TURBOFAN ENGINE COMPRISING A FAIRING BEING LOCATED IN THE SECONDARY FLOW CHANNEL AND HAVING A SEPARATE END ELEMENT
TURBOFAN ENGINE COMPRISING A FAIRING BEING LOCATED IN THE SECONDARY FLOW CHANNEL AND HAVING A SEPARATE END ELEMENT
- Neue Suche nach: THIES ROBERT
- Neue Suche nach: THIES ROBERT
A turbofan engine including a core engine and at least one fan by means of which fluid is guided to a primary flow channel for the core engine as well as to a secondary flow channel of the turbofan engine, wherein the secondary flow channel is provided for an outer fluid flow that is guided past the core engine, and at least one splitter fairing arranged inside the secondary flow channel around which the fluid flow is flowing during operation of the turbofan engine, which cases at least one component of the turbofan engine that is guided radially through the secondary flow channel, and which has an end element with a leading edge section that is facing towards the fluid flow and/or a trailing edge section that is positioned in the flow direction of the fluid flow.
Dokumentinformationen
TURBOFAN ENGINE COMPRISING A FAIRING BEING LOCATED IN THE SECONDARY FLOW CHANNEL AND HAVING A SEPARATE END ELEMENT
2018-02-15
Patent
Elektronische Ressource
Englisch
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
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