$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Frictional roll control apparatus for a spinning projectile 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F42B-010/02
  • F42B-010/00
  • F41G-007/00
출원번호 US-0955682 (2004-09-30)
등록번호 US-7412930 (2008-08-19)
발명자 / 주소
  • Smith,Douglas L.
  • Morris,Joseph P.
출원인 / 주소
  • General Dynamic Ordnance and Tactical Systems, Inc.
대리인 / 주소
    Shutts & Bowen, LLP
인용정보 피인용 횟수 : 17  인용 특허 : 47

초록

The invention relates generally to a roll damping apparatus for a spinning projectile having a first section and a second section rotatably attached about a roll axis. The roll damping apparatus comprises a first portion attached to the front section, and a second portion attached to the rear sectio

대표청구항

What is claimed is: 1. A spinning projectile having a roll axis, comprising: a front section rotatable about the roll axis; a rear section rotatable about the roll axis, the rear section rotatably attached to the front section; an aerosurface attached to the front section and adapted to create a fi

이 특허에 인용된 특허 (47)

  1. Shaffer James E., Airborne vehicle having deployable wing and control surface.
  2. Dunn Albert J. (Bangor ; Co. Down GB5), Control systems for moving bodies.
  3. Carlson J. David ; LeRoy Douglas F. ; Holzheimer John C. ; Prindle Donald R. ; Marjoram Robert H., Controllable brake.
  4. Perry, Craig; Schroeder, Richard W.; Voigt, Allan A., Cover ejection and fin deployment system for a gun-launched projectile.
  5. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA), Differential yoke-aerofin thrust vector control system.
  6. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA), Differential yoke-aerofin thrust vector control system.
  7. Alford Robert L. (Excelsior MN) Rupert John G. (Mahtomedi MN), Electro-mechanical roll control apparatus and method.
  8. Pijaca, Thomas; Schellens, William J., Extendable and controllable flight vehicle wing/control surface assembly.
  9. Allan A. Voigt ; Che-Ram S. Voigt ; John S. Speicher ; Charles R. Ericson, Fin and cover release system.
  10. Pazmany Ladislao (San Diego CA), Fin erection mechanism.
  11. Speicher John M. ; Voigt Che-Ram S. ; Perry Craig D. ; Voigt Allan A., Fin lock mechanism.
  12. Clancy,John A.; Bybee,Thomas D.; Friedrich,William A., Fixed canard 2-D guidance of artillery projectiles.
  13. Smith John A. (Bedford MA) Sinclair Ronald R. (Moultonboro NH), Guidance system for a projectile.
  14. Barrett ; Jr. Rolin F., Guided bullet.
  15. Jay Lipeles ; R. Glenn Brosch, Guided bullet.
  16. Bains William R. (Lake Elsinore CA), Guided projectile flight control fin system.
  17. May, Michael C.; Schroeder, Richard W.; Voigt, Allan A.; Speicher, John M.; Voigt, Che-Ram S., Gun-launched rolling projectile actuator.
  18. Voigt Allan A. ; Speicher John M., Integrated missile fin deployment system.
  19. J. David Carlson, Magnetically actuated motion control device.
  20. Robinson, Nicholas Alan, Magneto-rheological variable limited slip differential.
  21. Carlson J. David, Magnetorheological brake with integrated flywheel.
  22. Voigt Che-Ram S. (Geyserville CA), Mechanism for thrust vector control using multiple nozzles.
  23. Voigt Allan A. ; Schroeder Richard W. ; Voigt Che-Ram S. ; Speicher John M., Mechanism for thrust vector control using multiple nozzles and only two yoke plates.
  24. Linick James (Naples FL), Method and apparatus for radial thrust trajectory correction of a ballistic projectile.
  25. Seidel Wolfgang,DEX ; Guischard Frank,DEX, Method for autonomous guidance of a spin-stabilized artillery projectile and autonomously guided artillery projectile for realizing this method.
  26. Rastegar, Jahangir S.; Pelz, Richard B., Methods and apparatus for increasing aerodynamic performance of projectiles.
  27. Rastegar, Jahangir S.; Pelz, Richard B., Methods and apparatus for increasing aerodynamic performance of projectiles.
  28. Rastegar, Jahangir S.; Pelz, Richard B., Methods and apparatus for increasing aerodynamic performance of projectiles.
  29. Rastegar,Jahangir S.; Pelz,Richard B., Methods and apparatus for increasing aerodynamic performance of projectiles.
  30. Kranz Walter (Taufkirchen DEX), Missile having rotor ring.
  31. Geswender, Chris Eugene; Harline, Shawn Brent; Blaha, George A., Missile with odd symmetry tail fins.
  32. Grosso Vincent A. (Hopkinton MA), Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same.
  33. Grosso Vincent A. (Hopkinton MA), Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same.
  34. Frazer Alson C. (Santa Ana CA), Passive auto-erecting alignment wings for long rod penetrator.
  35. Sands Timothy B. (Acton MA) Sinclair Ronald R. (Moultonboro NH), Prime power source and control for a guided projectile.
  36. McClain III ; Harry T. (Riviera AZ), Projectile having plural rotatable sections with aerodynamic air foil surfaces.
  37. White Charles O., Range limited projectile using augmented roll damping.
  38. White, Charles O., Ranged limited projectile using augmented roll damping.
  39. Klestadt, Ralph H.; Stratton, Robert D.; Owan, Christopher P.; Prudic, Laurence F., Single actuator direct drive roll control.
  40. Jay Lipeles, Smart bullet.
  41. Eric L. Kathe, Sonic rarefaction wave recoilless gun system.
  42. Deakin Richard S. (Haslemere GBX), Stabilization systems.
  43. Drori Mordeki (89 Zahal St. Kiron ILX), Stabilized projectiles.
  44. Seeger Hans-Jochen (Ganderkesee DEX), Steering of an aerodynamic vehicle.
  45. Chisolm Bruce E., Tail fin deployment device.
  46. Voigt Allan A., Variable coupling arrangement for an integrated missile steering system.
  47. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA), Yoke nozzle actuation system.

이 특허를 인용한 특허 (17)

  1. Nikkel, Jonathan P.; Tyree, Anthony K., Deployable lifting surface for air vehicle.
  2. Harris, Gordon L.; Harris, Stephen L., Ground-projectile guidance system.
  3. Harris, Gordon; Harris, Stephen, Ground-projectile guidance system.
  4. Geswender, Chris E., Guidance control for spinning or rolling projectile.
  5. Geswender, Chris E.; Alejandro, Stevie; Vesty, Paul, Guidance control for spinning or rolling vehicle.
  6. Peterson, Bryan P.; Edel, Joshua L.; Head, Lawrence P., Limited range rifle projectile.
  7. Himmelmann, Richard A., Magneto-rheologic damper for electromechanical actuator.
  8. Celmins, Ilmars, Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards.
  9. Alexander, Steven B., Projectile guidance kit.
  10. Geswender, Chris E.; Zamora, Matthew A., Projectile with deployable control surfaces.
  11. Flood, William M.; O'Brien, Paul M.; Carlson, Eugene W., Roll isolation bearing.
  12. Geswender, Chris E.; Vesty, Paul; Frost, Geoffrey W.; Morgan, Bruce E.; Strassman, Doron, Rolling vehicle having collar with passively controlled ailerons.
  13. Schmidt, Robert P.; Tomes, Mark J., Spin sensor for low spin munitions.
  14. Hoffberg, Steven M., Steerable rotating projectile.
  15. Geswender, Christopher E.; Dryer, Richard; Vesty, Paul, Steerable spin-stabilized projectile.
  16. Plumer, Matt; Gibson, Jeff; Byrne, Jim; Richardson, Brian, Systems and methods for retaining and deploying canards.
  17. Morris, Joseph P.; Smith, Douglas L., Trajectory modification of a spinning projectile.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로