GB2243877A - Adjustable nozzle for hypersonic engine combustion chamber - Google Patents

Adjustable nozzle for hypersonic engine combustion chamber Download PDF

Info

Publication number
GB2243877A
GB2243877A GB9106049A GB9106049A GB2243877A GB 2243877 A GB2243877 A GB 2243877A GB 9106049 A GB9106049 A GB 9106049A GB 9106049 A GB9106049 A GB 9106049A GB 2243877 A GB2243877 A GB 2243877A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
wall
engine
section
cross
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.)
Withdrawn
Application number
GB9106049A
Other languages
English (en)
Other versions
GB9106049D0 (en
Inventor
Joachim Kretschmer
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB9106049D0 publication Critical patent/GB9106049D0/en
Publication of GB2243877A publication Critical patent/GB2243877A/en
Withdrawn legal-status Critical Current

Links

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
    • F02K9/60—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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
GB9106049A 1990-03-31 1991-03-21 Adjustable nozzle for hypersonic engine combustion chamber Withdrawn GB2243877A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4010471A DE4010471A1 (de) 1990-03-31 1990-03-31 Brennkammer mit duese fuer einen hyperschallantrieb

Publications (2)

Publication Number Publication Date
GB9106049D0 GB9106049D0 (en) 1991-05-08
GB2243877A true GB2243877A (en) 1991-11-13

Family

ID=6403526

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9106049A Withdrawn GB2243877A (en) 1990-03-31 1991-03-21 Adjustable nozzle for hypersonic engine combustion chamber

Country Status (4)

Country Link
DE (1) DE4010471A1 (de)
FR (1) FR2660416A1 (de)
GB (1) GB2243877A (de)
IT (1) IT1245582B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10094336B2 (en) 2014-04-17 2018-10-09 Raytheon Company Articulated diffuser and door for submerged ram air turbine power and cooling control

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4222947C2 (de) * 1992-07-11 1995-02-02 Deutsche Aerospace Strahltriebwerk
DE4237860A1 (de) * 1992-11-10 1994-05-11 Schlafhorst & Co W Fadenführungstrommel
DE10208161A1 (de) * 2002-02-26 2003-09-18 Alban Geissler Düsenantriebssystem
CN107120210B (zh) * 2017-06-25 2023-05-23 北京航天三发高科技有限公司 一种超音速喷管
CN115183269B (zh) * 2022-07-21 2023-06-20 中国航发沈阳发动机研究所 一种采用陶瓷基叶片和整流支板整流的加力燃烧室

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB757457A (en) * 1953-09-10 1956-09-19 Snecma Rocket control
GB875496A (en) * 1959-12-07 1961-08-23 Gen Electric Improvements in or relating to ducted-fan gas turbine jet propulsion engines
GB1044243A (en) * 1965-04-20 1966-09-28 Rolls Royce Jet propulsion engines
GB1069872A (en) * 1963-02-19 1967-05-24 Bristol Siddeley Engines Ltd Engine fuel supply systems
GB1114181A (en) * 1964-05-28 1968-05-15 Bristol Siddeley Engines Ltd Fuel control systems for aircraft
GB1132236A (en) * 1965-08-03 1968-10-30 Mini Of Technology Supersonic fluid flow exhaust nozzles
GB1417504A (en) * 1972-05-02 1975-12-10 Snecma Variable-geometry nozzles for jet propulsion engines

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB805418A (en) * 1955-10-05 1958-12-03 Power Jets Res & Dev Ltd Jet propulsion plant
US3060679A (en) * 1958-10-24 1962-10-30 Gen Electric Powerplant
US3192712A (en) * 1962-12-31 1965-07-06 Gen Electric Load balancing arrangement for annular variable area jet exhaust nozzle
DE1892865U (de) * 1963-01-08 1964-05-14 Bristol Siddeley Engines Ltd Strahltriebwerk.
DE2255306C3 (de) * 1972-11-11 1975-06-12 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Aerodynamische Flammenhalterung für luftatmende Strahltriebwerke

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB757457A (en) * 1953-09-10 1956-09-19 Snecma Rocket control
GB875496A (en) * 1959-12-07 1961-08-23 Gen Electric Improvements in or relating to ducted-fan gas turbine jet propulsion engines
GB1069872A (en) * 1963-02-19 1967-05-24 Bristol Siddeley Engines Ltd Engine fuel supply systems
GB1114181A (en) * 1964-05-28 1968-05-15 Bristol Siddeley Engines Ltd Fuel control systems for aircraft
GB1044243A (en) * 1965-04-20 1966-09-28 Rolls Royce Jet propulsion engines
GB1132236A (en) * 1965-08-03 1968-10-30 Mini Of Technology Supersonic fluid flow exhaust nozzles
GB1417504A (en) * 1972-05-02 1975-12-10 Snecma Variable-geometry nozzles for jet propulsion engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10094336B2 (en) 2014-04-17 2018-10-09 Raytheon Company Articulated diffuser and door for submerged ram air turbine power and cooling control

Also Published As

Publication number Publication date
ITMI910790A1 (it) 1992-09-22
FR2660416A1 (fr) 1991-10-04
GB9106049D0 (en) 1991-05-08
DE4010471C2 (de) 1992-11-19
ITMI910790A0 (it) 1991-03-22
IT1245582B (it) 1994-09-29
DE4010471A1 (de) 1991-10-02

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)