CN1322275A - 用于对气流分散进行控制并且减小边载荷的火箭发动机喷管轮廓 - Google Patents

用于对气流分散进行控制并且减小边载荷的火箭发动机喷管轮廓

Info

Publication number
CN1322275A
CN1322275A CN98814321A CN98814321A CN1322275A CN 1322275 A CN1322275 A CN 1322275A CN 98814321 A CN98814321 A CN 98814321A CN 98814321 A CN98814321 A CN 98814321A CN 1322275 A CN1322275 A CN 1322275A
Authority
CN
China
Prior art keywords
shape
nozzle
engine
derivative
contour
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CN98814321A
Other languages
English (en)
Chinese (zh)
Inventor
扬·海根德
扬·马特松
马茨·奥洛夫松
约翰·安加德
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero AB
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 Volvo Aero AB filed Critical Volvo Aero AB
Publication of CN1322275A publication Critical patent/CN1322275A/zh
Pending legal-status Critical Current

Links

Images

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
    • F02K9/97—Rocket nozzles
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/16—Two-dimensional parabolic

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Testing Of Engines (AREA)
  • Control Of Turbines (AREA)
CN98814321A 1998-12-04 1998-12-04 用于对气流分散进行控制并且减小边载荷的火箭发动机喷管轮廓 Pending CN1322275A (zh)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SE1998/002222 WO2000034641A1 (en) 1998-12-04 1998-12-04 Rocket nozzle contour for flow separation control and side load reduction

Publications (1)

Publication Number Publication Date
CN1322275A true CN1322275A (zh) 2001-11-14

Family

ID=20411802

Family Applications (1)

Application Number Title Priority Date Filing Date
CN98814321A Pending CN1322275A (zh) 1998-12-04 1998-12-04 用于对气流分散进行控制并且减小边载荷的火箭发动机喷管轮廓

Country Status (7)

Country Link
US (1) US6574964B1 (enExample)
EP (1) EP1135588A1 (enExample)
JP (1) JP2002531766A (enExample)
CN (1) CN1322275A (enExample)
RU (1) RU2209333C2 (enExample)
UA (1) UA46175C2 (enExample)
WO (1) WO2000034641A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11359842B2 (en) 2019-03-27 2022-06-14 Lg Electronics Inc. Air conditioning apparatus

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2196917C1 (ru) * 2002-02-06 2003-01-20 Федеральное государственное унитарное предприятие "Исследовательский Центр им. М.В. Келдыша" Камера жидкостного ракетного двигателя
RU2215171C1 (ru) * 2002-03-19 2003-10-27 Открытое акционерное общество Научно-производственное объединение "Искра" Сопло ракетного двигателя твердого топлива
FR2882401B1 (fr) * 2005-02-22 2007-05-11 Agence Spatiale Europeenne Dispositif et procede pour reduire les forces laterales non stationnaires agissant sur une tuyere d'un moteur de fusee
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
DE102010042890B4 (de) * 2010-10-25 2020-07-30 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerksvorrichtung für einen Flugkörper, Prüfstand oder Startrampe für einen Flugkörper und Verfahren zur Reduzierung einer Seitenlast bei einer Triebwerksvorrichtung
AT511466B1 (de) 2011-08-03 2012-12-15 Hoerbiger Kompressortech Hold Fluidmischer
US9009966B2 (en) * 2013-03-15 2015-04-21 Northrop Gurmman Systems Corporation Internal/external single expansion ramp nozzle with integrated third stream
RU2531161C1 (ru) * 2013-04-24 2014-10-20 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Осесимметричное сопло ракетного двигателя
RU2552020C2 (ru) * 2013-09-23 2015-06-10 Государственный научный центр Российской Федерации-федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" Сопло ракетного двигателя
DE102015011958B4 (de) * 2015-09-18 2024-02-01 Arianegroup Gmbh Schubdüse

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3352495A (en) * 1965-01-29 1967-11-14 Thiokol Chemical Corp Nozzle construction
US3394549A (en) 1965-07-06 1968-07-30 North American Rockwell Step nozzle
FR2602275B1 (fr) * 1986-08-04 1990-08-10 Onera (Off Nat Aerospatiale) Perfectionnements aux tuyeres de propulseurs pour reduction d'efforts lateraux
FR2618488B1 (fr) 1987-07-20 1989-12-15 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
RU2095609C1 (ru) * 1989-08-03 1997-11-10 Конструкторское бюро "Химавтоматики" Сопло камеры жидкостного ракетного двигателя
US6324833B1 (en) * 1990-04-24 2001-12-04 Cordant Technologies, Inc. Reinforced composite articles and method of making same
FR2705737B1 (fr) 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à divergent échancré.
FR2705739B1 (fr) 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à section de sortie sélectivement réduite.
US6176077B1 (en) * 1996-02-12 2001-01-23 Volvo Aero Corporation Rocket engine nozzle
NL1004193C2 (nl) 1996-04-01 1997-10-02 Sjoerd Meijer Werkwijze voor het bewerken van metaalplaat.
JP3924326B2 (ja) * 1996-09-23 2007-06-06 ボルボ エアロ コーポレイション 制御された温度ロケットノズル
RU2117814C1 (ru) * 1996-10-30 1998-08-20 Владимир Ильич Масютин Оптимальное сопло жидкостного ракетного двигателя ракет стратегического назначения
DE19755732C2 (de) 1997-12-15 2000-01-13 Waeschle Gmbh Verfahren zum Herstellen von Granulaten aus polymeren Werkstoffen

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11359842B2 (en) 2019-03-27 2022-06-14 Lg Electronics Inc. Air conditioning apparatus

Also Published As

Publication number Publication date
EP1135588A1 (en) 2001-09-26
UA46175C2 (uk) 2002-05-15
JP2002531766A (ja) 2002-09-24
US6574964B1 (en) 2003-06-10
RU2209333C2 (ru) 2003-07-27
WO2000034641A1 (en) 2000-06-15

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication