IT8721567A0 - Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina - Google Patents

Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina

Info

Publication number
IT8721567A0
IT8721567A0 IT8721567A IT2156787A IT8721567A0 IT 8721567 A0 IT8721567 A0 IT 8721567A0 IT 8721567 A IT8721567 A IT 8721567A IT 2156787 A IT2156787 A IT 2156787A IT 8721567 A0 IT8721567 A0 IT 8721567A0
Authority
IT
Italy
Prior art keywords
checking
turbine engines
exhaust limits
exhaust
limits
Prior art date
Application number
IT8721567A
Other languages
English (en)
Other versions
IT1228547B (it
Inventor
Robert Wayne Rice
Nicholas Dean Lappos
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8721567A0 publication Critical patent/IT8721567A0/it
Application granted granted Critical
Publication of IT1228547B publication Critical patent/IT1228547B/it

Links

Classifications

    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/052—Torque
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Eletrric Generators (AREA)
  • Catching Or Destruction (AREA)
  • Controls For Constant Speed Travelling (AREA)
IT8721567A 1986-08-04 1987-08-03 Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina IT1228547B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US89268986A 1986-08-04 1986-08-04

Publications (2)

Publication Number Publication Date
IT8721567A0 true IT8721567A0 (it) 1987-08-03
IT1228547B IT1228547B (it) 1991-06-20

Family

ID=25400361

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8721567A IT1228547B (it) 1986-08-04 1987-08-03 Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina

Country Status (6)

Country Link
JP (1) JPS6345429A (it)
BR (1) BR8701672A (it)
DE (1) DE3725687A1 (it)
FR (1) FR2602270A1 (it)
GB (1) GB2193535A (it)
IT (1) IT1228547B (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8730187D0 (en) * 1987-12-24 1988-02-03 Rolls Royce Plc Overspeed limiter for gas turbine aeroengine
US5258505A (en) * 1991-07-26 1993-11-02 Canon Kabushiki Kaisha Trisazo compounds, and dye compositions containing same
GB2262623B (en) * 1991-12-17 1995-04-26 Rolls Royce Plc Aircraft engine management system
US6012676A (en) * 1998-03-31 2000-01-11 Sikorsky Aircraft Corporation Integrated fire and flight control system with automatic engine torque limiting
FR2878288B1 (fr) 2004-11-25 2007-01-19 Eurocopter France Procede et dispositif pour optimiser l'enveloppe de performances d'un turbomoteur
FR2888287B1 (fr) 2005-07-07 2011-04-08 Eurocopter France Procede d'optimisation de l'enveloppe de perfomances d'un turbomoteur.
DE102009016106A1 (de) * 2009-02-20 2010-08-26 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zum Messen der Beanspruchung rotierender Wellen von Turbomaschinen und Flugtriebwerken und Vorrichtung zur Durchführung des Verfahrens
DE102009016105B4 (de) * 2009-02-20 2017-11-16 Rolls-Royce Deutschland Ltd & Co Kg Verfahren und Vorrichtung zum Messen der Beanspruchung rotierender Wellen
FR2966881B1 (fr) 2010-10-29 2013-08-30 Eurocopter France Installation motrice d'un aeronef, aeronef, et procede de pilotage dudit aeronef.
FR2985715B1 (fr) 2012-01-12 2013-12-27 Eurocopter France Installation motrice d'un aeronef, aeronef, et procede de pilotage dudit aeronef
US9771167B2 (en) 2013-01-16 2017-09-26 Airbus Helicopters Monitor system for monitoring the starting of a rotary wing aircraft, an aircraft, and a method using the system
FR3000989A1 (fr) 2013-01-16 2014-07-18 Eurocopter France Systeme de surveillance du demarrage d'un aeronef a voilure tournante, aeronef et procede mettant en oeuvre ce systeme
FR3034403B1 (fr) 2015-03-31 2017-03-31 Airbus Helicopters Procede et dispositif pour arreter un turbomoteur en fonctionnement nominal

Also Published As

Publication number Publication date
IT1228547B (it) 1991-06-20
DE3725687A1 (de) 1988-02-18
GB2193535A (en) 1988-02-10
GB8718303D0 (en) 1987-09-09
BR8701672A (pt) 1988-01-05
FR2602270A1 (fr) 1988-02-05
JPS6345429A (ja) 1988-02-26

Similar Documents

Publication Publication Date Title
IL83975A (en) Method of reclassifying nozzle of gas turbine engines
IT9021809A0 (it) Perfezionati motori e metodi per fare i medesimi
GB2173602B (en) Method and device for spin-testing of turbocharger rotor
EP0238871A3 (en) Measuring device for the analysis of the exhaust gases of combustion engines, and method for the use of such a device
IT1126488B (it) Tenuta di turbomotore a gas e metodo per fare la medesima
AU7122487A (en) Method and device for the post combustion of process exhaust gasses
FR2552159B1 (fr) Dispositif de liaison et d'etancheite de secteurs d'aubes de stator de turbine
IT1222057B (it) Complesso di tenuta in particolare per turbomotori a gas
DE3670505D1 (de) Pyrolyse- und verbrennungsverfahren und -anlage.
IT8922686A0 (it) Contrappeso di bilanciatura senza bulloni per motori di turbina
IT8721567A0 (it) Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina
IT1235706B (it) Perfezionamento nei motori a turbina a gas
IT8619917A1 (it) Metodo ed apparato per la polverizzazione di combustibile
IT1163366B (it) Prediffusore per motori a turbina a gas
GB2102595B (en) Method and apparatus for promoting a surge condition in a stalled gas turbine engine
DK474385D0 (da) Metode og anordning til testning af taetheden i en forbraendingsmotor
GB8610559D0 (en) Gas turbine engines
IT8149642A0 (it) Procedimento ed apparecchio per la generazione di gas in motori alternativi a combustione interna
IT1240293B (it) Metodo e apparato per rivelare stalli di un turbomotore a gas
IT8048196A0 (it) Rotore per turbocompressore a gasdi scarico e procedimento per produrlo
IT1089024B (it) Metodo ed apparato per correggere la distorsione di palette di turbomotori a gas
IT1224248B (it) Silenziatore per piccoli motori
IT8648062A0 (it) Attrezzatura per la lavorazione e manutenzione delle teste di motori a combustione interna
DK0378085T3 (da) Udstødningsgasturbinegeneratoranlæg
IT8619848A0 (it) Metodo e apparato per controllare aerei a motori multipli.