DE1526815A1 - Zweikreisturbinentriebwerk - Google Patents

Zweikreisturbinentriebwerk

Info

Publication number
DE1526815A1
DE1526815A1 DE19651526815 DE1526815A DE1526815A1 DE 1526815 A1 DE1526815 A1 DE 1526815A1 DE 19651526815 DE19651526815 DE 19651526815 DE 1526815 A DE1526815 A DE 1526815A DE 1526815 A1 DE1526815 A1 DE 1526815A1
Authority
DE
Germany
Prior art keywords
engine
compressor
struts
blades
fan
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
DE19651526815
Other languages
German (de)
English (en)
Inventor
Dibble Charles Gordon Ferguson
Fisher Lee Joseph
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 DE1526815A1 publication Critical patent/DE1526815A1/de
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE19651526815 1964-12-02 1965-11-20 Zweikreisturbinentriebwerk Pending DE1526815A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US41668164A 1964-12-02 1964-12-02
US41668064A 1964-12-02 1964-12-02

Publications (1)

Publication Number Publication Date
DE1526815A1 true DE1526815A1 (de) 1971-01-28

Family

ID=27023449

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19651526815 Pending DE1526815A1 (de) 1964-12-02 1965-11-20 Zweikreisturbinentriebwerk

Country Status (3)

Country Link
DE (1) DE1526815A1 (sv)
GB (1) GB1197711A (sv)
SE (1) SE333275B (sv)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008013542A1 (de) 2008-03-11 2009-09-17 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit mehrstromiger Rotoranordnung

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4704862A (en) * 1985-05-29 1987-11-10 United Technologies Corporation Ducted prop engine
ATE371097T1 (de) * 1998-02-26 2007-09-15 Allison Advanced Dev Co Zapfsystem für eine kompressorwand sowie betriebsverfahren
DE102004042739A1 (de) * 2004-09-03 2006-03-09 Mtu Aero Engines Gmbh Fan für ein Flugtriebwerk sowie Flugtriebwerk
FR2966126B1 (fr) * 2010-10-15 2013-06-28 Airbus Operations Sas Nacelle d'aeronef incorporant un cadre arriere incline vers l'arriere
US10267160B2 (en) * 2015-08-27 2019-04-23 Rolls-Royce North American Technologies Inc. Methods of creating fluidic barriers in turbine engines
GB201813675D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813671D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813672D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813674D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813670D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201820400D0 (en) * 2018-12-14 2019-01-30 Rolls Royce Plc Ice crystal protection for a gas turbine engine
CN110005544A (zh) * 2019-05-12 2019-07-12 西北工业大学 自驱动外涵道环形扇叶压缩装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008013542A1 (de) 2008-03-11 2009-09-17 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit mehrstromiger Rotoranordnung

Also Published As

Publication number Publication date
GB1197711A (en) 1970-07-08
SE333275B (sv) 1971-03-08

Similar Documents

Publication Publication Date Title
DE1526815A1 (de) Zweikreisturbinentriebwerk
DE60312817T2 (de) Turbofandüse und Geräuschminderungsverfahren in einer solchen Düse
DE69922443T2 (de) Berstschutzring für eine Gasturbine
DE4039810C1 (sv)
DE3940981C2 (de) Auswuchtgewicht zum Auswuchten des Rotors eines Gasturbinentriebwerks
DE60220636T2 (de) Gasturbine mit gegenläufigen Niederdruckrotoren
DE69824817T2 (de) Frequenzabgestimmte Turbomaschinenschaufel
EP0680557B1 (de) Turbinenstrahltriebwerk mit gebläse oder prop-fan
DE3812027A1 (de) Propfan-turbotriebwerk
DE3614157C2 (de) Gasturbinentriebwerk mit gegenläufigen Propellern
DE3338456A1 (de) Gasturbinentriebwerk
DE3703502A1 (de) Ringfluegel- bzw. -geblaesestrahltriebwerk
DE1911076A1 (de) Kompressor und Turbinenstrahltriebwerk
DE602004005906T2 (de) Gekrümmte Schaufel für Strahltriebwerk
DE2454054A1 (de) Innentriebwerk bzw. gasgenerator fuer gasturbinentriebwerke
DE2549771A1 (de) Gasturbinentriebwerk mit konvertiblen zubehoerteilen
DE2353042A1 (de) Vorrichtung zur laermverminderung bei strahltriebwerken
DE2507797A1 (de) Verkleidungsanordnung fuer turbofan- triebwerk
DE2644066A1 (de) Tragfluegelprofilstruktur mit abbrechkante
DE1601561A1 (de) Gekuehlte Schaufel fuer mit hohen Temperaturen arbeitendes Turbinentriebwerk
DE1628376A1 (de) Axialverdichter
WO2002081883A2 (de) Nebenstrom-strahltriebwerk für den vorausantrieb von luftfahrzeugen
WO2019121022A1 (de) Schubdüse für ein turbofan-triebwerk eines überschallflugzeugs
EP3306066A1 (de) Turbofan-triebwerk für ein ziviles überschallflugzeug
DE102011113205A1 (de) Rotoranordnung