IT8025895A0 - SYSTEM FOR FLEXIBLE POWER TAKE-OFF IN HIGH PERFORMANCE AIRCRAFT GAS TURBINES. - Google Patents

SYSTEM FOR FLEXIBLE POWER TAKE-OFF IN HIGH PERFORMANCE AIRCRAFT GAS TURBINES.

Info

Publication number
IT8025895A0
IT8025895A0 IT8025895A IT2589580A IT8025895A0 IT 8025895 A0 IT8025895 A0 IT 8025895A0 IT 8025895 A IT8025895 A IT 8025895A IT 2589580 A IT2589580 A IT 2589580A IT 8025895 A0 IT8025895 A0 IT 8025895A0
Authority
IT
Italy
Prior art keywords
high performance
power take
gas turbines
flexible power
aircraft gas
Prior art date
Application number
IT8025895A
Other languages
Italian (it)
Other versions
IT1133799B (en
Inventor
Gerhard Kissel
Dieter Baack
Gerhard Kopp
Horst Niehaus
Original Assignee
Messerschmitt Boelkow Blohm
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 Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Publication of IT8025895A0 publication Critical patent/IT8025895A0/en
Application granted granted Critical
Publication of IT1133799B publication Critical patent/IT1133799B/en

Links

Classifications

    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
IT25895/80A 1979-11-16 1980-11-11 SYSTEM FOR THE FLEXIBLE GRIP OF POSTENCE IN GAS TURBINES OF HIGH-PERFORMANCE AIRCRAFTS IT1133799B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2946371A DE2946371C2 (en) 1979-11-16 1979-11-16 Auxiliary propulsion system for aircraft auxiliary equipment

Publications (2)

Publication Number Publication Date
IT8025895A0 true IT8025895A0 (en) 1980-11-11
IT1133799B IT1133799B (en) 1986-07-09

Family

ID=6086194

Family Applications (1)

Application Number Title Priority Date Filing Date
IT25895/80A IT1133799B (en) 1979-11-16 1980-11-11 SYSTEM FOR THE FLEXIBLE GRIP OF POSTENCE IN GAS TURBINES OF HIGH-PERFORMANCE AIRCRAFTS

Country Status (4)

Country Link
DE (1) DE2946371C2 (en)
FR (1) FR2469567A1 (en)
GB (1) GB2063188B (en)
IT (1) IT1133799B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3502578A1 (en) * 1985-01-26 1986-07-31 Klöckner-Humboldt-Deutz AG, 5000 Köln AUXILIARY DRIVE FOR A GAS TURBINE ENGINE
DE3515770A1 (en) * 1985-05-02 1986-11-06 Klöckner-Humboldt-Deutz AG, 5000 Köln AUXILIARY DRIVE ARRANGEMENT WITH GEARBOX FOR A GAS TURBINE ENGINE
US7975465B2 (en) * 2003-10-27 2011-07-12 United Technologies Corporation Hybrid engine accessory power system
DE102008018101A1 (en) 2008-04-09 2009-10-15 Rolls-Royce Deutschland Ltd & Co Kg Jet engine with at least one emergency drive

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2863288A (en) * 1954-11-19 1958-12-09 Jack & Heintz Inc Air pressure control means for air turbine drive systems
BE567824A (en) * 1957-05-20
GB1212109A (en) * 1968-08-09 1970-11-11 Rolls Royce Engine assembly
US3514945A (en) * 1968-10-04 1970-06-02 Avco Corp Gas turbine accessory power drive unit
US4068470A (en) * 1974-11-08 1978-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with convertible accessories
DE2519152C2 (en) * 1975-04-30 1982-11-25 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Device for starting aircraft engines and operating aircraft auxiliary devices

Also Published As

Publication number Publication date
IT1133799B (en) 1986-07-09
GB2063188A (en) 1981-06-03
GB2063188B (en) 1983-09-28
DE2946371A1 (en) 1981-05-27
FR2469567B3 (en) 1982-07-23
DE2946371C2 (en) 1982-07-08
FR2469567A1 (en) 1981-05-22

Similar Documents

Publication Publication Date Title
IT1243892B (en) LOW TEMPERATURE ROTOR - HIGH TEMPERATURE FOR TURBINES.
IT1090803B (en) TORQUE MEASURING DEVICE FOR PROPULSORS AND GAS TURBINES, IN PARTICULAR FOR TURBO JET PROPULSORS
IT1122733B (en) COMPOSITE CERAMIC BLADE FOR GAS TURBINE
JPS54160911A (en) Blade for gas turbine engine
DE3880995T2 (en) ROTOR FOR A GAS TURBINE.
ZA777122B (en) Inlet air cleaner assembly for turbine engines
IT8020482A0 (en) BLADE ROTOR FOR GAS TURBINE ENGINE.
IT1006614B (en) PROCEDURE AND CONBUSTION EQUIPMENT PARTICULARLY FOR GAS TURBINES
IT7821869A0 (en) COOLED ROTOR BLADE FOR GAS TURBINE ENGINE.
DE69107148D1 (en) Gas turbine with cooled blades.
GB2043786B (en) Gas turbine engine power plant
IT1122732B (en) COMPOSITE CERAMIC BLADE FOR GAS TURBINE
MX150266A (en) IMPROVEMENTS IN GAS TURBINE PLANT
IT8323356A0 (en) COUPLED. SUPPORT SYSTEM FOR TURBO SHAFT GAS TURBINE ENGINES
IT8321090A0 (en) PRE-DIFFUSER FOR GAS TURBINE ENGINES.
IT1130186B (en) COMBUSTION SYSTEM FOR DOUBLE STAGE / DOUBLE OPERATION GAS TURBINE
IT8324164A0 (en) IMPROVEMENTS MADE TO THE AIR INTAKES OF AGAS TURBINE ENGINES MOUNTED ON AIRCRAFT.
IT8021276A0 (en) ANTI-ICE SYSTEM FOR GAS TURBINE ENGINE NOSE.
IT7922830A0 (en) COOLING AIR SUPPLY SYSTEM FOR GAS TURBINE ENGINE.
DE3680351D1 (en) FUEL NOZZLE FOR A GAS TURBINE.
IT1193595B (en) PRGANO COMMAND, IN PARTICULAR FOR THE START-UP OF AIR TURBINES FOR AIRCRAFT FOR AIRCRAFT
IT8224980A0 (en) GAS TURBINE BLADE COOLING SYSTEM.
JPS54101014A (en) Winggshaped blade for gas turbine engine
GB2021699A (en) Gas turbine blade cooling arrangement
IT8025895A0 (en) SYSTEM FOR FLEXIBLE POWER TAKE-OFF IN HIGH PERFORMANCE AIRCRAFT GAS TURBINES.