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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Hauptverfasser: LEMARCHAND, Kévin, Morgane, TANTOT, Nicolas, Jérôme, Jean, CHARIER, Gilles, Alain, Marie, VLASTUIN, Jonathan, Evert, NOWAKOWSKI, Nathalie, YESILCIMEN, Henri
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creator LEMARCHAND, Kévin, Morgane
TANTOT, Nicolas, Jérôme, Jean
CHARIER, Gilles, Alain, Marie
VLASTUIN, Jonathan, Evert
NOWAKOWSKI, Nathalie
YESILCIMEN, Henri
description 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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language eng ; fre ; ger
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title TURBOJET WITH STEP-DOWN MECHANISM
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