Primary heat exchanger crossover bypass manifold
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United States of America Patent
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Jan 23, 2018
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N/A
app pub date -
Sep 24, 2012
filing date -
Sep 24, 2012
priority date (Note) -
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Abstract
An aircraft is provided including an environmental control system (ECS) having a first ECS pack and a second ECS pack. A duct couples the first ECS pack to the second ECS pack. The duct includes a first bypass conduit configured to form a bypass around a first primary heat exchanger of the first ECS pack. A second bypass conduit configured to form a bypass around a second primary heat exchanger of the second ECS pack. The duct includes a crossover conduit extending between the first bypass conduit and the second bypass conduit. The duct includes a plurality of valves for selectively controlling a flow between the first bypass conduit and the second bypass conduit.
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