$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Three-axis attitude control propulsion device and flying object comprising the same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00    G05D-001/00   
미국특허분류(USC) 244/003.1; 244/003.21
출원번호 US-0781701 (2004-02-20)
우선권정보 JP-2003-102445(2003-04-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wenderoth, Lind &
인용정보 피인용 횟수 : 12  인용 특허 : 14
초록

A three-axis attitude control propulsion device and a flying object like a rocket including the device are provided in which combustion gas for attitude control can be efficiently used. A three-axis attitude control propulsion device 4, having six nozzles has a motor case 6 and three-way discharge changeover valves 10, 10' of a valve plug rotation type enabling a changeover of a flow passage by rotation of the valve plug. Combustion gas 18 is generated by combustion of propellant 8 in the motor case 6. The three-axis attitude control propulsion device ...

대표
청구항

What is claimed is: 1. A three-axis attitude control propulsion device comprising a pressure generating means and two three-way discharge changeover means connected to one end of said pressure generating means, said two three-way discharge changeover means positioned with 180 degrees between each other in a rotational symmetry around a reference of an axis of said pressure generating means, wherein one of said two three-way discharge changeover means has three discharge ports, said three discharge ports having openings having orientations including (a) ...

이 특허에 인용된 특허 (14)

  1. Metz Pierre (Paris FRX). Control device using gas jets for a guided missile. USP1984114482107.
  2. Kranz Walter (Taufkrichen DEX). Control propulsion unit, especially for exerting transverse forces on a missile. USP1990124979697.
  3. Ryan William F. (Phoenix AZ). Fluidic thruster control and method. USP1983114413795.
  4. Kirschner ; Jr. Thomas J. (Port Deposit MD). Gas generator or rocket motor with selective discrete time vs. output profiles. USP1977034011720.
  5. Metz Pierre (Paris FRX). Gas jet steering device and method missile comprising such a device. USP1984084463921.
  6. Metz Pierre (Palaiseau FRX) Antonicelli Marc (Meung 1 Loire FRX). Homing device for guided missiles using side nozzles. USP1987124712747.
  7. Bagley Cloy J. (Fountain Valley CA). Lateral thruster for missiles. USP1990114967982.
  8. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  9. Anderson ; Jr. Carl W. (7914 Springfield Village Dr. Springfield VA 22152). Radial bleed total thrust control apparatus and method for a rocket propelled missile. USP1991075028014.
  10. Davies Guy E. (Hampshire GB2). Reaction jet control system. USP1989084856734.
  11. Bernard Marc (Marcilly en Villette FRX). System of vehicle guidance by continuous gas jets. USP1991045004184.
  12. Brodersen, Rolf K.. Thrust vector control for large deflection angles. USP1983054384690.
  13. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.
  14. Moll, Manfred. Wing-stabilized projectile. USP1985094541592.

이 특허를 인용한 특허 피인용횟수: 12

  1. Hanlon, Casey; Geck, Kellan; Johnson, Andrew T.. Actuation assembly. USP2012128338768.
  2. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  3. Pfiffer, Andre; Caubet, Pascal; Larrieu, Jean-Michel. Combined steering and drag-reduction device. USP2016119500456.
  4. Bergmann, Edward; London, Brian; Dineen, Andrew. Guidance control system for projectiles. USP2012098269156.
  5. Caubet, Pascal; Ferrant, Aurore. In-flight attitude control and direct thrust flight control system of a vehicle and craft comprising such a system. USP2015119194332.
  6. Yehezkeli,Oded; Kunreich,Irad. Method and system for adjusting the flight path of an unguided projectile, with compensation for jittering deviation. USP2008127467761.
  7. Sharpin, David; Kolanek, Jim; Cvetnic, Mark A.; Hutchings, Mike; Tennison, James; Nelson, Kent Carl; Hunsberger, Harold Kregg; Baseghi, Behshad. Methods and apparatuses for active protection from aerial threats. USP2015109170070.
  8. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  9. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  10. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  11. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  12. Frey, Jr., Robert D.. Tail thruster control for projectiles. USP2015109157714.