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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| Abstract | 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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| AbstractList | 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. |
| Author | Lauder, Timothy F |
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| Notes | Application Number: US201715603895 |
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| PublicationDateYYYYMMDD | 2018-11-29 |
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| RelatedCompanies | Sikorsky Aircraft Corporation |
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| Snippet | 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... |
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| SubjectTerms | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| Title | VARIABLE GEOMETRY ENGINE INLET FOR HIGH SPEED AIRCRAFT |
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