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This page displays all 「FI」 in main group F02C3/00. |
HB:Handbook | ||||
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CC:Concordance | |||||
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Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) | HB | CC | 3G104 | |
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.using exhaust-gas pressure in a pressure exchanger to compress combustion-air (pressure exchangers per seF04F 13/00) | HB | CC | 3G104 | |
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.having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) [1, 5, 2006.01] | HB | CC | 3G104 | |
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..having compressor and turbine passages in a single rotor (F02C 3/073 takes precedence) [3, 2006.01] | HB | CC | 3G104 | |
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...the compressor and the turbine being of the radial flow type [3] | HB | CC | 3G104 | |
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..the compressor being of the positive-displacement type [3] | HB | CC | 3G104 | |
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..the compressor comprising only axial stages (F02C 3/10 takes precedence) [3] | HB | CC | 3G104 | |
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...having counter-rotating rotors (F02C 3/073 takes precedence) [3] | HB | CC | 3G104 | |
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...the compressor and turbine stages being concentric [3] | HB | CC | 3G104 | |
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..the compressor comprising at least one radial stage (F02C 3/10 takes precedence) [3] | HB | CC | 3G104 | |
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...of the centripetal type [3] | HB | CC | 3G104 | |
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..with another turbine driving an output shaft but not driving the compressor | HB | CC | 3G104 | |
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...related to control | HB | CC | 3G104 | |
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..with two or more rotors connected by power transmission [5] | HB | CC | 3G104 | |
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...with variable power transmission between rotors [5] | HB | CC | 3G104 | |
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..having variable working fluid interconnections between turbines or compressors or stages of different rotors [5] | HB | CC | 3G104 | |
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.characterised by the arrangement of the combustion chamber in the plant (combustion chambers per seF23R) [3] | HB | CC | 3G104 | |
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..the combustion chambers being formed at least partly in the turbine rotor | HB | CC | 3G104 | |
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.using a special fuel, oxidant, or dilution fluid to generate the combustion products [3] | HB | CC | 3G104 | |
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..the fuel or oxidant being gaseous at standard temperature and pressure (F02C 3/28 takes precedence) [3] | HB | CC | 3G104 | |
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..the fuel or oxidant being liquid at standard temperature and pressure [3] | HB | CC | 3G104 | |
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related to the structure of the injection device or burner | HB | CC | 3G104 | |
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Others | HB | CC | 3G104 | |
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..the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension | HB | CC | 3G104 | |
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...using a separate gas producer for gasifying the fuel before combustion [3] | HB | CC | 3G104 | |
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..Adding water, steam or other fluids to the combustible ingredients or to the working fluid before discharge from the turbine (heating of air intakes to prevent icing F02C 7/047) [3] | HB | CC | 3G104 | |
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Supply into the burner | HB | CC | 3G104 | |
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.Water supplied | HB | CC | 3G104 | |
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.Steam supplied | HB | CC | 3G104 | |
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.Air or exhaust gas supplied | HB | CC | 3G104 | |
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Others | HB | CC | 3G104 | |
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.Inducing air flow by fluid jet, e.g. ejector action [3] | HB | CC | 3G104 | |
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.with recycling of part of the working fluid, i.e. semiclosed cycles with combustion products in the closed part of the cycle [3, 2006.01] | HB | CC | 3G104 | |
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.Open cycles [3] | HB | CC | 3G104 | |