IT7819442A0 - Perfezionamenti apportati ai gruppi motopropulsori a turbina a gas. - Google Patents

Perfezionamenti apportati ai gruppi motopropulsori a turbina a gas.

Info

Publication number
IT7819442A0
IT7819442A0 IT7819442A IT1944278A IT7819442A0 IT 7819442 A0 IT7819442 A0 IT 7819442A0 IT 7819442 A IT7819442 A IT 7819442A IT 1944278 A IT1944278 A IT 1944278A IT 7819442 A0 IT7819442 A0 IT 7819442A0
Authority
IT
Italy
Prior art keywords
gas turbine
improvements made
turbine power
power units
units
Prior art date
Application number
IT7819442A
Other languages
English (en)
Other versions
IT1092531B (it
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of IT7819442A0 publication Critical patent/IT7819442A0/it
Application granted granted Critical
Publication of IT1092531B publication Critical patent/IT1092531B/it

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
    • F02K3/062—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 aft fan
    • 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
    • F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows
IT19442/78A 1977-01-19 1978-01-19 Perfezionamenti apportati ai gruppi motopropolsori a turbina a gas IT1092531B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2018/77A GB1551881A (en) 1977-01-19 1977-01-19 Gas turbine engine powerplants

Publications (2)

Publication Number Publication Date
IT7819442A0 true IT7819442A0 (it) 1978-01-19
IT1092531B IT1092531B (it) 1985-07-12

Family

ID=9732149

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19442/78A IT1092531B (it) 1977-01-19 1978-01-19 Perfezionamenti apportati ai gruppi motopropolsori a turbina a gas

Country Status (6)

Country Link
US (1) US4183210A (it)
JP (1) JPS53112319A (it)
DE (1) DE2801374C2 (it)
FR (1) FR2378182A1 (it)
GB (1) GB1551881A (it)
IT (1) IT1092531B (it)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4466587A (en) * 1981-12-21 1984-08-21 General Electric Company Nacelle installation
GB2117054B (en) * 1982-02-17 1985-01-30 Rolls Royce Aircraft propulsion engine having a rear mounted propfan
DE3430221A1 (de) * 1984-08-17 1986-02-27 Herbert 6290 Weilburg Zemann Gasturbine mit ansaugrohren
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
GB2192234B (en) * 1986-07-02 1991-04-17 Rolls Royce Plc A turbofan gas turbine engine
JPH0570221U (ja) * 1991-02-16 1993-09-24 高北農機株式会社 肥料散布機
DE4129357C2 (de) * 1991-07-03 1993-10-28 Kastens Karl Tangentialgebläse für Turbotriebwerke
GB0617769D0 (en) * 2006-09-09 2006-10-18 Rolls Royce Plc An engine
DE102008060488A1 (de) * 2008-12-05 2010-06-10 Rolls-Royce Deutschland Ltd & Co Kg Verfahren und Vorrichtung zum Betrieb eines mit Schubpropellern versehenen Turboprop-Flugtriebwerkes
US9718536B2 (en) 2010-05-18 2017-08-01 Hamilton Sundstrand Corporation Counter-rotating open-rotor (CROR)
US9017037B2 (en) 2012-01-24 2015-04-28 United Technologies Corporation Rotor with flattened exit pressure profile
EP2971535A4 (en) 2013-03-15 2017-02-15 United Technologies Corporation Geared turbofan engine having a reduced number of fan blades and improved acoustics
US9850818B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US9850794B2 (en) * 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US10060316B2 (en) 2015-06-29 2018-08-28 General Electric Company Power generation system exhaust cooling
US10087801B2 (en) * 2015-06-29 2018-10-02 General Electric Company Power generation system exhaust cooling
US10030558B2 (en) 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US10215070B2 (en) 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
US10077694B2 (en) 2015-06-29 2018-09-18 General Electric Company Power generation system exhaust cooling
US9840953B2 (en) 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US9856768B2 (en) 2015-06-29 2018-01-02 General Electric Company Power generation system exhaust cooling
US9938874B2 (en) 2015-06-29 2018-04-10 General Electric Company Power generation system exhaust cooling
DE102015111666A1 (de) 2015-07-17 2017-01-19 Johann Schwöller Antriebsvorrichtung für ein Flugzeug sowie ein Flugzeug mit einer solchen Antriebsvorrichtung
US10316759B2 (en) 2016-05-31 2019-06-11 General Electric Company Power generation system exhaust cooling

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB647908A (en) * 1946-09-27 1950-12-28 Packard Motor Car Co Jet propulsion unit
FR997672A (fr) * 1949-09-29 1952-01-09 Système d'échappement en dépression applicable aux turbines à gaz
GB838602A (en) * 1957-03-06 1960-06-22 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine plant
US3348379A (en) * 1963-09-25 1967-10-24 Rolls Royce Turbojet engine with compressor bypass and aft fan
GB1333102A (en) * 1970-07-08 1973-10-10 British Aircraft Corp Ltd Propuldion power plant for aircraft
FR2228949B1 (it) * 1973-05-08 1977-02-11 Snecma
FI53869C (fi) * 1973-05-11 1978-08-10 Valmet Oy Kontrollanordning foer kraftmaskin
FR2270450A1 (en) * 1974-03-29 1975-12-05 Snecma Gas turbine with split air flow - has low pressure turbine stage crossed by main and secondary flow mixture

Also Published As

Publication number Publication date
DE2801374A1 (de) 1978-07-20
IT1092531B (it) 1985-07-12
US4183210A (en) 1980-01-15
DE2801374C2 (de) 1982-02-25
GB1551881A (en) 1979-09-05
FR2378182A1 (fr) 1978-08-18
JPS53112319A (en) 1978-09-30
FR2378182B1 (it) 1985-03-22

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