IT1060258B - GAS TURBINE ENGINE - Google Patents

GAS TURBINE ENGINE

Info

Publication number
IT1060258B
IT1060258B IT2263276A IT2263276A IT1060258B IT 1060258 B IT1060258 B IT 1060258B IT 2263276 A IT2263276 A IT 2263276A IT 2263276 A IT2263276 A IT 2263276A IT 1060258 B IT1060258 B IT 1060258B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
Prior art date
Application number
IT2263276A
Other languages
Italian (it)
Original Assignee
Rolls Royce 1971 Ltd
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 Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT1060258B publication Critical patent/IT1060258B/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
    • F02K3/06—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
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00—Mathematical features
    • F05D2200/30—Mathematical features miscellaneous
    • F05D2200/32—Mathematical features miscellaneous even
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller

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)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
IT2263276A 1975-04-23 1976-04-23 GAS TURBINE ENGINE IT1060258B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1673275 1975-04-23

Publications (1)

Publication Number Publication Date
IT1060258B true IT1060258B (en) 1982-07-10

Family

ID=10082664

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2263276A IT1060258B (en) 1975-04-23 1976-04-23 GAS TURBINE ENGINE

Country Status (4)

Country Link
JP (1) JPS51127914A (en)
DE (1) DE2617427A1 (en)
FR (1) FR2308789A1 (en)
IT (1) IT1060258B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11255221B2 (en) * 2017-09-20 2022-02-22 General Electric Company Lube system for geared turbine section
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Also Published As

Publication number Publication date
FR2308789A1 (en) 1976-11-19
DE2617427A1 (en) 1976-10-28
JPS51127914A (en) 1976-11-08

Similar Documents

Publication Publication Date Title
IT1045592B (en) GAS TUREINA ENGINE
IT1111236B (en) GAS TURBINE ENGINE
IT1130936B (en) GAS TURBINE ENGINE
IT7821288A0 (en) GAS TURBINE ENGINE.
IT997686B (en) GAS TURBINE ENGINE
IT1075182B (en) IMPROVEMENT IN GAS TURBINE ENGINES
BR7503391A (en) GAS TURBINE IMPROVEMENT
GB1544454A (en) Gas turbine engines
GB1551860A (en) Gas turbine engines
GB1546722A (en) Gas turbine engine
IT1074205B (en) GAS TURBINE PROUPULSOR MECHANISM
IT1068895B (en) GAS TURBINE ENGINE APPARATUS FOR AIRCRAFTS
FR2315611A1 (en) GAS TURBINE ENGINE
FR2315612A1 (en) GAS TURBINE ENGINE
JPS5236211A (en) Gas turbine engine
IT1074030B (en) COMBISTOR ARRANGEMENT FOR GAS TURBINE
JPS5214122A (en) Gas turbine engine
IT1034600B (en) GAS TURBINE ENGINE
FR2334826A1 (en) GAS TURBINE
IT1077139B (en) IGNITION SYSTEM FOR GAS TURBINE ENGINE
FR2314361A1 (en) GAS TURBINE ENGINE
JPS5211313A (en) Gas turbine engine
IT1068291B (en) BLADE OR BLADE FOR A GAS TURBINE ENGINE
IT1034362B (en) GAS TURBINE
JPS5211312A (en) Gas turbine engine