Double ended brush seal assembly for a compressor
A technology of brush seals and compressors, which is applied to the sealing of engines, components of pumping devices for elastic fluids, engine components, etc., and can solve problems such as complex and expensive seals
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[0020] FIG. 1 shows a schematic exemplary power generation system indicated by reference numeral 10 . Power generation system 10 is a gas turbine system having compressor 20 (shown in FIG. 1 ), combustor 22 and turbine 24 . Air enters power generation system 10 through air inlet 30 connected to compressor 20 (shown in FIG. 1 ) and is compressed by compressor 20 (shown in FIG. 1 ). The compressed air is then mixed with fuel by fuel nozzles 34 . Fuel nozzles 34 inject an air-fuel mixture at a specific ratio into combustor 22 for combustion. Combustion generates hot pressurized exhaust gases, which drive blades (not shown) located within turbine 24 .
[0021] 2-3 illustrate the axial brush seal assembly 54 positioned between the rotor 46 of the compressor 20 (shown in FIG. 1 ) and the compressor discharge housing barrel 42 . Axial brush seal assembly 54 serves to reduce or prevent gas flow leakage into central gas flow region 60 or high pressure packing (HPP) region 64 during ...
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