BE687557A - - Google Patents

Info

Publication number
BE687557A
BE687557A BE687557DA BE687557A BE 687557 A BE687557 A BE 687557A BE 687557D A BE687557D A BE 687557DA BE 687557 A BE687557 A BE 687557A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE687557A publication Critical patent/BE687557A/xx

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
    • F02K1/1269—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the internal downstream series having its flaps hinged at their downstream ends on the downstream ends of the flaps of the external downstream series hinged on a fixed structure at their upstream ends
    • 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

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)
BE687557D 1965-12-30 1966-09-29 BE687557A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US517543A US3398896A (en) 1965-12-30 1965-12-30 Supersionic convergent-divergent jet exhaust nozzles

Publications (1)

Publication Number Publication Date
BE687557A true BE687557A (xx) 1967-03-01

Family

ID=24060237

Family Applications (1)

Application Number Title Priority Date Filing Date
BE687557D BE687557A (xx) 1965-12-30 1966-09-29

Country Status (4)

Country Link
US (1) US3398896A (xx)
BE (1) BE687557A (xx)
DE (1) DE1526823A1 (xx)
GB (1) GB1116999A (xx)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115253495A (zh) * 2022-07-27 2022-11-01 国能龙源环保南京有限公司 烟气脱硫系统用灰斗流化装置和流化灰循环方法

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4000854A (en) * 1975-10-02 1977-01-04 General Electric Company Thrust vectorable exhaust nozzle
US4420932A (en) * 1982-03-02 1983-12-20 The United States Of America As Represented By The Secretary Of The Air Force Pressure control system for convergent-divergent exhaust nozzle
GB2194597B (en) * 1986-08-29 1990-07-25 Rolls Royce Plc A variable area exhaust nozzle for a gas turbine engine
US6164059A (en) * 1995-11-17 2000-12-26 United Technologies Corporation Multi-expansion ejector nozzle with diverging walls
US5842643A (en) * 1996-12-03 1998-12-01 General Electric Company Articulated exhaust nozzle fairing
GB0504272D0 (en) * 2005-03-02 2005-04-06 Rolls Royce Plc A turbine engine and a method of operating a turbine engine
DE102017104043A1 (de) * 2017-02-27 2018-08-30 Rolls-Royce Deutschland Ltd & Co Kg Konvergent-divergente Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs und Verfahren zur Reduzierung des Heckwiderstands hinter einer solchen Schubdüse
CN112727634B (zh) * 2020-12-07 2022-08-16 西安航天动力研究所 一种矩形截面喷管

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2926491A (en) * 1958-08-25 1960-03-01 Orenda Engines Ltd Actuating means for variable nozzles
US3214905A (en) * 1960-11-28 1965-11-02 Gen Electric Variable area convergent-divergent nozzle
US3214904A (en) * 1960-11-28 1965-11-02 Gen Electric Variable area convergent-divergent nozzle and actuation system therefor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115253495A (zh) * 2022-07-27 2022-11-01 国能龙源环保南京有限公司 烟气脱硫系统用灰斗流化装置和流化灰循环方法
CN115253495B (zh) * 2022-07-27 2024-07-02 国能龙源环保南京有限公司 烟气脱硫系统用灰斗流化装置和流化灰循环方法

Also Published As

Publication number Publication date
DE1526823A1 (de) 1970-03-19
US3398896A (en) 1968-08-27
GB1116999A (en) 1968-06-12

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