RU2243403C2 - Ракетный двигатель (варианты) и ротор для него (варианты), способ осуществления рабочих процессов в ракетном двигателе (варианты) и способ охлаждения ракетного двигателя - Google Patents

Ракетный двигатель (варианты) и ротор для него (варианты), способ осуществления рабочих процессов в ракетном двигателе (варианты) и способ охлаждения ракетного двигателя Download PDF

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Publication number
RU2243403C2
RU2243403C2 RU2001127660/06A RU2001127660A RU2243403C2 RU 2243403 C2 RU2243403 C2 RU 2243403C2 RU 2001127660/06 A RU2001127660/06 A RU 2001127660/06A RU 2001127660 A RU2001127660 A RU 2001127660A RU 2243403 C2 RU2243403 C2 RU 2243403C2
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RU
Russia
Prior art keywords
combustion chamber
channel
specified
shaft
rocket
Prior art date
Application number
RU2001127660/06A
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English (en)
Russian (ru)
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RU2001127660A (ru
Inventor
Гвидо Дж. ДЕФИВЕР (US)
Гвидо Дж. ДЕФИВЕР
Джон Ф. ДЖОУНС (US)
Джон Ф. ДЖОУНС
Дин С. МАСГРЕЙВ (US)
Дин С. МАСГРЕЙВ
Ричард Д. СТИВЕНС (US)
Ричард Д. СТИВЕНС
Роберт С. мл. ТОМПСОН (US)
Роберт С. мл. ТОМПСОН
Грегг Г. УИЛЬЯМС (US)
Грегг Г. УИЛЬЯМС
Original Assignee
Уильямс Интэнэшнл Ко., эЛ.эЛ.Си.
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Publication of RU2001127660A publication Critical patent/RU2001127660A/ru
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/66—Combustion or thrust chambers of the rotary type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Testing Of Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Telescopes (AREA)
RU2001127660/06A 1999-03-10 2000-03-10 Ракетный двигатель (варианты) и ротор для него (варианты), способ осуществления рабочих процессов в ракетном двигателе (варианты) и способ охлаждения ракетного двигателя RU2243403C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12362199P 1999-03-10 1999-03-10
US60/123,621 1999-03-10

Publications (2)

Publication Number Publication Date
RU2001127660A RU2001127660A (ru) 2003-06-20
RU2243403C2 true RU2243403C2 (ru) 2004-12-27

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001127660/06A RU2243403C2 (ru) 1999-03-10 2000-03-10 Ракетный двигатель (варианты) и ротор для него (варианты), способ осуществления рабочих процессов в ракетном двигателе (варианты) и способ охлаждения ракетного двигателя

Country Status (11)

Country Link
US (3) US6220016B1 (enExample)
EP (1) EP1171705B1 (enExample)
JP (3) JP4386589B2 (enExample)
CN (2) CN1201076C (enExample)
AT (1) ATE386203T1 (enExample)
AU (1) AU6045800A (enExample)
CA (1) CA2364284C (enExample)
DE (2) DE60044733D1 (enExample)
IL (4) IL164184A0 (enExample)
RU (1) RU2243403C2 (enExample)
WO (1) WO2000057048A2 (enExample)

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RU2539064C2 (ru) * 2013-03-12 2015-01-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Двигательная установка космического летательного аппарата
RU2551713C1 (ru) * 2014-06-26 2015-05-27 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель

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CN104309562A (zh) * 2014-10-25 2015-01-28 陈恒兰 车用准固液推进剂火箭防护系统
CN105630002B (zh) * 2014-10-30 2018-11-02 北京精密机电控制设备研究所 一种液体火箭发动机变推力调节机电伺服机构
CN106050475A (zh) * 2016-08-03 2016-10-26 杨斯涵 一种液固耦合式火箭发动机
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RU2551713C1 (ru) * 2014-06-26 2015-05-27 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель

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CN1343282A (zh) 2002-04-03
EP1171705A2 (en) 2002-01-16
CA2364284A1 (en) 2000-09-28
DE60044733D1 (de) 2010-09-02
CN1201076C (zh) 2005-05-11
IL164183A0 (en) 2005-12-18
US6269647B1 (en) 2001-08-07
DE60038012D1 (de) 2008-03-27
US6205770B1 (en) 2001-03-27
EP1171705B1 (en) 2008-02-13
CA2364284C (en) 2008-05-06
DE60038012T2 (de) 2009-02-12
IL145349A0 (en) 2002-06-30
AU6045800A (en) 2000-10-09
IL145349A (en) 2007-06-17
IL164184A0 (en) 2005-12-18
JP2009150402A (ja) 2009-07-09
JP2009150401A (ja) 2009-07-09
JP2002540340A (ja) 2002-11-26
WO2000057048A3 (en) 2001-01-18
CN100417801C (zh) 2008-09-10
CN1670353A (zh) 2005-09-21
EP1171705A4 (en) 2005-01-12
US6220016B1 (en) 2001-04-24
JP4386589B2 (ja) 2009-12-16
WO2000057048A2 (en) 2000-09-28
ATE386203T1 (de) 2008-03-15

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