$\require{mediawiki-texvc}$

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.

Combustion ignition

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
  • F02K-003/00
출원번호 US-0334019 (2002-12-30)
발명자 / 주소
  • Nordeen,Craig A.
  • Norris,James W.
  • Twelves, Jr.,Wendell V.
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Bachman &
인용정보 피인용 횟수 : 18  인용 특허 : 21

초록

Distributed initiation (e.g., multipoint or continuous) is utilized to obtain constant volume-like combustion performance in a pulse combustion device in the absence of detonation. A number of such devices may be utilized as turbine engine combustors.

대표청구항

What is claimed is: 1. A pulse combustion device comprising: a vessel having a gas inlet and a gas outlet; a valve for opening and closing the inlet to admit a charge of gas; and means for producing a distributed ignition of said gas along a flow path within the vessel to initiate combustion of sai

이 특허에 인용된 특허 (21)

  1. Louis G. Hunter, Jr. ; Kent W. Benner, Annular liquid fueled pulse detonation engine.
  2. Hunter ; Jr. Louis G. (Fort Worth TX) Winfree Don D. (Keller TX), Annular pulse detonation apparatus and method.
  3. Louis G. Hunter ; Billy D. Couch ; Paul E. Hagseth, Combined cycle pulse combustion/gas turbine engine.
  4. James E. Johnson ; Lawrence W. Dunbar ; Lawrence Butler, Combined cycle pulse detonation turbine engine.
  5. Johnson, James E.; Dunbar, Lawrence W.; Butler, Lawrence, Combined cycle pulse detonation turbine engine operating method.
  6. Dodd Alec G,GBX, Gas turbine engine casing.
  7. Putnam Abbott A. (Columbus OH) Locklin David W. (Columbus OH), Heating apparatus.
  8. Hunter, Jr., Louis G., MAPP gas fuel for flight vehicles having pulse detonation engines and method of use.
  9. Gregory Vincent Meholic ; William Randolph Stowell, Magnetohydrodynamic flow control for pulse detonation engines.
  10. McSpadden Hugh J. (Glendale AZ) Olander Donald E. (Tempe AZ), Multi-stage rocket motors.
  11. Hunter ; Jr. Louis G. (Ft. Worth TX), On line pulsed detonation/deflagration soot blower.
  12. Sumitani Shigeto (Fuji JPX), Pulse combustor.
  13. Meholic, Gregory Vincent, Pulse detonation aerospike engine.
  14. Hunter ; Jr. Louis G. (Fort Worth TX) Winfree Don D. (Keller TX), Pulse detonation apparatus with inner and outer Spherical valves.
  15. Hunter ; Jr. Louis G. (Fort Worth TX) Winfree Don D. (Keller TX), Pulse detonation engine.
  16. Winfree Don D. ; Hunter ; Jr. Louis G., Pulse detonation igniter for pulse detonation chambers.
  17. Lorenz Edmund (Badendorf 54 A-8413 St. Georgen a.d. Stiefing ATX), Pulse-controlled turbine.
  18. Hinkey John B. ; Williams Joseph T. ; Bussing Thomas R.A., Pulsed combustion acoustic wave generator.
  19. Philip Harold Snyder, Pulsed detonation engine wave rotor.
  20. DeRoche Mark, Repetitive detonation generator.
  21. Plemmons Larry W. (Fairfield OH) Wesling Richard A. (Cincinnati OH), Seal exit flow discourager.

이 특허를 인용한 특허 (18)

  1. Rupp, George D; Troia, Trajaen J., Airflow modulation for dual mode combined cycle propulsion systems.
  2. Rupp, George D.; Troia, Trajaen J., Airflow modulation system and method.
  3. Nordeen, Craig A., Direct induction combustor/generator.
  4. Brumberg, Justin Thomas; Rasheed, Adam, Fluidic deflagration-to-detonation initiation obstacles.
  5. Brumberg, Justin Thomas; Rasheed, Adam; Davis, Dustin Wayne, Integrated deflagration-to-detonation obstacles and cooling fluid flow.
  6. Chandran, Ravi; Newport, Dave G.; Burciaga, Daniel A.; Leo, Daniel Michael; Miller, Justin Kevin; Harrington, Kaitlin Emily; Attwood, Brian Christopher, Liquid fuel production system having parallel product gas generation.
  7. Chandran, Ravi; Leo, Daniel Michael; Freitas, Shawn Robert; Newport, Dave G.; Whitney, Hamilton Sean Michael; Burciaga, Daniel A., Method for converting biomass into fischer-tropsch products with carbon dioxide recycling.
  8. Henry,John Leslie, Methods and apparatus for generating gas turbine engine thrust using a pulse detonator.
  9. Lupkes,Kirk R.; Lidstone,Gary L., Pulse combustion device.
  10. Lupkes,Kirk R.; Lidstone,Gary L.; Parish,Mark W., Pulse combustion device.
  11. Chandran, Ravi; Newport, Dave G.; Burciaga, Daniel A.; Leo, Daniel Michael; Miller, Justin Kevin; Harrington, Kaitlin Emily; Attwood, Brian Christopher; Whitney, Hamilton Sean Michael, Pulse combustion heat exchanger system and method.
  12. Chandran, Ravi; Newport, Dave G.; Burciaga, Daniel A.; Leo, Daniel Michael; Miller, Justin Kevin; Harrington, Kaitlin Emily; Attwood, Brian Christopher; Whitney, Hamilton Sean Michael, Pulse combustion heat exchanger system and method.
  13. Murayama,Motohide; Yamawaki,Shigemichi; Toh,Hidemi; Kobayashi,Hideo; Takahashi,Katsuyoshi; Chiba,Kaoru; Ohyagi,Shigeharu, Pulse detonation engine system for driving turbine.
  14. Boespflug, Matthew Patrick; Steenburgh, Dennis; Saddoughi, Seyed Gholami; Bennett, Grover Andrew, Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production.
  15. Razzell, Anthony G; Taylor, Mark D; Mason, Samuel A; Miller, Robert J, Pulse jet engine having pressure sensor means for controlling fuel delivery into a combustion chamber.
  16. Chandran, Ravi; Burciaga, Daniel A.; Leo, Daniel Michael; Freitas, Shawn Robert; Newport, Dave G.; Miller, Justin Kevin; Harrington, Kaitlin Emily; Attwood, Brian Christopher, Two-stage energy-integrated product gas generation system and method.
  17. Kenyon, Ross Hartley; Brumberg, Justin Thomas, Variable initiation location system for pulse detonation combustor.
  18. Miller, Brandon Wayne; Prentice, Ian Francis; Niergarth, Daniel Alan, Variable pitch fan for gas turbine engine and method of assembling the same.
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