-
Hot, high-pressure is bled (extracted) from the compressor section of the aircraft’s engine.
Fighter Compression System
-
high stage is used since the pressure here will be higher than from the low stage.
Low Throttle Settings:
-
the low stage will supply the bleed air since the pressure & temp. will be sufficient the operate the Environmental Control System (ECS) on the acft.
High Throttle settings:
-
SPRING LOADED CLOSED
HOT AIR VALVE
-
SPRING LOADED OPEN
COLD AIR VALVE
-
used to reg. pressure from there engine compressor section during low throttle settings.
+ Approx. 1100 degrees F @ MAX throttle settings
+ valve OPEN idle & low throttle
+ electrically controlled by the Air Source SW.
+ pneumatically (air) actuated OPEN.
+ spring actuated CLOSED.
+ regulates the output pressure to 50-65 PSIG.
High Stage Bleed Air Regulator & SOV
-
used to regulate the pressure form the engine’s compressor section during high throttle settings.
+ electrically controlled by the Air Source SW.
+ pneumatically (air) actuated CLOSED.
+ spring actuated OPEN.
+ regulates the output pressure to 80-90 PSIG.
Low Stage Bleed Air Regulator & SOV
-
used to determine which stage of compression will be used to supply bleed air for ECS operation.
+ located in the left main landing gear wheel well.
+ senses & compares pressures @ low stage of
compression w/ pressures downstream of the
variable Air Pressure Reg. SOV. (Change Over)
> When adequate pressure is available @ low stage of compression.
IT will provide an electrical signal to the EDC S/C {THE BRAIN}
> The EDC S/C will signal the high stage bleed air regulator & SOV to close. <
> The closing of the high stage valve allows the low stage reg. & sob to begin reg’n the pressure from the engine’s compressor section <
Environmental Digital Control Differential Pressure Transducer (EDC DPT)
-
prevents high stage air from entering the low stage duct system.
+ located in the low stage bleed air duct.
+ Allows Air to flow in one direction only!
Bleed Air Check Valve
-
used to operate the ECS.
( COLD AIR VALVE )
+electrically controlled by the Air Source Switch.
- pneumatically actuated CLOSED
+ spring - actuated OPEN
- regulates output pressure btwn 25- 70 PSI.
+ this output pressures used to operate the ECS.
> The output pressure of the VAPR is controlled by the EDC C/T <
Variable Air Pressure Regulator & SOV. ( VAPR SOV )
-
indicates a malfunction of either high or low stage bleed air pressure regulator & sov’s.
+ POP-UP type indicator
- RESET only after malfunction is repaired
- a manual reset button located in the jot air duct down stream of the high & low stage of bleed air regulator & sov’s.
+ if the sys. pressure reaches 95-103 PSIG for more than 20-60 sec. IT will extend.
Over-pressure Indicator
-
converts pneumatic signals to electrical signals & vice vera.
+ DIRECTLY controls the flow of serve air to operate the VAPR, therefore it controls the output pressure of the VAPR.
+ responds to upstream bleed air pressure & electrical cabin airflow demand signals from the EDC S/C.
- tells “BRAIN” how much air is in the system.
+ gives and/or takes away servo air to/from VAPR
Environmental Digital Control (EDC) Converter/ Transducer [EDC C/T]
-
used to minimize sys. shutdowns caused by excessive bleed air temps. { 370 - 475 degrees F }
- does so by providing warm air manifold temp. signals to the EDC S/C
> if temp. in the manifold reaches 475 degree F, the EDC S/C will place the ECS in the cutback mode <
Warm Manifold Temperature Sensor
-
____________ & ______________ are the only temp. sensors that can actuate ‘CUTBACK MODE’.
Turbine Inlet & Warm Air Manifold
-
high stage bleed air regulator & sov is energized CLOSED. Allowing the ECS to operate using lower pressure & lower temperature air form the low stage of compression.
Cutback Mode (Warm Manifold Temperature Sensor)
-
increases the cooling efficacy of the heat exchangers when opened.
- required when the aircraft is on the ground, during low airspeeds or during excessive temps @ high airspeeds.
+ ‘The Brain’ is the controller { RAM AIR - primary cooling }
+ is energized CLOSED & de-energized OPEN.
+ controlled by the EDC S/C during [normals operation]
> in response (FEEDS) to airspeeds inputs from CADC < aka MACH & ALTITUDE
Ejector Shutoff Valve {SOV}
-
Airspeeds decreased flow 160 knots the EDC S/C _____ the ejector SOV.
opens
-
Airspeeds above 160 knots the EDC S/C will direct the ejector SOV to ____ in response to overheat signals from { 2 temp sensors _ & _ ?)
OPEN, compressor inlet & turbine inlet
-
a low pressure area is created behind ejector nozzles.
- low pressure will draw +++ ram air over the heat exchanger to increase their cooling efficiency.
1) GND - 160 knots = OPEN
2) RE-OPENS - overheat condition - IN FLT.
Ejector SOV (In open)
-
ALL TEMP SENSORS EXCEPT ____ & ____ SENSORS, SEND SIGNALS TO THE BRAIN
CABIN & DUCT
-
monitors the compressor inlet duct temperature
+ directs a signal to the EDC S/C for controlling ejector SOV & VAPR operations.
+ minimizes sys. shutdowns
> The EDC S/C will open the ejector SOV to increase ram airflow over the heat exchangers when compressor inlet temperatures increase above 400 degrees F. <
(STAGE 1) (RESET)
> The ejector SOV will be closed when the compressor inlet temp decreases to 370 degrees F. or less (overheat protection) <
(STAGE 2) (ACTIVE)
- If the compressor inlet temp climbs above 465 degrees F, the EDC S/C signals the EDC C/T to reduce the VAPR output.
Compressor Inlet Temp. Sensor
-
* Reduced bleed airflow through the heat exchangers will reduce the _________. *
temperature
-
-monitors turbine inlet duct temperature.
+ directs a signal to the EDC S/C for controlling SOV, VAPR, & cutback mode operations.
- prevents over-speed conditions
- only has (CUTBACK)
> The EDC S/C will open the ejector SOV to increase ram airflow over the heat exchangers when turbine inlet temperature increases above 180 degrees F. <
> The ejector SOV will be closed when the turbine inlet temperature decreases to 180 degrees F or less (over heat protection).
225 degrees - STAGE 1 & 2
280 degrees - CUT BACK MODE
Overheat Condition Stages:
Stage 1- Brain Opens EJT
Stage 2 - Brain closes VAPR through EDC C/T w/ 25 PSI.
Stage 3 - CUTBACK ‘Brain’ Shuts Down HIGH STAGE (to force use of low-stage)
Turbine Inlet Temperature Sensor
-
- to compute the cabin airflow demand & provide an output signal (electrical) to the EDC converter/transducer to modulate the output pressure of the VAPR SOV (modulating bleed airflow)
+an electronic digital controller
+ it receives & processes the following input signals:
- Cabin airflow
- Cabin air supply inlet duct temperatures
- Compressor & turbine inlet temperature
- Total (ram air) temperature
- Available bleed air pressure
- CADC: airspeed & altitude
- Warm air manifold temperature sensor
+ minimizes sys. shutdowns by monitoring temps during sys. operation of bleed air & ac sys’s.
+ provides the ECS w/ over temp protection by controlling ejector SOV ops.
+ operates the ECS in ‘cutback’ mode {during extreme sys. operating temps.}
-ejector valve
- high/ low stage
- cutback mode
- AC/TEMP control functions
Environmental Digital Control Sensor Controller (EDC S/C) " THE BRAIN "
-
- a pneumatic connector that provides a connection for an external air source during ground operation & checkout of the ECS w/o starting the engine.
+ located in the left man in wheel well & incorporates a dual check valve to prevent discharge of engine bleed air during flight & ground operation of the acft engines.
Ground Service Receptacle/ Check Valve
-
- a plug-in type replay located in the air conditioning matrix.
+ Shuts All AC Sys. Down
+ energized during excessive temperature conditions to prevent damage to the aircraft.
- energized replay will cause the sys. to shutdown by completing an electrical circuit to the solenoids of the 3 primary bleed air valves (low stage, high stage & VAPR).
+the components used to energize the relay are:
-Hot Air Bypass Thermostatic SW
-Turbine Inlet Thermostatic SW
- Cockpit Supply Thermostatic SW
- Fuel Pressure Supply Thermostatic SW.
Air Over-Temperature Relay
-
- located in the warm air manifold this is normally open thermostat limits maximum temperature in the manifold.
+ when it exceeds 510 degrees F, the thermostatic sw completes an electrical circuit to energize the air over-temperature relay ( shutting down the ECS )
Hot Air Bypass Thermostatic SW
-
located in the inlet duct of the turbine (expansion side), this switch is normally open.
- When temperature increases 310(+10)degrees F, the thermostat closes
+ energizing the air over-temperature replay { shutting down the bleed air sys.}
- REOPENS when the temperature decreases to 270 degrees F
+ Bleed air system valves are re-reopened, restoring ECS operation.
Turbine Inlet Thermostatic SW
-
- located in the cabin air supply inlet duct the cabin temperature thermostatic sw limits the maximum cabin temp.
+ will energize the air over-temp relay
+ automatically shut down the bleed air sys.
+ sw is normally open
+ will close if temp in the duct reaches 200 degrees F.
Cockpit Supply Thermostatic SW
-
- located in the right wheel well in the fuel tank pressurization line.
+ When temperature increases to 450 degrees F, the thermostat closes, energizing the air over-temperature relay & shuts down the bleed air sys.
- The sw reopens when the temp decreases to 380 degrees F, allowing the 3 primary bleed air valves to re-open & restore ECS operation.
Fuel Pressure Supply Thermostatic SW
-
energizes the 3 primary bleed air valves closed
& Ram Air Shutoff Valve open. (Requires air to close)
A/S SW: OFF
-
+ de-energizes the three primary bleed air valves open
+ energizes the Ram Air Shutoff Valve closed.
A/S SW: NORM
-
normal air conditioning continues
& the the solenoid on the Cabin Pressure Relief
& Dump Valve is energized dumping cabin pressure.
A/S SW: DUMP
-
energizes the 3 primary bleed air valves closed
de-energized the Ram Air SOV open
- ambient air enters to ventilate the cabin & the equipment compartments.
+ The Relief & Dump Valve is also energized open allowing the ram air to vent from the cabin.
A/S SW: RAM
-
Where is the Source Servo Air System?
Inlet side of compress or Turbine
-
is used to actuate valves open or closed.
+ provides air signals to the air conditioning sys. valves.
Servo Air System
-
Servo air opened & Spring loaded closed
HOT VALVES
-
SPRING LOADED OPEN & SERVO AIR CLOSED
COLD AIR VALVES
-
+ filters the servo air prior to entering the servo air regulator valve
+ done to ensure no particles enter the servo air system.
* Time Changed
* Phase Inspections
[disposable wire mesh unit]
Servo Filter
-
+ regulates the servo airflow into the system
Servo Air Regulator
-
Air pressure entering the Servo Air Regulator is between __ to __ PSIG.
25 to 70
-
Servo Air Regulator decreases the pressure to __ to __ PSIG.
16 to 20
-
If airflow is blocked, the Servo Air Regulator has an ____ ________ ______ setting of __ PSIG.
over pressure relief , 25 PSIG
-
- constructed on INCONEL & STEEL
- covered w/ insulation
Hot Air Ducting
-
- constructed w/ ALUMINUM ALLOY
- covered w/ insulation
Cold Air Ducting
-
- Used on HOT air ducts
- Reusable E-seal gasket
V-coupling
-
COLD AIR DUCTS
Low pressure flexible
-
WARM & COLD air ducts
- used where high pressure or frequent removal is anticipated
Fixed Cavity flexible couplings
-
Blue - low temp apps
Red - used on al apps.
Packings (O-rings)
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