GE Power Heavy-Duty Gas Turbine Operating and Maintenance Considerations GER-362OP
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Publication Title | GE Power Heavy-Duty Gas Turbine Operating and Maintenance Considerations GER-362OP
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Page | 056 Direct Access
Borescope
Compressor
Bleeds/Blading
Inner Segments
Inner Liner
Inner Casing
Compressor
Inlet
Compressor
Bearing
Turbine
First Blade
Hot Gas
Casing
Figure E-7. GT11N2 (Sample B – Fleet with Silo Combustor)
Direct Access
Borescope
Combustor Segments/
Burners and Shells
Turbine First Stage
Compressor
Bleeds/Blading/MP3
Compressor
Inlet
Compressor
Bearing
Turbine Blading
(Plugs in S3N/S4N)
Combustor Inner Parts
Turbine Inlet
(opening of combustor dome)
Buckets 1 – 4
(Plugs in S2N/S3N/S4N)
Turbine Last Blade
Exhause Housing
Turbine Bearing
Turbine Bearing
Figure E-8. GT13E2 (E-Fleet with Annular Combustor
Direct Access
Borescope
PK2 Plenum
EV Combustor
HPT S1N/S1B
(1x EV Lance Access)
SEV Combustor
HPT S1B/OGV LPT S1N
(3x SEV Lance Access)
LPT Blading
(Plugs in S2N/S3N/S4N)
Turbine Last Blade
Exhause Housing
Turbine Bearing
Compressor
Inlet
Compressor
Bearing
Compressor Bleeds/Blading
(MP2/3/4)
Figure E-9. GT24/GT26 (F – Fleet with Annular Combustor)
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