DE2410142A1 - Konvergent-divergente auslassduese mit variablem querschnitt - Google Patents

Konvergent-divergente auslassduese mit variablem querschnitt

Info

Publication number
DE2410142A1
DE2410142A1 DE2410142A DE2410142A DE2410142A1 DE 2410142 A1 DE2410142 A1 DE 2410142A1 DE 2410142 A DE2410142 A DE 2410142A DE 2410142 A DE2410142 A DE 2410142A DE 2410142 A1 DE2410142 A1 DE 2410142A1
Authority
DE
Germany
Prior art keywords
primary
flaps
connecting ring
outlet nozzle
downstream
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
DE2410142A
Other languages
German (de)
English (en)
Inventor
Charles Henry Gross
Jun Arthur Mccardle
Robert Lee Sponseller
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE2410142A1 publication Critical patent/DE2410142A1/de
Pending 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
    • 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • 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
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/323—Arrangement of components according to their shape convergent
    • 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
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
DE2410142A 1973-06-18 1974-03-02 Konvergent-divergente auslassduese mit variablem querschnitt Pending DE2410142A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00371056A US3814325A (en) 1973-06-18 1973-06-18 Variable area convergent-divergent exhaust nozzle

Publications (1)

Publication Number Publication Date
DE2410142A1 true DE2410142A1 (de) 1975-01-09

Family

ID=23462294

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2410142A Pending DE2410142A1 (de) 1973-06-18 1974-03-02 Konvergent-divergente auslassduese mit variablem querschnitt

Country Status (8)

Country Link
US (1) US3814325A (enExample)
JP (1) JPS5026905A (enExample)
BE (1) BE812513A (enExample)
CA (1) CA994114A (enExample)
DE (1) DE2410142A1 (enExample)
FR (1) FR2233499B3 (enExample)
GB (1) GB1456280A (enExample)
IT (1) IT1007851B (enExample)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3931708A (en) * 1973-10-11 1976-01-13 United Technologies Corporation Variable flap for a variable pitch ducted fan propulsor
US4141501A (en) * 1975-05-09 1979-02-27 Rolls-Royce (1971) Limited Nozzles for gas turbine engines
GB1533986A (en) * 1976-04-12 1978-11-29 Rolls Royce Nozzles for gas turbine engines
FR2724977B1 (fr) * 1980-12-30 1996-12-13 Snecma Tuyere convergente-divergente en particulier pour turboreacteur
US4587806A (en) * 1981-05-11 1986-05-13 United Technologies Corporation Area two-dimensional converging/diverging nozzle
US4527388A (en) * 1982-07-12 1985-07-09 The Garrett Corporation Jet propulsion apparatus and methods
US5201800A (en) * 1990-02-26 1993-04-13 General Electric Company Method for discharging combustion gases from an exhaust nozzle
US5103639A (en) * 1990-02-26 1992-04-14 General Electric Company Exhaust nozzle having variable contour exhaust flap
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
US5239815A (en) * 1991-09-23 1993-08-31 United Technologies Corporation Sync-ring assembly for a gas turbine engine exhaust nozzle
US5245823A (en) * 1991-09-23 1993-09-21 United Technologies Corporation External flap vectoring mechanism
FR2691508B1 (fr) * 1992-05-20 1994-07-08 Snecma Verin a fluide sous pression et tuyere a section variable en faisant application.
US5431344A (en) * 1993-11-12 1995-07-11 United Technologies Corporation Sliding throat gas turbine engine nozzle
US5806302A (en) * 1996-09-24 1998-09-15 Rohr, Inc. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
RU2238419C1 (ru) * 2003-06-04 2004-10-20 Государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" - дочернее предприятие Федерального государственного унитарного предприятия "Российская самолетостроительная корпорация "МиГ" Устройство для снятия характеристик вентилятора в составе двухконтурного турбореактивного двигателя с раздельными соплами внешнего и внутреннего контура
GB2449477B (en) * 2007-05-24 2009-05-13 Rolls Royce Plc A duct installation
US7874160B2 (en) * 2007-08-21 2011-01-25 United Technologies Corporation Nozzle-area ratio float bias
US8020386B2 (en) * 2007-08-21 2011-09-20 United Technologies Corporation Rollertrack pivoting axi-nozzle
US8127532B2 (en) 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
US8959889B2 (en) 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
US8572986B2 (en) * 2009-07-27 2013-11-05 United Technologies Corporation Retainer for suspended thermal protection elements in a gas turbine engine
FR2970519B1 (fr) * 2011-01-14 2013-03-22 Snecma Volet interne commande, tuyere le comprenant, turbomachine d'aeronef comprenant une telle tuyere
US8443931B2 (en) 2011-04-06 2013-05-21 Lockheed Martin Corporation Noise reduction of supersonic jet engines
US9810085B2 (en) * 2011-08-22 2017-11-07 United Technologies Corporation Flap seal for gas turbine engine movable nozzle flap
EP2971657B1 (en) * 2013-03-12 2021-08-04 Raytheon Technologies Corporation Expanding shell flow control device
GB2588652A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
GB2588651A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
GB2588653A (en) * 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
US11661905B1 (en) * 2022-01-17 2023-05-30 Florida Turbine Technologies, Inc. 2D variable-area plug nozzle
CN120840874A (zh) 2022-04-29 2025-10-28 湾流航空航天公司 用于与推进系统一起使用的喷嘴组件

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044258A (en) * 1958-11-25 1962-07-17 Gen Electric Adjustable converging-diverging nozzle
US3038304A (en) * 1959-04-17 1962-06-12 Gen Electric Variable exhaust nozzle configuration
GB951130A (en) * 1961-07-28 1964-03-04 Rolls Royce Improvements relating to jet engines
US3403858A (en) * 1967-03-31 1968-10-01 United Aircraft Corp Exhaust nozzle actuation system
US3599875A (en) * 1969-02-10 1971-08-17 United Aircraft Corp Translating air scoop ejector nozzle
DE1936800C3 (de) * 1969-07-19 1975-08-07 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Hinsichtlich ihres Austrittsquerschnitts änderbare konvergente Schubdüse für ein Gasturbinenstrahltriebwerk
US3592389A (en) * 1969-11-24 1971-07-13 Gen Motors Corp Flap linkage
US3662957A (en) * 1970-10-28 1972-05-16 United Aircraft Corp Low friction track bearing assembly

Also Published As

Publication number Publication date
US3814325A (en) 1974-06-04
GB1456280A (en) 1976-11-24
BE812513A (fr) 1974-07-15
CA994114A (en) 1976-08-03
JPS5026905A (enExample) 1975-03-20
IT1007851B (it) 1976-10-30
FR2233499B3 (enExample) 1976-12-24
FR2233499A1 (enExample) 1975-01-10

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