IT201600130851A1 - Piastrella termoisolante per camere di combustione di turbine a gas - Google Patents

Piastrella termoisolante per camere di combustione di turbine a gas

Info

Publication number
IT201600130851A1
IT201600130851A1 IT102016000130851A IT201600130851A IT201600130851A1 IT 201600130851 A1 IT201600130851 A1 IT 201600130851A1 IT 102016000130851 A IT102016000130851 A IT 102016000130851A IT 201600130851 A IT201600130851 A IT 201600130851A IT 201600130851 A1 IT201600130851 A1 IT 201600130851A1
Authority
IT
Italy
Prior art keywords
thermo
gas turbine
combustion chambers
turbine combustion
insulating tile
Prior art date
Application number
IT102016000130851A
Other languages
English (en)
Inventor
Paolo Macelloni
Original Assignee
Ansaldo Energia 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 Ansaldo Energia Spa filed Critical Ansaldo Energia Spa
Priority to IT102016000130851A priority Critical patent/IT201600130851A1/it
Priority to EP17209153.0A priority patent/EP3339737B1/en
Priority to US15/852,520 priority patent/US10808931B2/en
Priority to CN201711406727.XA priority patent/CN108240638B/zh
Publication of IT201600130851A1 publication Critical patent/IT201600130851A1/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/02—Casings; Linings; Walls characterised by the shape of the bricks or blocks used
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/13—Parts of turbine combustion chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/04—Repairing fractures or cracked metal parts or products, e.g. castings
    • B23P6/045—Repairing fractures or cracked metal parts or products, e.g. castings of turbine components, e.g. moving or stationary blades, rotors, etc.
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00019—Repairing or maintaining combustion chamber liners or subparts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/16—Two dimensionally sectional layer
    • Y10T428/163—Next to unitary web or sheet of equal or greater extent
    • Y10T428/164—Continuous two dimensionally sectional layer
    • Y10T428/166—Glass, ceramic, or metal sections [e.g., floor or wall tile, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Furnace Housings, Linings, Walls, And Ceilings (AREA)
  • Thermal Insulation (AREA)
IT102016000130851A 2016-12-23 2016-12-23 Piastrella termoisolante per camere di combustione di turbine a gas IT201600130851A1 (it)

Priority Applications (4)

Application Number Priority Date Filing Date Title
IT102016000130851A IT201600130851A1 (it) 2016-12-23 2016-12-23 Piastrella termoisolante per camere di combustione di turbine a gas
EP17209153.0A EP3339737B1 (en) 2016-12-23 2017-12-20 Thermoinsulating tile for a combustion chamber of a gas turbine
US15/852,520 US10808931B2 (en) 2016-12-23 2017-12-22 Thermoinsulating tile for a combustion chamber of a gas turbine
CN201711406727.XA CN108240638B (zh) 2016-12-23 2017-12-22 用于燃气涡轮的燃烧室的绝热瓦

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102016000130851A IT201600130851A1 (it) 2016-12-23 2016-12-23 Piastrella termoisolante per camere di combustione di turbine a gas

Publications (1)

Publication Number Publication Date
IT201600130851A1 true IT201600130851A1 (it) 2018-06-23

Family

ID=58670218

Family Applications (1)

Application Number Title Priority Date Filing Date
IT102016000130851A IT201600130851A1 (it) 2016-12-23 2016-12-23 Piastrella termoisolante per camere di combustione di turbine a gas

Country Status (4)

Country Link
US (1) US10808931B2 (it)
EP (1) EP3339737B1 (it)
CN (1) CN108240638B (it)
IT (1) IT201600130851A1 (it)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4838030A (en) * 1987-08-06 1989-06-13 Avco Corporation Combustion chamber liner having failure activated cooling and dectection system
US20050241148A1 (en) * 2004-04-28 2005-11-03 Siemens Westinghouse Power Corporation Thermally insulating layer incorporating a distinguishing agent and method for inspecting the same
US20060177665A1 (en) * 2003-08-13 2006-08-10 Siemens Aktiengesellschaft Arrangement of at least one heat-insulation layer on a carrier body
GB2455850A (en) * 2007-12-19 2009-06-24 Gen Electric Method for allowing for improved inspection of components having barrier coatings
US20120167664A1 (en) * 2010-12-30 2012-07-05 General Electric Company Methods, systems and apparatus for detecting material defects in combustors of combustion turbine engines
EP2698503A1 (en) * 2012-08-17 2014-02-19 Siemens Aktiengesellschaft Turbomachine component marking

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3797896A (en) * 1971-04-21 1974-03-19 Avco Corp Bearing for wear detection
US4604604A (en) * 1984-06-29 1986-08-05 International Harvester Company Vapor emitting wear indicator
US6527849B2 (en) * 1990-06-19 2003-03-04 Carolyn M. Dry Self-repairing, reinforced matrix materials
US5451110A (en) * 1993-12-28 1995-09-19 Syedala Industries, Inc. Bearing wear indicator
FR2732338B1 (fr) * 1995-03-28 1997-06-13 Europ Propulsion Materiau composite protege contre l'oxydation par matrice auto-cicatrisante et son procede de fabrication
EP0943867B1 (de) * 1998-03-17 2002-12-18 ALSTOM (Switzerland) Ltd Keramische Auskleidung einer Brennkammer
WO2000006796A1 (en) * 1998-07-27 2000-02-10 Imperial College Of Science, Technology And Medicine Thermal barrier coating with thermoluminescent indicator material embedded therein
US9534783B2 (en) * 2011-07-21 2017-01-03 United Technologies Corporation Insert adjacent to a heat shield element for a gas turbine engine combustor
WO2014187659A1 (de) 2013-05-21 2014-11-27 Siemens Aktiengesellschaft Hitzeschildkachel für einen hitzeschild einer brennkammer
FR3007028B1 (fr) * 2013-06-13 2015-07-03 Herakles Barriere environnementale pour substrat refractaire contenant du silicium
US9804058B2 (en) * 2014-02-27 2017-10-31 Pratt & Whitney Canada Corp. Method of facilitating visual detection of a crack in a component of a gas turbine engine
US9938839B2 (en) * 2014-03-14 2018-04-10 General Electric Company Articles having reduced expansion and hermetic environmental barrier coatings and methods for their manufacture

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4838030A (en) * 1987-08-06 1989-06-13 Avco Corporation Combustion chamber liner having failure activated cooling and dectection system
US20060177665A1 (en) * 2003-08-13 2006-08-10 Siemens Aktiengesellschaft Arrangement of at least one heat-insulation layer on a carrier body
US20050241148A1 (en) * 2004-04-28 2005-11-03 Siemens Westinghouse Power Corporation Thermally insulating layer incorporating a distinguishing agent and method for inspecting the same
GB2455850A (en) * 2007-12-19 2009-06-24 Gen Electric Method for allowing for improved inspection of components having barrier coatings
US20120167664A1 (en) * 2010-12-30 2012-07-05 General Electric Company Methods, systems and apparatus for detecting material defects in combustors of combustion turbine engines
EP2698503A1 (en) * 2012-08-17 2014-02-19 Siemens Aktiengesellschaft Turbomachine component marking

Also Published As

Publication number Publication date
US10808931B2 (en) 2020-10-20
CN108240638B (zh) 2022-07-08
EP3339737B1 (en) 2019-10-23
CN108240638A (zh) 2018-07-03
US20180179958A1 (en) 2018-06-28
EP3339737A1 (en) 2018-06-27

Similar Documents

Publication Publication Date Title
GB201610878D0 (en) Gas turbine engine
GB2551551B (en) Gas Turbine Engine
GB201600180D0 (en) Gas turbine engine
GB201512900D0 (en) Gas turbine engine
GB201610879D0 (en) Gas turbine engine
GB2545538B (en) A gas turbine engine having sequential combustion
DK3226365T3 (da) Gasudledningsrør
GB201616108D0 (en) Gas turbine engine
HK1247977A1 (zh) 燃氣渦輪發動機
GB201418396D0 (en) Gas turbine engine support structures
GB201619960D0 (en) Gas turbine engine
GB201603254D0 (en) Gas turbine engine
GB2550201B (en) Gas turbine engine
GB201609702D0 (en) Gas turbine engine
GB201512494D0 (en) Gas turbine engine
GB201510167D0 (en) Gas turbine engine
GB201618454D0 (en) Gas turbine engine
GB201616197D0 (en) Gas turbine engine
GB201614888D0 (en) Gas turbine engine
GB2549368B (en) A turbine engine combustion chamber
GB201618016D0 (en) Gas turbine engine
GB201616613D0 (en) Gas turbine engine
GB201614889D0 (en) Gas turbine engine
IT201600130851A1 (it) Piastrella termoisolante per camere di combustione di turbine a gas
GB2571891B (en) Gas turbine engine