TURBINE ENGINE WITH A CONTRA-ROTATING TURBINE FOR AN AIRCRAFT

characterised in that said bearings are all situated downstream from the trailing edge of the last turbine wheel of the contra-rotating turbine and upstream from the reduction gear.

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Bibliographic Details
Main Authors BELMONTE, Olivier, LEVISSE, Paul Ghislain Albert, BENSLAMA, Yanis
Format Patent
LanguageEnglish
Published 16.04.2020
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
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Summary:characterised in that said bearings are all situated downstream from the trailing edge of the last turbine wheel of the contra-rotating turbine and upstream from the reduction gear.
Bibliography:Application Number: US201916596609