FR2312659A1 - Methode de commande d'une turbo-soufflante - Google Patents

Methode de commande d'une turbo-soufflante

Info

Publication number
FR2312659A1
FR2312659A1 FR7615893A FR7615893A FR2312659A1 FR 2312659 A1 FR2312659 A1 FR 2312659A1 FR 7615893 A FR7615893 A FR 7615893A FR 7615893 A FR7615893 A FR 7615893A FR 2312659 A1 FR2312659 A1 FR 2312659A1
Authority
FR
France
Prior art keywords
turbo
control method
blower control
blower
control
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR7615893A
Other languages
English (en)
Other versions
FR2312659B1 (fr
Inventor
Arthur Paul Adamson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2312659A1 publication Critical patent/FR2312659A1/fr
Application granted granted Critical
Publication of FR2312659B1 publication Critical patent/FR2312659B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control

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)
FR7615893A 1975-05-29 1976-05-26 Methode de commande d'une turbo-soufflante Granted FR2312659A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/581,750 US4068469A (en) 1975-05-29 1975-05-29 Variable thrust nozzle for quiet turbofan engine and method of operating same

Publications (2)

Publication Number Publication Date
FR2312659A1 true FR2312659A1 (fr) 1976-12-24
FR2312659B1 FR2312659B1 (fr) 1983-04-01

Family

ID=24326426

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7615893A Granted FR2312659A1 (fr) 1975-05-29 1976-05-26 Methode de commande d'une turbo-soufflante

Country Status (6)

Country Link
US (1) US4068469A (fr)
JP (1) JPS51146614A (fr)
DE (1) DE2623764A1 (fr)
FR (1) FR2312659A1 (fr)
GB (1) GB1545901A (fr)
IT (1) IT1123057B (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4242864A (en) * 1978-05-25 1981-01-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated control system for a gas turbine engine
DE4012212A1 (de) * 1990-04-14 1991-10-24 Mtu Muenchen Gmbh Duese fuer ein hyperschalltriebwerk
US5833140A (en) * 1996-12-12 1998-11-10 United Technologies Corporation Variable geometry exhaust nozzle for a turbine engine
US6705547B2 (en) * 2002-02-01 2004-03-16 Luis Manuel Braga Da Costa Campos Active noise reducing nozzle
US7669785B2 (en) 2006-04-24 2010-03-02 The Boeing Company Integrated engine exhaust systems and methods for drag and thermal stress reduction
DE102006019299B3 (de) * 2006-04-26 2007-11-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Ummanteltes Turbofan-Flugzeugtriebwerk
US8776952B2 (en) * 2006-05-11 2014-07-15 United Technologies Corporation Thermal management system for turbofan engines
WO2008045062A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Tuyère à section variable pour nacelle de soufflante de moteur à turbine à gaz équipée d' un système d'actionnement coulissant
WO2008045079A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Commande de fonctionnement de moteur à double flux
DE602006019008D1 (de) * 2006-10-12 2011-01-27 United Technologies Corp Modulationsströmung durch turbomotorkühlsystem
US20100000220A1 (en) * 2006-10-12 2010-01-07 Zaffir Chaudhry Fan variable area nozzle with electromechanical actuator
EP2061964B1 (fr) * 2006-10-12 2015-03-04 United Technologies Corporation Moteur à turboréacteur à structure interne fixée comprenant des passages carénés
US7797944B2 (en) * 2006-10-20 2010-09-21 United Technologies Corporation Gas turbine engine having slim-line nacelle
US7721549B2 (en) * 2007-02-08 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
US20080273961A1 (en) 2007-03-05 2008-11-06 Rosenkrans William E Flutter sensing and control system for a gas turbine engine
US9228534B2 (en) 2007-07-02 2016-01-05 United Technologies Corporation Variable contour nacelle assembly for a gas turbine engine
US20090226303A1 (en) * 2008-03-05 2009-09-10 Grabowski Zbigniew M Variable area fan nozzle fan flutter management system
US9267463B2 (en) * 2008-03-25 2016-02-23 United Technologies Corp. Gas turbine engine systems involving variable nozzles with flexible panels
US8356483B2 (en) * 2008-04-10 2013-01-22 United Technologies Corp Gas turbine engine systems involving variable nozzles with sliding doors
GB0820174D0 (en) * 2008-11-05 2008-12-10 Rolls Royce Plc A gas turbine engine variable area exhaust nozzle
US8959889B2 (en) 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
US8127532B2 (en) * 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
US20110120079A1 (en) * 2009-11-24 2011-05-26 Schwark Jr Fred W Variable area fan nozzle stiffeners and placement
US8511973B2 (en) * 2010-06-23 2013-08-20 Rohr, Inc. Guide system for nacelle assembly
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
US9416751B2 (en) * 2010-12-07 2016-08-16 Hamilton Sundstrand Corporation Actuation system
US8869508B2 (en) 2012-01-31 2014-10-28 United Technologies Corporation Gas turbine engine variable area fan nozzle control
US9593628B2 (en) 2012-01-31 2017-03-14 United Technologies Corporation Gas turbine engine variable area fan nozzle with ice management
US20140137538A1 (en) * 2012-11-16 2014-05-22 United Technologies Corporation Fast Response Bypass Engine
GB201609071D0 (en) 2016-05-24 2016-07-06 Rolls Royce Plc Aircraft gas turbine engine nacelle

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1552336A (fr) * 1967-01-12 1969-01-03
US3598318A (en) * 1970-04-10 1971-08-10 Boeing Co Movable acoustic splitter for nozzle area control and thrust reversal
FR2076107A1 (fr) * 1970-01-14 1971-10-15 Rolls Royce
DE2106876A1 (de) * 1970-05-18 1971-12-02 Fahlbusch H Mantelgebläse-Turbojet-Trieb werk
FR2120172A1 (fr) * 1971-01-02 1972-08-11 Dowty Rotol Ltd
US3721389A (en) * 1971-06-10 1973-03-20 Boeing Co Exit nozzle assemblies for gas turbine power plants
US3889882A (en) * 1974-03-25 1975-06-17 Gen Electric Retractable sound suppressor for a gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934966A (en) * 1957-11-12 1960-05-03 Westinghouse Electric Corp Control apparatus
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
US3514952A (en) * 1964-07-01 1970-06-02 Us Air Force Variable bypass turbofan engine
US3261164A (en) * 1964-09-23 1966-07-19 United Aircraft Corp Convergent-divergent co-annular primary nozzle
US3401524A (en) * 1967-04-21 1968-09-17 United Aircraft Corp Control for ducted fan engine
GB1418665A (en) * 1972-04-27 1975-12-24 Rolls Royce Fluid flow ducts

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1552336A (fr) * 1967-01-12 1969-01-03
FR2076107A1 (fr) * 1970-01-14 1971-10-15 Rolls Royce
US3598318A (en) * 1970-04-10 1971-08-10 Boeing Co Movable acoustic splitter for nozzle area control and thrust reversal
DE2106876A1 (de) * 1970-05-18 1971-12-02 Fahlbusch H Mantelgebläse-Turbojet-Trieb werk
FR2120172A1 (fr) * 1971-01-02 1972-08-11 Dowty Rotol Ltd
US3721389A (en) * 1971-06-10 1973-03-20 Boeing Co Exit nozzle assemblies for gas turbine power plants
US3889882A (en) * 1974-03-25 1975-06-17 Gen Electric Retractable sound suppressor for a gas turbine engine

Also Published As

Publication number Publication date
GB1545901A (en) 1979-05-16
IT1123057B (it) 1986-04-30
JPS51146614A (en) 1976-12-16
FR2312659B1 (fr) 1983-04-01
DE2623764A1 (de) 1976-12-09
US4068469A (en) 1978-01-17

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Legal Events

Date Code Title Description
ST Notification of lapse