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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| Main Authors | , , |
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| Format | Patent |
| Language | English |
| Published |
16.04.2020
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| Subjects | |
| Online Access | Get full text |
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| Abstract | 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. |
|---|---|
| AbstractList | 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. |
| Author | BENSLAMA, Yanis BELMONTE, Olivier LEVISSE, Paul Ghislain Albert |
| Author_xml | – fullname: BELMONTE, Olivier – fullname: LEVISSE, Paul Ghislain Albert – fullname: BENSLAMA, Yanis |
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| Notes | Application Number: US201916596609 |
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| PublicationDateYYYYMMDD | 2020-04-16 |
| PublicationDate_xml | – month: 04 year: 2020 text: 20200416 day: 16 |
| PublicationDecade | 2020 |
| PublicationYear | 2020 |
| RelatedCompanies | SAFRAN AIRCRAFT ENGINES |
| RelatedCompanies_xml | – name: SAFRAN AIRCRAFT ENGINES |
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| Snippet | 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... |
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| SubjectTerms | 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 | TURBINE ENGINE WITH A CONTRA-ROTATING TURBINE FOR AN AIRCRAFT |
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