IT1183454B - COOLING AIR CONTROL SYSTEM FOR GAS TURBO ENGINE - Google Patents

COOLING AIR CONTROL SYSTEM FOR GAS TURBO ENGINE

Info

Publication number
IT1183454B
IT1183454B IT19738/85A IT1973885A IT1183454B IT 1183454 B IT1183454 B IT 1183454B IT 19738/85 A IT19738/85 A IT 19738/85A IT 1973885 A IT1973885 A IT 1973885A IT 1183454 B IT1183454 B IT 1183454B
Authority
IT
Italy
Prior art keywords
control system
cooling air
air control
turbo engine
gas turbo
Prior art date
Application number
IT19738/85A
Other languages
Italian (it)
Other versions
IT8519738A0 (en
Inventor
Gary Craig Wollenweber
Tseng Wu-Yang
Thomas John Sullivan
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 IT8519738A0 publication Critical patent/IT8519738A0/en
Application granted granted Critical
Publication of IT1183454B publication Critical patent/IT1183454B/en

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
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/084—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades the fluid circulating at the periphery of a multistage rotor, e.g. of drum type
    • 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
IT19738/85A 1984-03-02 1985-03-01 COOLING AIR CONTROL SYSTEM FOR GAS TURBO ENGINE IT1183454B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US58582084A 1984-03-02 1984-03-02

Publications (2)

Publication Number Publication Date
IT8519738A0 IT8519738A0 (en) 1985-03-01
IT1183454B true IT1183454B (en) 1987-10-22

Family

ID=24343091

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19738/85A IT1183454B (en) 1984-03-02 1985-03-01 COOLING AIR CONTROL SYSTEM FOR GAS TURBO ENGINE

Country Status (7)

Country Link
JP (1) JPS60228731A (en)
CA (1) CA1233125A (en)
DE (1) DE3507036A1 (en)
FR (1) FR2560639B1 (en)
GB (1) GB2155114B (en)
IT (1) IT1183454B (en)
SE (1) SE458544B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4732538A (en) * 1984-03-02 1988-03-22 General Electric Company Blade hub air scoop
US5039278A (en) * 1989-04-11 1991-08-13 General Electric Company Power turbine ventilation system
ITBO20050197A1 (en) 2005-03-25 2006-09-26 Omt Off Mecc Tartarini PRESSURE REGULATOR FOR GAS AND RELATED ASSEMBLY AND DISASSEMBLY METHOD
US10221706B2 (en) * 2015-11-17 2019-03-05 General Electric Company Variable pitch fan actuator

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745501A (en) * 1952-03-13 1956-05-15 Gen Motors Corp Propeller spinner assembly
US3870434A (en) * 1973-12-21 1975-03-11 Gen Electric Gear arrangement for variable pitch fan
US4046435A (en) * 1975-07-14 1977-09-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Bearing seat usable in a gas turbine engine

Also Published As

Publication number Publication date
CA1233125A (en) 1988-02-23
IT8519738A0 (en) 1985-03-01
SE8500989L (en) 1985-09-03
GB2155114A (en) 1985-09-18
FR2560639B1 (en) 1988-12-02
GB2155114B (en) 1988-04-07
SE8500989D0 (en) 1985-02-28
DE3507036A1 (en) 1985-09-12
SE458544B (en) 1989-04-10
GB8505194D0 (en) 1985-04-03
JPS60228731A (en) 1985-11-14
FR2560639A1 (en) 1985-09-06
JPH0585736B2 (en) 1993-12-08

Similar Documents

Publication Publication Date Title
IT1135606B (en) AUXILIARY VENTILATION SYSTEM FOR GAS TURBO ENGINES
IT1177449B (en) GAS TURBO ENGINE COMPONENT COOLING SYSTEM
IT1208034B (en) VORTEX DISTRIBUTOR FOR A GAS TURBO ENGINE COOLING SYSTEM.
GB2108202B (en) Air cooling systems for gas turbine engines
IT1137928B (en) GAME CONTROL SYSTEM FOR GAS TURBO ENGINES
IT1131511B (en) CONTROL SYSTEM FOR GAS TURBO ENGINE
IT1204307B (en) AIR CONTROL SYSTEM PARTICULARLY FOR AIRCRAFT ENGINES
GB2172053B (en) Gas turbine engine valve control system
IT1174537B (en) CONTROL SYSTEM FOR GAS TURBINE ENGINE
IT1188534B (en) FUEL CONTROL SYSTEM FOR GAS TURBINE ENGINES
GB2174824B (en) Control systems for gas turbine engines
GB2095335B (en) Gas turbine engine air intake system
IT7922830A0 (en) COOLING AIR SUPPLY SYSTEM FOR GAS TURBINE ENGINE.
IT1150240B (en) TEMPERATURE CONTROL SYSTEM FOR AIR CONDITIONERS
IT8521319A0 (en) GAS TURBO ENGINE CONTROL SYSTEM.
IT8747638A0 (en) FUEL CONTROL SYSTEM FOR AFTERHEATING EQUIPMENT FOR GAS TURBINE ENGINES
IT1183454B (en) COOLING AIR CONTROL SYSTEM FOR GAS TURBO ENGINE
IT1140119B (en) COMPRESSED AIR DISPENSER SYSTEM PARTICULARLY FOR GAS TURBO ENGINES
IT1178575B (en) AIR CONTROL SYSTEM ESPECIALLY FOR GAS TURBO ENGINE
IT1169055B (en) CONTROL SYSTEM FOR THE ATTACHMENT AND RELEASE OF EXHAUST GAS TURBOCHARGERS
GB8619343D0 (en) Gas turbine engine & navigational system
GB2158883B (en) Gas turbine engine cooling air supply
IT1174123B (en) CONTROL SYSTEM FOR INSERTING AND DISCONNECTING AN EXHAUST GAS TURBOCHARGER
IT8324209A0 (en) CONTROL SYSTEM FOR AIRCRAFT GAS TURBO ENGINES.
IT1177240B (en) AIR VALVE CONTROL SYSTEM ON A TWO-STAGE BLOWER BURNER FOR DIESEL OR GAS

Legal Events

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

Effective date: 19930323