VARIABLE GEOMETRY ENGINE INLET FOR HIGH SPEED AIRCRAFT
An aircraft includes an airframe, an engine mounted to the airframe, and an engine inlet for receiving an ambient airflow and providing the ambient airflow to the engine. An amount of airflow provided to the engine inlet is controllable.
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Main Author | |
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Format | Patent |
Language | English |
Published |
29.11.2018
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Subjects | |
Online Access | Get full text |
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Summary: | An aircraft includes an airframe, an engine mounted to the airframe, and an engine inlet for receiving an ambient airflow and providing the ambient airflow to the engine. An amount of airflow provided to the engine inlet is controllable. |
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Bibliography: | Application Number: US201715603895 |