IT996472B - Perfezionamento nei gruppi propul sori a turbina a gas per uso aero nautico - Google Patents

Perfezionamento nei gruppi propul sori a turbina a gas per uso aero nautico

Info

Publication number
IT996472B
IT996472B IT53753/73A IT5375373A IT996472B IT 996472 B IT996472 B IT 996472B IT 53753/73 A IT53753/73 A IT 53753/73A IT 5375373 A IT5375373 A IT 5375373A IT 996472 B IT996472 B IT 996472B
Authority
IT
Italy
Prior art keywords
aero
improvement
gas turbine
turbine power
power units
Prior art date
Application number
IT53753/73A
Other languages
English (en)
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 IT996472B publication Critical patent/IT996472B/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
    • F02K3/075—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 controlling flow ratio between flows
IT53753/73A 1972-11-17 1973-11-16 Perfezionamento nei gruppi propul sori a turbina a gas per uso aero nautico IT996472B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5316072A GB1415679A (en) 1972-11-17 1972-11-17 Gas turbine engine powerplant

Publications (1)

Publication Number Publication Date
IT996472B true IT996472B (it) 1975-12-10

Family

ID=10466838

Family Applications (1)

Application Number Title Priority Date Filing Date
IT53753/73A IT996472B (it) 1972-11-17 1973-11-16 Perfezionamento nei gruppi propul sori a turbina a gas per uso aero nautico

Country Status (6)

Country Link
US (1) US3913321A (it)
JP (1) JPS5521179B2 (it)
DE (1) DE2356699A1 (it)
FR (1) FR2207244B1 (it)
GB (1) GB1415679A (it)
IT (1) IT996472B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4052845A (en) * 1974-06-20 1977-10-11 United Technologies Corporation Variable ratio bypass gas turbine engine with flow diverter valve
GB2242172B (en) * 1982-03-23 1991-12-11 Rolls Royce Plc Gas turbine engine
US4569199A (en) * 1982-09-29 1986-02-11 The Boeing Company Turboprop engine and method of operating the same
JPS59106958A (ja) * 1982-12-13 1984-06-20 東洋製罐株式会社 アルミニウム層を含む積層体
US5107675A (en) * 1983-03-18 1992-04-28 Rolls-Royce Limited Gas turbine engine
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
DE3467601D1 (en) * 1984-04-02 1987-12-23 Boeing Co Turboprop engine
US4979363A (en) * 1984-11-17 1990-12-25 Rolls-Royce Plc Diverter valve with bypass duct obturator
GB2192941B (en) * 1986-07-25 1990-10-03 Rolls Royce Plc A variable area aircraft air intake
GB2192940B (en) * 1986-07-25 1990-10-31 Rolls Royce Plc A variable area aircraft air intake
US5417055A (en) * 1988-06-28 1995-05-23 Rolls-Royce Plc Valve for diverting fluid flows in turbomachines
GB2301402B (en) * 1988-12-02 1997-09-03 Rolls Royce Plc Valve for diverting fluid flows in gas turbine engines
DE9421496U1 (de) * 1993-05-15 1996-01-18 Ueth & Haug Gmbh Vorrichtung zum Austrennen von Endoprothesen
RU2165547C2 (ru) * 1998-03-17 2001-04-20 Владимир Иосифович Белоус Многоступенчатый осевой компрессор авиационного двигателя

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3316717A (en) * 1965-09-15 1967-05-02 Gen Motors Corp Dual fan engine
US3528246A (en) * 1966-12-29 1970-09-15 Helen M Fischer Fan arrangement for high bypass ratio turbofan engine
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control
BE791058A (fr) * 1971-11-08 1973-03-01 Boeing Co Moteurs a taux de derivation accru ou variable
US3792584A (en) * 1972-02-16 1974-02-19 Boeing Co Increased or variable bypass ratio engines
GB1389347A (en) * 1972-05-25 1975-04-03 Rolls Royce Gas turbine power plant
US3841091A (en) * 1973-05-21 1974-10-15 Gen Electric Multi-mission tandem propulsion system

Also Published As

Publication number Publication date
GB1415679A (en) 1975-11-26
DE2356699A1 (de) 1974-05-30
JPS49135015A (it) 1974-12-26
FR2207244B1 (it) 1978-12-01
FR2207244A1 (it) 1974-06-14
US3913321A (en) 1975-10-21
JPS5521179B2 (it) 1980-06-07

Similar Documents

Publication Publication Date Title
SE7501470L (sv) Komposition lemplig for anvendning i slang eller elastomera stavar.
IT962232B (it) Paletta per l impiego in motori a turbina a gas
IT997686B (it) Motore a turbina a gas
IT945233B (it) Perfezionamento nei rotori di motori a turbina a gas
NO139950C (no) Skipspropell med vridbare blader.
IT996472B (it) Perfezionamento nei gruppi propul sori a turbina a gas per uso aero nautico
CH544217A (de) Gasturbinenschaufel
IT1030805B (it) Perfezionamenti in o relativi a motori a turbina a gas
IT981975B (it) Perfezionamento nei copertoni d aereo
IT1041546B (it) Dispositivo di governo con impugnatura in particolare per motori fuoriboro
IT973011B (it) Propulsore combinato per navi
IL35837A0 (en) Means for measuring bow in a turbine blade
IT1005859B (it) Perfezionamento nei motori a getto per aeromobili
IT979808B (it) Perfezionamento nei freni in particolareper uso aeronautico
DK150937C (da) Planende eller halvplanende baad
NO140623C (no) Katamaran med flere drivpropeller.
IT1039656B (it) Bulro di poppa per navi
AT343715B (de) Schienenrad in leichtbauweise
IT1042169B (it) Perfezionamenti nei gruppi pro pulsori con turbina a gas
IT950563B (it) Perfezionamento nei rotori per turbine a gas
IT1112084B (it) Perfezionamento nei complessi pro pulsori a turbina a gas in particolare per veicoli
IT989643B (it) Perfezionamento nei gruppi propul sori a turbina a gas per aeromobi li
IT1042158B (it) Perfezionamenti nei motori a turbina a gas
IT1022216B (it) Perfezionamento nei condotti di eliche in particolare di eliche marine
NO143321C (no) Marin konstruksjon for stasjonaer anbringelse i arktiske sjoeomraader