Control of clearance between aircraft rotor blades and a casing
A device for controlling clearance between the tips of rotating blades of an aircraft turbomachine and a casing. An air circulation path allows air to be blown onto the casing in order to change its temperature. In addition, heating means heat the circulating air.
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Main Authors | , , , , |
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Format | Patent |
Language | English |
Published |
03.05.2022
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Subjects | |
Online Access | Get full text |
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Summary: | A device for controlling clearance between the tips of rotating blades of an aircraft turbomachine and a casing. An air circulation path allows air to be blown onto the casing in order to change its temperature. In addition, heating means heat the circulating air. |
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Bibliography: | Application Number: US202016875376 |