Aircraft Bypass Duct Heat Exchanger
A turbine engine heat exchanger has an array of heat exchanger plates mounted to an inner case wall for providing heat transfer from a bleed flowpath to a bypass flowpath. Each plate has: first and second faces along the bypass flowpath; a proximal edge mounted to the inner case wall; an inlet along...
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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
16.09.2021
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Subjects | |
Online Access | Get full text |
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Summary: | A turbine engine heat exchanger has an array of heat exchanger plates mounted to an inner case wall for providing heat transfer from a bleed flowpath to a bypass flowpath. Each plate has: first and second faces along the bypass flowpath; a proximal edge mounted to the inner case wall; an inlet along the proximal edge; an outlet along the proximal edge; and a branch segment of the bleed flowpath passing from the inlet to the outlet |
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Bibliography: | Application Number: US202017139174 |