SE333275B - Axialkompressor foer dubbelstroemsmotor - Google Patents

Axialkompressor foer dubbelstroemsmotor

Info

Publication number
SE333275B
SE333275B SE15612/65A SE1561265A SE333275B SE 333275 B SE333275 B SE 333275B SE 15612/65 A SE15612/65 A SE 15612/65A SE 1561265 A SE1561265 A SE 1561265A SE 333275 B SE333275 B SE 333275B
Authority
SE
Sweden
Prior art keywords
current engine
axial compressor
dual current
dual
compressor
Prior art date
Application number
SE15612/65A
Other languages
English (en)
Inventor
C Dibble
D Howard
L Fischer
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SE333275B publication Critical patent/SE333275B/sv

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/022Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/20Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/64Reversing fan flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/06Plants 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
SE15612/65A 1964-12-02 1965-12-02 Axialkompressor foer dubbelstroemsmotor SE333275B (sv)

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
SE333275B true SE333275B (sv) 1971-03-08

Family

ID=27023449

Family Applications (1)

Application Number Title Priority Date Filing Date
SE15612/65A SE333275B (sv) 1964-12-02 1965-12-02 Axialkompressor foer dubbelstroemsmotor

Country Status (3)

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

Families Citing this family (13)

* 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
DE102008013542A1 (de) 2008-03-11 2009-09-17 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit mehrstromiger Rotoranordnung
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

Also Published As

Publication number Publication date
GB1197711A (en) 1970-07-08
DE1526815A1 (de) 1971-01-28

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