DE1526818A1 - Konvergente-divergente Duese mit Duesenmittelkoerper - Google Patents

Konvergente-divergente Duese mit Duesenmittelkoerper

Info

Publication number
DE1526818A1
DE1526818A1 DE19661526818 DE1526818A DE1526818A1 DE 1526818 A1 DE1526818 A1 DE 1526818A1 DE 19661526818 DE19661526818 DE 19661526818 DE 1526818 A DE1526818 A DE 1526818A DE 1526818 A1 DE1526818 A1 DE 1526818A1
Authority
DE
Germany
Prior art keywords
flaps
nozzle
center body
section
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
DE19661526818
Other languages
German (de)
English (en)
Inventor
Rabone George Roger
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 DE1526818A1 publication Critical patent/DE1526818A1/de
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1269Varying 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/08Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/32Arrangement of components according to their shape
    • F05D2250/323Arrangement of components according to their shape convergent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/32Arrangement of components according to their shape
    • F05D2250/324Arrangement 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)
  • Supercharger (AREA)
DE19661526818 1965-12-08 1966-07-30 Konvergente-divergente Duese mit Duesenmittelkoerper Pending DE1526818A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US51241665A 1965-12-08 1965-12-08

Publications (1)

Publication Number Publication Date
DE1526818A1 true DE1526818A1 (de) 1970-03-19

Family

ID=24038988

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19661526818 Pending DE1526818A1 (de) 1965-12-08 1966-07-30 Konvergente-divergente Duese mit Duesenmittelkoerper

Country Status (3)

Country Link
BE (1) BE685446A (fr)
DE (1) DE1526818A1 (fr)
GB (1) GB1111195A (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4012212A1 (de) * 1990-04-14 1991-10-24 Mtu Muenchen Gmbh Duese fuer ein hyperschalltriebwerk
CN114776462B (zh) * 2022-04-14 2024-06-18 中国航发沈阳发动机研究所 一种喉道可调单边膨胀喷管
CN114776465A (zh) * 2022-05-25 2022-07-22 厦门大学 一种基于旋转爆震发动机的可调塞式喷管

Also Published As

Publication number Publication date
BE685446A (fr) 1967-01-16
GB1111195A (en) 1968-04-24

Similar Documents

Publication Publication Date Title
DE970090C (de) Rueckstossduese fuer Rueckstosstriebwerke
DE60312817T2 (de) Turbofandüse und Geräuschminderungsverfahren in einer solchen Düse
DE2638883C2 (de) Schubdüse
DE2042026A1 (de) Antriebsduese mit Schalldaempfungseinrichtung
EP3388649B1 (fr) Nacelle de moteur pour une turbosoufflante
DE1456037B1 (de) Schubumkehreinrichtung für ein Strahltriebwerk
DE2507797A1 (de) Verkleidungsanordnung fuer turbofan- triebwerk
DE2410142A1 (de) Konvergent-divergente auslassduese mit variablem querschnitt
DE1526821A1 (de) Konvergente-divergente Strahltriebwerksaustrittsduese
DE2638873A1 (de) Ausstroemduese mit austrittskonus in ringform fuer variablen betriebszyklus und verfahren zum betrieb derselben
DE102016118783A1 (de) Turbofan-Triebwerk für ein ziviles Überschallflugzeug
DE1526817A1 (de) Konvergente-divergente Strahltriebswerksaustrittsduese
CH373228A (de) Rückstosstriebwerk für Überschall-Fluggeschwindigkeit
DE1286334B (de) UEberschallschubduese fuer Gasturbinenstrahltriebwerke
DE1943403A1 (de) Schubumkehrvorrichtung fuer Gasturbinenstrahltriebwerke
DE102017130568A1 (de) Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs
DE2638882A1 (de) Ausstroemduese mit austrittskonus und klappe fuer variablen betriebszyklus und verfahren zum betrieb derselben
DE69627713T2 (de) Betätigungssystem für eine strahldüse mit schubvektorsteuerung mit mehreren hydraulischen kreisläufen
DE1182475B (de) Schubduese fuer die Abgase eines Strahltriebwerkes
DE4004416C2 (de) Turbo-Staustrahltriebwerk mit Absperreinrichtung für variablen Umschaltbetrieb
DE2629049A1 (de) Duese mit variablem querschnitt und belastungsausgleich
DE1526818A1 (de) Konvergente-divergente Duese mit Duesenmittelkoerper
DE102017104036A1 (de) Konvergent-divergente Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs und Verfahren zur Einstellung der Düsenhalsfläche in einer Schubdüse eines Turbofan-Triebwerks
DE1526823A1 (de) Konvergente-divergente Duesenstrahlaustrittsduese fuer UEberschallbetrieb
DE1526851A1 (de) Strahlduese