BOEING 737-800/900ER Air Cycle Machine Operation

Air Cycle Machine Operation
The two air condition packs provide “conditioned” air (temp and moisture) to the air condition system. They are supplied with bleed air from the bleed manifold, normally from the APU or the high pressure compressor of the engines. Hot air flowing into the packs has a temperature of ± 199 – 227°C, controlled by the engine BASOV and the pre-cooler. To get to the normal temperature range of 18 – 30°C of the AC system, it needs to be cooled which is accomplished by the two packs.
Let’s look at the flow of air through a pack explaining the components the air passes. Air enters the pack through the PACK FLOW CONTROL VALVE and can go in two directions, into the cooling circuit or it by-passes the so called ACM (air cycle machine) circuitry.
The cooling cycle starts at the “primary” (air–to–air) heat exchangers that cools the air. The heat exchanger works like a car radiator but exchanges hot bleed air to the ram air duct airflow. On the ground by the way, duct airflow is created by a fan which is driven off the ACM. Next the air “hits” the compressor of the ACM which turns the compressor and turbine resulting in an increase of pressure and temperature. Another “secondary” heat exchanger cools the air again, where after the following components in the manifold are to “create” and extract water from the air. A “secondary” water extractor drains water from the manifold, a re-heater pre cools the air before it enters the condenser and warms the air (from the 2nd water extractor) before it enters the turbine to increase efficiency of that turbine operation. The condenser creates water droplets in the air where after the “primary” water extractor removes water by creating a swirling motion, “centrifuging” that water to the outer collector wall where it is collected and relieved in the ram air duct adding in cooling at the heat exchangers. The last component of the pack is the expansion turbine which can cool the air to below the freezing level as a function of very fast expansion (extracting energy) of the air. Finally the air is mixed with by-pass air representing the pack control requested output temperature.
The pack is protected against a request of a too high demand of cool air, thereby overloading that pack. This is accomplished by several temperature sensors detecting over temperatures in the cooling cycle causing the pack to trip off line. If this happens, it closes the pack flow control valve indicated by the PACK OFF indication on the bleed panel together with a MASTER CAUTION light (AIR COND). The solution to this problem is to let the pack cool down and selecting a warmer temperature before resetting and “unloading” the tripped pack or else the overload/overtemp will occur again.
Water is extracted from the air to protect the avionics in the aircraft against moisture, to prevent mold to form and against oxidation of metal components.
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