IT8323111A0 - ANTI-ICE SYSTEM FOR AGAS TURBINE. - Google Patents

ANTI-ICE SYSTEM FOR AGAS TURBINE.

Info

Publication number
IT8323111A0
IT8323111A0 IT8323111A IT2311183A IT8323111A0 IT 8323111 A0 IT8323111 A0 IT 8323111A0 IT 8323111 A IT8323111 A IT 8323111A IT 2311183 A IT2311183 A IT 2311183A IT 8323111 A0 IT8323111 A0 IT 8323111A0
Authority
IT
Italy
Prior art keywords
ice system
agas
turbine
agas turbine
ice
Prior art date
Application number
IT8323111A
Other languages
Italian (it)
Other versions
IT1166979B (en
Inventor
Vasco Mezzedimi
Giampiero Ferrari Aggradi
Alessandro Pini
Original Assignee
Nuovo Pignone Spa
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 Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Priority to IT23111/83A priority Critical patent/IT1166979B/en
Publication of IT8323111A0 publication Critical patent/IT8323111A0/en
Priority to SE8404617A priority patent/SE8404617L/en
Priority to GB08423721A priority patent/GB2147364A/en
Priority to CH4494/84A priority patent/CH660620A5/en
Priority to FR8415116A priority patent/FR2552816A1/en
Priority to DE19843436273 priority patent/DE3436273A1/en
Priority to JP59206462A priority patent/JPS6095137A/en
Application granted granted Critical
Publication of IT1166979B publication Critical patent/IT1166979B/en

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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Hydraulic Turbines (AREA)
IT23111/83A 1983-10-03 1983-10-03 ANTI-ICE SYSTEM FOR GAS TURBINE IT1166979B (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
IT23111/83A IT1166979B (en) 1983-10-03 1983-10-03 ANTI-ICE SYSTEM FOR GAS TURBINE
SE8404617A SE8404617L (en) 1983-10-03 1984-09-14 SYSTEM FOR PREVENTING TURBINE ICE CREATION
GB08423721A GB2147364A (en) 1983-10-03 1984-09-19 Anti-icing system for a gas turbine
CH4494/84A CH660620A5 (en) 1983-10-03 1984-09-19 ANTI-ICE DEVICE FOR GAS TURBINE.
FR8415116A FR2552816A1 (en) 1983-10-03 1984-10-02 ANTI-ICING SYSTEM FOR A GAS TURBINE
DE19843436273 DE3436273A1 (en) 1983-10-03 1984-10-03 ICE PROTECTION DEVICE FOR A GAS TURBINE
JP59206462A JPS6095137A (en) 1983-10-03 1984-10-03 Water adhesion preventing apparatus for gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT23111/83A IT1166979B (en) 1983-10-03 1983-10-03 ANTI-ICE SYSTEM FOR GAS TURBINE

Publications (2)

Publication Number Publication Date
IT8323111A0 true IT8323111A0 (en) 1983-10-03
IT1166979B IT1166979B (en) 1987-05-06

Family

ID=11203901

Family Applications (1)

Application Number Title Priority Date Filing Date
IT23111/83A IT1166979B (en) 1983-10-03 1983-10-03 ANTI-ICE SYSTEM FOR GAS TURBINE

Country Status (7)

Country Link
JP (1) JPS6095137A (en)
CH (1) CH660620A5 (en)
DE (1) DE3436273A1 (en)
FR (1) FR2552816A1 (en)
GB (1) GB2147364A (en)
IT (1) IT1166979B (en)
SE (1) SE8404617L (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2705996B1 (en) * 1993-06-03 1995-07-07 Snecma Defrosting system for the front parts of a turbomachine.
DE19622057C2 (en) * 1996-05-31 2001-08-16 Energieversorgung Halle Gmbh Method and device for the efficient use of waste heat in power engines
EP0931214B1 (en) 1996-10-08 2002-07-24 Siemens Aktiengesellschaft Method for thermoregulating inlet air, and thermostat needed for its application
DE102006061926A1 (en) * 2006-12-21 2008-07-03 Siemens Ag Phase separator for a multiphase switching device
US8429891B2 (en) 2009-12-16 2013-04-30 General Electric Company Anti-icing system using radiant infrared energy from turbine exhaust flues
RU2435051C1 (en) * 2010-06-01 2011-11-27 Открытое акционерное общество Научно-производственное объединение "Искра" Air cleaning device for gas turbine installation
US8444093B1 (en) 2011-04-18 2013-05-21 Eran Epstein Airplane leading edge de-icing apparatus

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2435990A (en) * 1945-08-17 1948-02-17 Westinghouse Electric Corp Gas turbine lubricating oil cooling and air inlet deicing system
GB629044A (en) * 1946-10-30 1949-09-09 United Aircraft Corp Improvements in or relating to compressors, particularly for use with aircraft powerplants
GB659569A (en) * 1948-12-23 1951-10-24 Westinghouse Electric Int Co Improvements in or relating to lubrication systems for aviation power plants
GB720012A (en) * 1951-04-23 1954-12-08 Bristol Aeroplane Co Ltd Improvements in or relating to the cooling of aircraft propulsion plants
DE1009436B (en) * 1953-03-27 1957-05-29 Daimler Benz Ag Cooling and de-icing device for gas turbines
GB738889A (en) * 1953-07-03 1955-10-19 Armstrong Siddeley Motors Ltd Improvements relating to the supply of hot air from a gas turbine engine for anti-icing or other purposes
GB909928A (en) * 1960-08-05 1962-11-07 Rolls Royce Improvements relating to gas turbine engines
GB1018538A (en) * 1964-07-06 1966-01-26 Rolls Royce Gas turbine engine
DE1601602A1 (en) * 1967-12-01 1971-01-21 Licentia Gmbh Device for preheating the intake air in a gas turbine system with an exhaust stack
US3981466A (en) * 1974-12-23 1976-09-21 The Boeing Company Integrated thermal anti-icing and environmental control system
IT1123460B (en) * 1978-07-10 1986-04-30 Westinghouse Canada Ltd METHOD FOR HEATING THE DIRECT VANE IN A GAS TURBINE
US4328666A (en) * 1980-06-25 1982-05-11 General Electric Company Heat recovery anti-icing system
GB2088570A (en) * 1980-11-20 1982-06-09 Rolls Royce Gas turbine engine test bed with exhaust heat recovery

Also Published As

Publication number Publication date
FR2552816A1 (en) 1985-04-05
GB2147364A (en) 1985-05-09
DE3436273A1 (en) 1985-04-18
CH660620A5 (en) 1987-05-15
IT1166979B (en) 1987-05-06
GB8423721D0 (en) 1984-10-24
SE8404617D0 (en) 1984-09-14
JPS6095137A (en) 1985-05-28
SE8404617L (en) 1985-04-04

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19941013