gas generant compositions containing amine nitrates plus basic copper (II) nitrate and/or cobalt(III) triammine trinitra.
  18. Daniel W. Doll ; Gary K. Lund ; Craig D. Hughes ; Marc A. Hall ; David J. Macon, Gas generating eject motor.
  19. Metz Pierre (Paris FRX), Guided projectile.
  20. Hinrichs James O. (Odessa MO), High reverse pressure resistant low forward burst pressure rupture disc assembly.
  21. Osofsky Irving B. (28327 San Nicolas Dr. Rancho Palos Verdes CA 90274), High velocity impulse rocket.
  22. Stevens, George L., Igniter pellet cup.
  23. Denes Oscar L. (Greendale WI), Injection molded printed circuits.
  24. Felix Steven D., Man-packable missile weapon system.
  25. Linick James (Naples FL), Method and apparatus for radial thrust trajectory correction of a ballistic projectile.
  26. Metcalf, Gary S.; White, William E., Method of constructing insulated metal dome structure for a rocket motor.
  27. Martins, Laura J.; Cragun, Richard B.; Lund, Gary K.; Wells, Michael V.; Mancini, Vincent E., Method of making multi-base propellants from pelletized nitrocellulose.
  28. Kobayashi, Takashi; Oka, Seiji; Funahashi, Kazuo; Tsuruse, Hideki, Method of manufacturing a circuit print board.
  29. Dryer, Richard, Methods and apparatus for projectile guidance.
  30. Woessner, George T., Missile thrust system and valve with refractory piston cylinder.
  31. Lundstrom Norman H., Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate.
  32. Bastian Thomas W. (Fullerton CA) Roberts J. Sydney (Fullerton CA), Multi-burn solid fuel restartable rocket and method of use.
  33. Koyama, Masayoshi; Hayashi, Yoshitake; Otani, Kazuo, Multilayer circuit board and manufacturing method thereof.
  34. Morris Joseph W. (Rancho Cordova CA) Carlson Russell W. (Folsom CA) Peterson Kevin L. (Sacramento CA) Reich Edward M. (Orangevale CA), Multiple pintle nozzle propulsion control system.
  35. Cesaroni, Anthony Joseph; Dennett, Michael J.; Kline, Korey R.; Mahaffy, Kevin E.; Smith, Kevin W., Oxidizer package for propellant system for rockets.
  36. Cesaroni,Anthony J.; Dennett,Michael J.; Louwers,Jeroen, Propellant system for solid fuel rocket.
  37. Krishnan, Vinu B., Propulsion from combustion of solid propellant pellet-projectiles.
  38. Krishnan,Vinu B., Propulsion from combustion of solid propellant pellet-projectiles.
  39. Alan Z. Glasser, Propulsion system.
  40. Hattori Nobuyoshi,JPX ; Yamana Kaoru,JPX ; Tamada Tomoki,JPX, Quality management system and recording medium.
  41. Canterberry J. B. (Taft TN) Flanigan David A. (Ogden UT), Rapid burning propellant charge for automobile air bag inflators, rocket motors, and igniters therefor.
  42. Humiston Robert G. (Ogden UT) Ralston Joseph L. (North Ogden UT) Marchant Brent R. (Ogden UT), Reduced cost membrane seal assembly for pulsed rocket motor.
  43. Hibler Donald R. (Bates City MO) Hinrichs James O. (Odessa MO), Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor.
  44. Whitesides ; Jr. Roger H. (Somerville AL), Rocket motor or gas generator having controlled thrust or mass flow output.
  45. Cavalleri, Robert J.; Olden, Thomas A., Rocket motor with pellet and bulk solid propellants.
  46. Wilkinson, David B.; Cloyd, James S., Solid fuel rocket thrust control.
  47. Woessner, George T.; Abel, Stephen G.; Peck, Ronald A.; Baker, Mark H.; Christensen, Donald J., Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method.
  48. Dombrowski Daniel C. (Elkton MD) Frey Thomas J. (Wilmington DE) Nevrincean Andrew G. (Oxford PA), Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture.
  49. Carrier Joseph L. C. (Ste-Foy CAX) Constantinou Tryfon (Sillery CAX) Shea Charles J. (Ste-Foy CAX) Smith Donald L. (Ste-Foy CAX), Solid rocket motor with dual interrupted thrust.
  50. Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA), Solid-propellant-powered maneuvering system for spacecraft.
  51. Rohrbaugh,Eric M.; White,Jeffrey M., Steerable, intermittently operable rocket propulsion system.
  52. Knight,Andrew F., Super-staged and continuously staged rocket.
  53. Le Helley,Philippe; Jacques,Louis; Magni챕re,Christophe; Uhrig,Gilles; Bondon,Bernard; Tricot,Jean Claude; Boury,Didier; Telara,Marco; Bellomi,Paolo; Mastrangelo,Georgio, System and method of controlling pressure oscillations of hydrodynamic origin for a solid propellant thruster.
  54. Denoel Jean Denis,FRX ; Dumortier Andre,FRX, System for controlling a space vehicle by gating gas.
  55. Teter, Roger D.; Kudlick, Dean A.; Williams, Richard M., Three axis flap control system.
  56. Franz David Bruce (Ventura CA), Timed missile flight termination system.
  57. Tani, Motoaki; Hayashi, Nobuyuki; Abe, Tomoyuki; Takahashi, Yasuhito; Saeki, Yoshiyasu, Wiring board with core layer containing inorganic filler.

이 특허를 인용한 특허 (2)

  1. Nelson, Steven; Current, Peter; Stadler, Steven, Propulsion system comprising plurality of individually selectable solid fuel motors.
  2. Koehler, Frederick B.; Danforth, Jeremy C.; Lyman, Ward D.; Langhenry, Mark T.; Summers, Matt H.; Pontius, Paul E.; Pape, Brian M.; Stallings, Jared D.; Villarreal, James K.; Villarreal, Thomas, Satellite with integral thrusters.

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