Engine and Engine controls Flashcards
What kind of engine do we have
T700-GE-401C front drive turboshaft engine
what are the 5 sections of the engine
inlet compressor combustor turbine exhaust
air flow through engine
through inlet cowling then to swirl vanes inlet particle separator deswirl vanes compressor combustor gas generator turbine power turbine then out
describe the compressor section
5 stage axial and single stage centrifugal system
describe the combustion section
flow through annular combustion chamber
2 igniters
12 fuel injectors
function of gas generator turbine
drives the compressor and AGB
describe the gas generator turbine
two stage air cooled high performance axial design
which turbine shaft turns inside the other
Np spins inside Ng
what does the Np turbine do
drives high speed output shaft
where is TGT sensed
between Ng and Np turbines
how much of the total airflow is used for combustion
about 30%
what is the airflow not used for combustion used for
compressor inlet temp (T2) air
compressor discharge (P3) air
combustor and turbine cooling
engine oil seal pressurization
what does the AGB drive
starter, HMU, IPS blower, ODV
alternator, eng driven fuel boost pump
goal of the engine control system
proper and complete control of the engine to maintain a constant Np and Nr
major components of engine control system
HMU
ODV
EDECU
Alternator
series of fuel flow control valves
general function of HMU
provides Ng control
general function of EDECU
trims the HMU to meet Np requirements and lessen pilot workload
What does putting the PCL in the off position do
PAS mechanically shuts off fuel at the shutoff valve in the HMU
what does putting the PCL in the idle position do
Controls HMU to auto control start sequence to get to self sustaining combustion
what does putting the PCL in fly do
sets max level of power that could be supplied if demanded
what does putting the PCL in lockout and back do
disables TGT limiting, load sharing and Np governing and allows for manual control of Np and Ng
how to get engine back to normal from lockout
idle then fly
what does the solenoid on the quadrant do
prevents moving engines past idle with rotor brake on unless the override tab is pulled
function of the load demand system
routes collective input to control HMU to auto control engine speed and provide required power