Turbojet with step-down mechanism
Turbojet engine includes a fan, a compressor, a combustion chamber, and a turbine configured to rotatably drive the fan via a first reduction gear and the compressor via a second reduction gear, in which an outlet of the first reduction gear is rotatably coupled to an inlet of the second reduction g...
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Main Authors | , , , , , |
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Format | Patent |
Language | English |
Published |
23.08.2022
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Subjects | |
Online Access | Get full text |
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Summary: | Turbojet engine includes a fan, a compressor, a combustion chamber, and a turbine configured to rotatably drive the fan via a first reduction gear and the compressor via a second reduction gear, in which an outlet of the first reduction gear is rotatably coupled to an inlet of the second reduction gear by a reduction shaft, the reduction shaft being supported by a bearing arranged between the first reduction gear and the second reduction gear. |
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Bibliography: | Application Number: US201917278149 |