ATE482333T1 - Lavaldüse eines raketenantriebs - Google Patents

Lavaldüse eines raketenantriebs

Info

Publication number
ATE482333T1
ATE482333T1 AT08719289T AT08719289T ATE482333T1 AT E482333 T1 ATE482333 T1 AT E482333T1 AT 08719289 T AT08719289 T AT 08719289T AT 08719289 T AT08719289 T AT 08719289T AT E482333 T1 ATE482333 T1 AT E482333T1
Authority
AT
Austria
Prior art keywords
expansion
nozzle
throat
ring slot
rocket engine
Prior art date
Application number
AT08719289T
Other languages
English (en)
Inventor
Vasily Semenov
Alexander Sergienko
Original Assignee
Moscow Aviat I
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Moscow Aviat I filed Critical Moscow Aviat I
Application granted granted Critical
Publication of ATE482333T1 publication Critical patent/ATE482333T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust 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
    • F02K9/97—Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Eye Examination Apparatus (AREA)
  • Chair Legs, Seat Parts, And Backrests (AREA)
AT08719289T 2007-04-24 2008-03-13 Lavaldüse eines raketenantriebs ATE482333T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2007115187/06A RU2326259C1 (ru) 2007-04-24 2007-04-24 Высотное сопло лаваля
PCT/IB2008/000581 WO2008129372A2 (en) 2007-04-24 2008-03-13 Rocket engine laval nozzle with gas injection device

Publications (1)

Publication Number Publication Date
ATE482333T1 true ATE482333T1 (de) 2010-10-15

Family

ID=39581397

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08719289T ATE482333T1 (de) 2007-04-24 2008-03-13 Lavaldüse eines raketenantriebs

Country Status (6)

Country Link
EP (1) EP2137395B1 (de)
AT (1) ATE482333T1 (de)
DE (1) DE602008002737D1 (de)
ES (1) ES2352445T3 (de)
RU (1) RU2326259C1 (de)
WO (1) WO2008129372A2 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2465483C1 (ru) * 2011-03-31 2012-10-27 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") Способ изготовления сопла камеры сгорания жидкостного ракетного двигателя (жрд)
RU2551244C2 (ru) * 2013-07-16 2015-05-20 Федеральное государственное бюджетное учреждение науки Институт теоретической и прикладной механики им. С.А. Христиановича Сибирского отделения Российской академии наук (ИТПМ СО РАН) Способ увеличения тяги сверхзвукового сопла ракетного двигателя
RU167750U1 (ru) * 2016-03-15 2017-01-10 Федеральное государственное бюджетное образовательное учреждение высшего образования Московский авиационный институт (национальный исследовательский университет) (МАИ) Высотное сопло лаваля
FR3080407B1 (fr) * 2018-04-18 2020-04-24 Centre National De La Recherche Scientifique Controle de transition de regime et de vectorisation de poussee dans une tuyere a galbe multiple par injection secondaire
RU185255U1 (ru) * 2018-04-24 2018-11-28 Федеральное государственное бюджетное образовательное учреждение высшего образования "Московский авиационный институт (национальный исследовательский университет)" Высотное сопло Лаваля
CN110594044B (zh) * 2019-10-17 2022-03-18 哈尔滨工程大学 一种自适应高度的柔性延伸喷管
CN110985231B (zh) * 2019-11-19 2020-10-13 中国人民解放军国防科技大学 一种闭环自适应调节的引射器及火箭喷管
CN113153580B (zh) * 2021-03-31 2022-08-16 西北工业大学 一种固体火箭发动机的组合式喷管
CN114046211A (zh) * 2021-11-09 2022-02-15 北京航空航天大学 一种带有双扩张段的组合动力可调喷管
CN115095443B (zh) * 2022-06-03 2025-08-15 西北工业大学 一种带后甲板的单边膨胀双s弯喷管
CN115324775A (zh) * 2022-08-31 2022-11-11 北京星际荣耀科技有限责任公司 一种喷管结构和发动机以及飞行器
CN117267014A (zh) * 2023-10-18 2023-12-22 南京航空航天大学 一种带有和侧壁面一体化分流板的组合喷管

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2799990A (en) * 1955-12-21 1957-07-23 United Aircraft Corp Supersonic jet deflection device
US3095694A (en) * 1959-10-28 1963-07-02 Walter Hermine Johanna Reaction motors
US3210934A (en) * 1964-11-30 1965-10-12 Gen Motors Corp Jet engine exhaust
US3563467A (en) * 1966-09-07 1971-02-16 Thiokol Chemical Corp Rocket motor thrust nozzles
US3463402A (en) * 1966-12-28 1969-08-26 United Aircraft Corp Jet sound suppressing means
US4214441A (en) * 1978-09-12 1980-07-29 The United States Of America As Represented By The Secretary Of The Navy Infrared suppressor device
RU1093062C (ru) * 1982-12-30 1994-08-30 ЦАГИ им.профессора Н.Е.Жуковского Эжекторный увеличитель тяги турбореактивного двигателя
FR2618488B1 (fr) * 1987-07-20 1989-12-15 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
US5619851A (en) * 1989-02-08 1997-04-15 United Technologies Corporation Rocket nozzle for a rocket engine
DE10141108B4 (de) * 2001-08-22 2005-06-30 Eads Space Transportation Gmbh Raketentriebwerk mit geschlossenen Triebwerkskreislauf mit modularer Zuführung der Turbinenabgase

Also Published As

Publication number Publication date
ES2352445T3 (es) 2011-02-18
WO2008129372A2 (en) 2008-10-30
DE602008002737D1 (de) 2010-11-04
EP2137395A2 (de) 2009-12-30
EP2137395B1 (de) 2010-09-22
RU2326259C1 (ru) 2008-06-10
WO2008129372A3 (en) 2008-12-18

Similar Documents

Publication Publication Date Title
ATE482333T1 (de) Lavaldüse eines raketenantriebs
JP4927636B2 (ja) ガスタービンエンジンの圧力損失を減少するシステム
JP2013231576A5 (de)
JP2014181894A5 (de)
CN102235671B (zh) 具有流动套管的燃烧器
WO2008040869A3 (fr) Nacelle de réacteur d'aéronef et aéronef comportant une telle nacelle
JP2014181897A5 (de)
WO2003071117A8 (en) Ejector based engines
EP2103799A3 (de) Raketenschubdüse und Steuerungsverfahren der Abgasströmung in einem Raketentriebwerk
EP2778529A3 (de) Verbrenner für Gasturbinentriebwerk
US9938855B2 (en) Cooling system and method for supplying a cooling gas flow
JP2008169840A (ja) シンブル、スリーブ並びに燃焼器アセンブリの冷却法
JP2010209912A5 (de)
JP2014181906A5 (de)
JP2015063994A5 (de)
JP2014181899A5 (de)
EP1995443A3 (de) Verfahren und Vorrichtung zur Regelung eines Flüssigkeitsstroms durch ein Turbinentriebwerk
JP2014115072A5 (de)
JP2007120499A (ja) タービンエンジンで使用するマルチスロットのインタータービンダクトアセンブリ
RU2008147000A (ru) Топливная форсунка с изолирующей воздушной завесой
CA2580327A1 (en) Fuel conveying member with side-brazed sealing members
CN106661994B (zh) 阀导管歧管、阀导管歧管元件、运行歧管的方法及流体二极管盒元件
JP2011045877A5 (de)
RU2007137045A (ru) Переходной канал между двумя ступенями турбины
RU2005100177A (ru) Устройство для подачи охлаждающего воздуха к створкам выходного сопла

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties