SG11201807178TA - Flow element and method for coating a flow element - Google Patents

Flow element and method for coating a flow element

Info

Publication number
SG11201807178TA
SG11201807178TA SG11201807178TA SG11201807178TA SG11201807178TA SG 11201807178T A SG11201807178T A SG 11201807178TA SG 11201807178T A SG11201807178T A SG 11201807178TA SG 11201807178T A SG11201807178T A SG 11201807178TA SG 11201807178T A SG11201807178T A SG 11201807178TA
Authority
SG
Singapore
Prior art keywords
flow element
coating
flow
Prior art date
Application number
SG11201807178TA
Inventor
Jan Oke Peters
Thomas Gartner
Oliver Winter
Stefan Kuntzagk
Tim Lübcke
Original Assignee
Lufthansa Technik Ag
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 Lufthansa Technik Ag filed Critical Lufthansa Technik Ag
Publication of SG11201807178TA publication Critical patent/SG11201807178TA/en

Links

Classifications

    • 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
    • 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
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00—Thermal insulation in general
    • F16L59/02—Shape or form of insulating materials, with or without coverings integral with the insulating materials
    • F16L59/029—Shape or form of insulating materials, with or without coverings integral with the insulating materials layered
    • 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
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05004—Special materials for walls or lining
    • 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
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SG11201807178TA 2016-03-01 2017-02-27 Flow element and method for coating a flow element SG11201807178TA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102016103664.1A DE102016103664A1 (en) 2016-03-01 2016-03-01 Flow element and method for coating a flow element
PCT/EP2017/054459 WO2017148843A1 (en) 2016-03-01 2017-02-27 Flow element and method for coating a flow element

Publications (1)

Publication Number Publication Date
SG11201807178TA true SG11201807178TA (en) 2018-09-27

Family

ID=58191429

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201807178TA SG11201807178TA (en) 2016-03-01 2017-02-27 Flow element and method for coating a flow element

Country Status (6)

Country Link
US (1) US10488045B2 (en)
EP (1) EP3423752B1 (en)
CN (1) CN108700296A (en)
DE (1) DE102016103664A1 (en)
SG (1) SG11201807178TA (en)
WO (1) WO2017148843A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016103664A1 (en) * 2016-03-01 2017-09-07 Lufthansa Technik Ag Flow element and method for coating a flow element

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4055705A (en) * 1976-05-14 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal barrier coating system
US4326011A (en) * 1980-02-11 1982-04-20 United Technologies Corporation Hot corrosion resistant coatings
US6296447B1 (en) * 1999-08-11 2001-10-02 General Electric Company Gas turbine component having location-dependent protective coatings thereon
EP1669545A1 (en) * 2004-12-08 2006-06-14 Siemens Aktiengesellschaft Coating system, use and method of manufacturing such a coating system
DE102005060243A1 (en) 2005-12-14 2007-06-21 Man Turbo Ag Process for coating hollow internally cooled gas turbine blades with adhesive-, zirconium oxide ceramic- and Cr diffusion layers useful in gas turbine engine technology has adhesive layer applied by plasma or high rate spraying method
WO2007140805A1 (en) * 2006-06-08 2007-12-13 Siemens Aktiengesellschaft Coated turbine component and method of coating a turbine component
US20100285415A1 (en) * 2007-11-23 2010-11-11 Boettcher Andreas Burner Element and Burner Having Aluminum Oxide Coating and Method for Coating a Burner Element
EP2143819A1 (en) * 2008-07-11 2010-01-13 Siemens Aktiengesellschaft Coating method and corrosion protection coating for turbine components
DE102011103731A1 (en) * 2011-05-31 2012-12-06 Man Diesel & Turbo Se Method for applying a protective layer, with a protective layer coated component and gas turbine with such a component
GB201205020D0 (en) * 2012-03-22 2012-05-09 Rolls Royce Plc A method of manufacturing a thermal barrier coated article
DE102012015586A1 (en) * 2012-08-08 2014-05-15 MTU Aero Engines AG Duplex phase CrAl coating for improved corrosion / oxidation protection
DE102013217627A1 (en) 2013-09-04 2015-03-05 MTU Aero Engines AG Thermal insulation layer system with corrosion and erosion protection
US20150159507A1 (en) * 2013-12-06 2015-06-11 General Electric Company Article for high temperature service
US10294803B2 (en) * 2015-03-26 2019-05-21 General Electric Company Compositions and methods of deposition of thick environmental barrier coatings on CMC blade tips
US10253984B2 (en) * 2015-04-28 2019-04-09 United Technologies Corporation Reflective coating for components
DE102016103664A1 (en) * 2016-03-01 2017-09-07 Lufthansa Technik Ag Flow element and method for coating a flow element
US20180058228A1 (en) * 2016-08-26 2018-03-01 Barson Composites Corporation Hot corrosion-resistant coatings for gas turbine components
US20180355477A1 (en) * 2017-06-07 2018-12-13 Pratt & Whitney Canada Corp. Thermal coating system with aluminide

Also Published As

Publication number Publication date
EP3423752A1 (en) 2019-01-09
WO2017148843A1 (en) 2017-09-08
US10488045B2 (en) 2019-11-26
EP3423752B1 (en) 2020-04-01
CN108700296A (en) 2018-10-23
US20190078783A1 (en) 2019-03-14
DE102016103664A1 (en) 2017-09-07

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