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Page Title: POWER SECTION ASSEMBLY
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GENERAL  POWERPLANT  ASSEMBLY
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TM-55-2835-209-23 Gas Turbine Engine (Auxiliary Power Unit APU) Model T 62T 40 I Part Numbers 116305-100 and 116305-200 Manual
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GEARBOX ASSEMBLY

TM  55-2835-209-23 1-14 POWER SECTION ASSEMBLY a. The power section assembly is comprised of the integrated compressor, combustion and turbine  section.  The  inte- grated compressor utilized a centrifugal impeller and dif- fuser to provide the com- pressed air for combustion and bleed air purposes. Com- pressed air is the  compressor ing (1) and is the combustion to the bleed ai when bleed air lized. Fuel is into  the  combusti contained by assembly hous- directed into chamber (2) and r outlet port flow is uti- introduced on chamber by six fuel nozzles (3) and com- bined with compressed air, thus is ignited by the igniter plug assembly (4) creating the hot gas flow that drives the turbine. b. The turbine section (5) uti- lizes a turbine nozzle to in- crease the hot gas flow velocity  and  direct  it  against the blades of the turbine wheel. The hot gases transmit energy into the turbine wheel and are discharged rearward through the turbine wheel which in turn, drives the com- pressor  and  gearbox  assembly shaft (6). 1-8

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