Improved ground testing device for a turbomachine
A ground testing device for a turbomachine, including an aircraft engine (12) extending axially from an air inlet to a nozzle, a shroud (20) having an axis of revolution (A) and surrounding at least partially the engine (12) so as to create an annular air flow between the engine (12) and the shroud...
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| Main Authors | , |
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| Format | Patent |
| Language | English |
| Published |
22.05.2019
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| Subjects | |
| Online Access | Get full text |
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| Abstract | A ground testing device for a turbomachine, including an aircraft engine (12) extending axially from an air inlet to a nozzle, a shroud (20) having an axis of revolution (A) and surrounding at least partially the engine (12) so as to create an annular air flow between the engine (12) and the shroud (20) when the engine (12) is in operation, and a framework (22) allowing the shroud (20) to be supported. |
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| AbstractList | A ground testing device for a turbomachine, including an aircraft engine (12) extending axially from an air inlet to a nozzle, a shroud (20) having an axis of revolution (A) and surrounding at least partially the engine (12) so as to create an annular air flow between the engine (12) and the shroud (20) when the engine (12) is in operation, and a framework (22) allowing the shroud (20) to be supported. |
| Author | Louis Robert Baudoin Josselin David Florian Regnard |
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| Notes | Application Number: GB20180018220 |
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| PublicationDate | 20190522 |
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| PublicationYear | 2019 |
| RelatedCompanies | Safran Aircraft Engines |
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| Snippet | A ground testing device for a turbomachine, including an aircraft engine (12) extending axially from an air inlet to a nozzle, a shroud (20) having an axis of... |
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| SubjectTerms | MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
| Title | Improved ground testing device for a turbomachine |
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