IT1163259B - Metodo ed apparecchio per segnalare tempestivamente lo stallo del compressore in un motore a turbina a gas - Google Patents

Metodo ed apparecchio per segnalare tempestivamente lo stallo del compressore in un motore a turbina a gas

Info

Publication number
IT1163259B
IT1163259B IT20847/83A IT2084783A IT1163259B IT 1163259 B IT1163259 B IT 1163259B IT 20847/83 A IT20847/83 A IT 20847/83A IT 2084783 A IT2084783 A IT 2084783A IT 1163259 B IT1163259 B IT 1163259B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
compressor stall
report timely
timely
Prior art date
Application number
IT20847/83A
Other languages
English (en)
Italian (it)
Other versions
IT8320847A1 (it
IT8320847A0 (it
Inventor
Judith Anne Foster
John Winston St Jacques
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 IT8320847A0 publication Critical patent/IT8320847A0/it
Publication of IT8320847A1 publication Critical patent/IT8320847A1/it
Application granted granted Critical
Publication of IT1163259B publication Critical patent/IT1163259B/it

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
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Control Of Turbines (AREA)
  • Reverberation, Karaoke And Other Acoustics (AREA)
  • Telephonic Communication Services (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Supercharger (AREA)
IT20847/83A 1982-06-21 1983-04-29 Metodo ed apparecchio per segnalare tempestivamente lo stallo del compressore in un motore a turbina a gas IT1163259B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US39057382A 1982-06-21 1982-06-21

Publications (3)

Publication Number Publication Date
IT8320847A0 IT8320847A0 (it) 1983-04-29
IT8320847A1 IT8320847A1 (it) 1984-10-29
IT1163259B true IT1163259B (it) 1987-04-08

Family

ID=23543020

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20847/83A IT1163259B (it) 1982-06-21 1983-04-29 Metodo ed apparecchio per segnalare tempestivamente lo stallo del compressore in un motore a turbina a gas

Country Status (11)

Country Link
JP (1) JPS597738A (fr)
BE (1) BE896611A (fr)
DE (1) DE3314143A1 (fr)
DK (1) DK189683A (fr)
FR (1) FR2528907A1 (fr)
GB (1) GB2122398A (fr)
GR (1) GR78259B (fr)
IL (1) IL68467A0 (fr)
IT (1) IT1163259B (fr)
NL (1) NL8301518A (fr)
NO (1) NO831512L (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4581888A (en) * 1983-12-27 1986-04-15 United Technologies Corporation Compressor rotating stall detection and warning system
US5012637A (en) * 1989-04-13 1991-05-07 General Electric Company Method and apparatus for detecting stalls
DE19812159A1 (de) * 1998-03-20 1999-09-23 Ruhrgas Ag Verfahren zum Regeln des Volumenstroms von Gas, insbesondere Erdgas, durch einen Turboverdichter
US6513333B2 (en) 2000-05-25 2003-02-04 Honda Giken Kogyo Kabushiki Kaisha Surge detection system of gas turbine aeroengine
WO2003044353A1 (fr) * 2001-11-15 2003-05-30 Goodrich Pump & Engine Control Systems, Inc. Procede et appareil pour programmes d'accelerations adaptatives dans des systemes de commande de turbine a gaz
FR2962500B1 (fr) * 2010-07-08 2012-09-14 Snecma Procede et dispositif de detection d'un decollement tournant affectant un compresseur de turbomachine
FR2972233B1 (fr) * 2011-03-04 2017-10-20 Snecma Procede de suppression du decollement tournant dans une turbomachine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3426322A (en) * 1965-10-28 1969-02-04 Gen Electric Turbojet compressor stall warning indicator
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control
US4118926A (en) * 1977-02-28 1978-10-10 United Technologies Corporation Automatic stall recovery system

Also Published As

Publication number Publication date
DE3314143A1 (de) 1983-12-22
GB8309929D0 (en) 1983-05-18
GR78259B (fr) 1984-09-26
GB2122398A (en) 1984-01-11
IT8320847A1 (it) 1984-10-29
DK189683A (da) 1983-12-22
IL68467A0 (en) 1983-07-31
DK189683D0 (da) 1983-04-28
NO831512L (no) 1983-12-22
NL8301518A (nl) 1984-01-16
IT8320847A0 (it) 1983-04-29
JPS597738A (ja) 1984-01-14
FR2528907A1 (fr) 1983-12-23
BE896611A (fr) 1983-08-16

Similar Documents

Publication Publication Date Title
GB2082085B (en) Apparatus for removing nox and for providing better plant efficiency in simple cycle combustion turbine plants
IT1110712B (it) Metodo e apparato per controllare la spinta in un turbomotore a gas
GB2117053B (en) Gas turbines and engines
IT1151030B (it) Apparato e metodo per controllare il flusso nel condotto del ventilatore di un turbomotore a gas
IT1143304B (it) Metodo ed apparecchiatura per rivelare perdite in una struttura quale un edificio
IT9020481A0 (it) gondola per motore
IL69290A0 (en) Improvements in gas turbine engines
IT1129775B (it) Apparato per rilevare e indicare il verificarsi di uno stallo del compressore in un turbomotore a gas
DK158780C (da) Udstoedningsanlaeg til forbraendingsmotorer i et skib
IT1235706B (it) Perfezionamento nei motori a turbina a gas
IT8321090A1 (it) Prediffusore per motori a turbina a gas
GB2102595B (en) Method and apparatus for promoting a surge condition in a stalled gas turbine engine
IT1188884B (it) Collettore in particolare per un motore a sei cilindri in linea
IT8321087A1 (it) Struttura di diffusore per un motore a turbina a gas
IT1088226B (it) Metodo e dispositivo per migliorare il funzionamento di un motore dotato di un turbocompressore
IT1163259B (it) Metodo ed apparecchio per segnalare tempestivamente lo stallo del compressore in un motore a turbina a gas
GB2069053B (en) Water separator in gas turbine inlet
IT1197721B (it) Metodo e dispositivo per ottenere un pezzo sagomato tridimensionalmente
MX146552A (es) Mejoras en compresora centrifuga y metodo para incrementar su eficiencia
JPS52125927A (en) Method and apparatus for increase of mean efficiency in otto cycle engine
IT8621189A0 (it) Apparecchio ad asta in tensione e compressione per ammortizzare le oscillazioni delle pale di un motore di elicottero.
GB2316134B (en) Improvements in or relating to gas turbine engines
IT7949477A0 (it) Perfezionamento nei motori a turbina a gas
IT8948326A0 (it) Apparecchio di misurazione di pressione in motori con compressore comandato da turbina
IT8467114A0 (it) Metodo e dispositivo per la correzione automatica del rapporto aria combustibile in un motore endotermico alternativo