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BR8101795A - Turbina a gas - Google Patents

Turbina a gas

Info

Publication number
BR8101795A
BR8101795A BR8101795A BR8101795A BR8101795A BR 8101795 A BR8101795 A BR 8101795A BR 8101795 A BR8101795 A BR 8101795A BR 8101795 A BR8101795 A BR 8101795A BR 8101795 A BR8101795 A BR 8101795A
Authority
BR
Brazil
Prior art keywords
gas turbine
turbine
gas
Prior art date
Application number
BR8101795A
Other languages
English (en)
Inventor
M Stoten
Original Assignee
Pratt & Whitney Aircraft
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 Pratt & Whitney Aircraft filed Critical Pratt & Whitney Aircraft
Publication of BR8101795A publication Critical patent/BR8101795A/pt

Links

Classifications

    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage

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)
BR8101795A 1980-07-02 1981-03-26 Turbina a gas BR8101795A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16528980A 1980-07-02 1980-07-02

Publications (1)

Publication Number Publication Date
BR8101795A true BR8101795A (pt) 1982-08-17

Family

ID=22598283

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8101795A BR8101795A (pt) 1980-07-02 1981-03-26 Turbina a gas

Country Status (4)

Country Link
EP (1) EP0043554A1 (pt)
JP (1) JPS5738619A (pt)
BR (1) BR8101795A (pt)
CA (1) CA1153212A (pt)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2395983A (en) * 2002-12-03 2004-06-09 Rolls Royce Plc Mixed flow compressor for gas turbine engine
US10781705B2 (en) * 2018-11-27 2020-09-22 Pratt & Whitney Canada Corp. Inter-compressor flow divider profiling
US10967210B2 (en) 2019-03-25 2021-04-06 Volkswagen Aktiengesellschaft Transportation vehicle power safety
US11333173B2 (en) * 2019-04-26 2022-05-17 Pratt & Whitney Canada Corp. Inter-compressor cross-over pipe heat exchanger
US12116928B2 (en) * 2023-03-16 2024-10-15 Pratt & Whitney Canada Corp. Aircraft engine having two radially offset turbines

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2050349A (en) * 1931-11-23 1936-08-11 Milo Ab Gas turbine system for aerial propulsion
GB396622A (en) * 1932-01-20 1933-08-10 Milo Ab Improved system for driving propellers
GB689353A (en) * 1950-03-09 1953-03-25 Lysholm Alf Improvements in centrifugal compressors
FR1126906A (fr) * 1951-08-08 1956-12-04 Turbine à gaz, plus spécialement pour véhicules
GB724176A (en) * 1951-11-30 1955-02-16 Parsons & Co Ltd C A Improvements in and relating to combustion turbine plants
US2895295A (en) * 1952-04-04 1959-07-21 Solar Aircraft Co Variable speed gas turbine
US3209536A (en) * 1960-04-04 1965-10-05 Ford Motor Co Re-expansion type gas turbine engine with intercooler fan driven by the low pressure turbine
US3771312A (en) * 1970-11-19 1973-11-13 Automotive turbine engine

Also Published As

Publication number Publication date
EP0043554A1 (en) 1982-01-13
CA1153212A (en) 1983-09-06
JPS5738619A (en) 1982-03-03

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