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    Progress on the European Gas Turbine Program “AGATA”

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 001::page 179
    Author:
    R. Gabrielsson
    ,
    G. Holmqvist
    DOI: 10.1115/1.2818072
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The four-year European Gas Turbine Program “AGATA” was started in January 1993 with the objective of developing three critical components aimed at a 60 kW turbogenerator in an hybrid electric vehicle: a catalytic combustor, a radial turbine wheel and a static heat exchanger. The AGATA partners represent car manufacturers as well as companies and research institutes in the turbine, catalyst, and ceramic material fields in both France and Sweden. This paper outlines the main results of the AGATA project for the first three-year period. Experimental verification of the components started during the third year of the program. A high-pressure/temperature test rig for the combustor and the heat exchanger tests has been built and is now being commissioned. A high-temperature turbine spin rig will be ready late 1995. The turbine wheel design is completed and ceramic Si3 N4 spin disks have been manufactured by injection molding and Hot Isostatic Pressing (HIP). A straight blade design has been selected and FEM calculations have indicated that stress levels that occur during a cold start are below 300 MPa. The catalytic combustor final design for full-scale testing has been defined. Due to the high operating temperature, 1350°C, catalyst pilot tests have included aging, activity, and strength tests. Based on these tests, substrate and active materials have been selected. Initial full-scale tests including LDV measurements in the premix duct will start late 1995. The heat exchanger design has also been defined. This is based on a high-efficiency plate recuperator design. One critical item is the ceramic thermoplastic extrusion manufacturing method for the extremely thin exchanger plates another is the bonding technique: ceramic to ceramic and ceramic to metal. Significant progress on these two items has been achieved. The manufacturing of quarter scale prototypes is now in process.
    keyword(s): Gas turbines , Ceramics , Design , Turbines , Heat exchangers , Combustion chambers , Particle spin , Manufacturing , Catalysts , Wheels , Laser Doppler anemometry , Light trucks , High temperature , Operating temperature , Ducts , Finite element model , Hot pressing , Hybrid electric vehicles , Plates (structures) , Testing , Disks , Active materials , Blades , Bonding , Extruding , Turbogenerators , Stress , Injection molding , High pressure (Physics) , Finite element methods , Engineering prototypes , Measurement , Temperature AND Metals ,
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      Progress on the European Gas Turbine Program “AGATA”

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    https://yetl.yabesh.ir/yetl1/handle/yetl/120484
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. Gabrielsson
    contributor authorG. Holmqvist
    date accessioned2017-05-08T23:56:40Z
    date available2017-05-08T23:56:40Z
    date copyrightJanuary, 1998
    date issued1998
    identifier issn1528-8919
    identifier otherJETPEZ-26775#179_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120484
    description abstractThe four-year European Gas Turbine Program “AGATA” was started in January 1993 with the objective of developing three critical components aimed at a 60 kW turbogenerator in an hybrid electric vehicle: a catalytic combustor, a radial turbine wheel and a static heat exchanger. The AGATA partners represent car manufacturers as well as companies and research institutes in the turbine, catalyst, and ceramic material fields in both France and Sweden. This paper outlines the main results of the AGATA project for the first three-year period. Experimental verification of the components started during the third year of the program. A high-pressure/temperature test rig for the combustor and the heat exchanger tests has been built and is now being commissioned. A high-temperature turbine spin rig will be ready late 1995. The turbine wheel design is completed and ceramic Si3 N4 spin disks have been manufactured by injection molding and Hot Isostatic Pressing (HIP). A straight blade design has been selected and FEM calculations have indicated that stress levels that occur during a cold start are below 300 MPa. The catalytic combustor final design for full-scale testing has been defined. Due to the high operating temperature, 1350°C, catalyst pilot tests have included aging, activity, and strength tests. Based on these tests, substrate and active materials have been selected. Initial full-scale tests including LDV measurements in the premix duct will start late 1995. The heat exchanger design has also been defined. This is based on a high-efficiency plate recuperator design. One critical item is the ceramic thermoplastic extrusion manufacturing method for the extremely thin exchanger plates another is the bonding technique: ceramic to ceramic and ceramic to metal. Significant progress on these two items has been achieved. The manufacturing of quarter scale prototypes is now in process.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleProgress on the European Gas Turbine Program “AGATA”
    typeJournal Paper
    journal volume120
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818072
    journal fristpage179
    journal lastpage185
    identifier eissn0742-4795
    keywordsGas turbines
    keywordsCeramics
    keywordsDesign
    keywordsTurbines
    keywordsHeat exchangers
    keywordsCombustion chambers
    keywordsParticle spin
    keywordsManufacturing
    keywordsCatalysts
    keywordsWheels
    keywordsLaser Doppler anemometry
    keywordsLight trucks
    keywordsHigh temperature
    keywordsOperating temperature
    keywordsDucts
    keywordsFinite element model
    keywordsHot pressing
    keywordsHybrid electric vehicles
    keywordsPlates (structures)
    keywordsTesting
    keywordsDisks
    keywordsActive materials
    keywordsBlades
    keywordsBonding
    keywordsExtruding
    keywordsTurbogenerators
    keywordsStress
    keywordsInjection molding
    keywordsHigh pressure (Physics)
    keywordsFinite element methods
    keywordsEngineering prototypes
    keywordsMeasurement
    keywordsTemperature AND Metals
    treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 001
    contenttypeFulltext
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