IT1131033B - DRIVE SYSTEM TO BE USED IN A GAS TURBO ENGINE - Google Patents

DRIVE SYSTEM TO BE USED IN A GAS TURBO ENGINE

Info

Publication number
IT1131033B
IT1131033B IT20837/80A IT2083780A IT1131033B IT 1131033 B IT1131033 B IT 1131033B IT 20837/80 A IT20837/80 A IT 20837/80A IT 2083780 A IT2083780 A IT 2083780A IT 1131033 B IT1131033 B IT 1131033B
Authority
IT
Italy
Prior art keywords
drive system
turbo engine
gas turbo
engine
gas
Prior art date
Application number
IT20837/80A
Other languages
Italian (it)
Other versions
IT8020837A0 (en
Inventor
Dudley Owen Nash
Thomas Simmons Clayton
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 IT8020837A0 publication Critical patent/IT8020837A0/en
Application granted granted Critical
Publication of IT1131033B publication Critical patent/IT1131033B/en

Links

Classifications

    • 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
    • F02K3/075—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 controlling flow ratio between flows
    • 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)
  • Control Of Turbines (AREA)
  • Toys (AREA)
IT20837/80A 1979-04-23 1980-03-21 DRIVE SYSTEM TO BE USED IN A GAS TURBO ENGINE IT1131033B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3233079A 1979-04-23 1979-04-23

Publications (2)

Publication Number Publication Date
IT8020837A0 IT8020837A0 (en) 1980-03-21
IT1131033B true IT1131033B (en) 1986-06-18

Family

ID=21864363

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20837/80A IT1131033B (en) 1979-04-23 1980-03-21 DRIVE SYSTEM TO BE USED IN A GAS TURBO ENGINE

Country Status (6)

Country Link
JP (1) JPS55142937A (en)
DE (1) DE3015119A1 (en)
FR (1) FR2455179A1 (en)
GB (1) GB2047815B (en)
IL (1) IL59497A (en)
IT (1) IT1131033B (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58200038A (en) * 1982-05-18 1983-11-21 ゼネラル・エレクトリツク・カンパニイ Actuator for gas turbine engine
FR2527688B1 (en) * 1982-06-01 1987-03-27 Gen Electric SYSTEM FOR HANDLING AN ELEMENT MOUNTED WITHIN A CRANKCASE
US5417055A (en) * 1988-06-28 1995-05-23 Rolls-Royce Plc Valve for diverting fluid flows in turbomachines
GB8815292D0 (en) * 1988-06-28 1994-10-26 Rolls Royce Plc Valve for diverting fluid flows in turbomachines
DE3911715A1 (en) * 1989-04-10 1990-10-11 Mtu Muenchen Gmbh SHUT-OFF DEVICE FOR BLOWED, IN PARTICULAR BLOWED, RADIANT JET ENGINES
DE4004416C2 (en) * 1990-02-13 1993-10-14 Mtu Muenchen Gmbh Turbo ramjet with shut-off device for variable switching operation
US5123240A (en) * 1990-03-19 1992-06-23 General Electric Co. Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine
CA2036821A1 (en) * 1990-06-29 1991-12-30 Larry W. Stransky Bypass valve system
GB2259328B (en) * 1991-09-03 1995-07-19 Gen Electric Gas turbine engine variable bleed pivotal flow splitter
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
US6742324B2 (en) * 2002-09-13 2004-06-01 General Electric Company Methods and apparatus for supporting variable bypass valve systems
US6901739B2 (en) * 2003-10-07 2005-06-07 General Electric Company Gas turbine engine with variable pressure ratio fan system
FR2926328B1 (en) * 2008-01-14 2015-08-07 Snecma DOUBLE FLOW TURBOMACHINE COMPRISING A PRIMARY VEIN AND A MOBILE SPOUT IN THIS PRIMARY VEIN
US20120070271A1 (en) 2010-09-21 2012-03-22 Urban Justin R Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events
US8935926B2 (en) 2010-10-28 2015-01-20 United Technologies Corporation Centrifugal compressor with bleed flow splitter for a gas turbine engine
DE102011101331A1 (en) 2011-05-12 2012-11-15 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine engine with bleed air extraction device
CN109162829B (en) * 2018-09-04 2019-08-23 中国航发沈阳发动机研究所 The compressibility of variable cycle engine
CN111636978B (en) * 2020-06-16 2021-06-18 南京航空航天大学 Flow regulating mechanism suitable for turbine-based circulating combined engine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
GB864519A (en) * 1958-08-05 1961-04-06 Rolls Royce Improved annular fluid control valve device
US2934895A (en) * 1958-09-15 1960-05-03 Curtiss Wright Corp Dual cycle engine distributor construction
US3153904A (en) * 1961-12-29 1964-10-27 Stanley H Ellis Turbo-ramjet configuration
GB1124169A (en) * 1967-04-07 1968-08-21 Rolls Royce Mechanism e.g. for use in a jet nozzle
GB1300405A (en) * 1969-06-25 1972-12-20 Secr Defence Improvements in nozzles for gas turbine jet propulsion engines
FR2085470B1 (en) * 1970-04-23 1974-05-03 Snecma
US3638428A (en) * 1970-05-04 1972-02-01 Gen Electric Bypass valve mechanism
DE2247400C2 (en) * 1972-09-27 1975-01-16 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Device for blowing off compressed air from a compressor of a gas turbine jet engine
US4175384A (en) * 1977-08-02 1979-11-27 General Electric Company Individual bypass injector valves for a double bypass variable cycle turbofan engine
DE2740904A1 (en) * 1977-09-10 1979-03-22 Motoren Turbinen Union DEVICE FOR OPERATING SHUT-OFF ELEMENTS IN GAS TURBINE ENGINES, IN PARTICULAR GAS TURBINE JET

Also Published As

Publication number Publication date
IT8020837A0 (en) 1980-03-21
IL59497A (en) 1984-08-31
JPS642774B2 (en) 1989-01-18
GB2047815B (en) 1983-03-30
IL59497A0 (en) 1980-05-30
FR2455179A1 (en) 1980-11-21
GB2047815A (en) 1980-12-03
JPS55142937A (en) 1980-11-07
DE3015119A1 (en) 1980-11-06
FR2455179B1 (en) 1984-07-20

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19930323