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.
Turbofan-Triebwerk mit einer im Sekundärstromkanal liegenden und ein separates Abschlusselement aufweisenden Verkleidung
Turbofan engine with cladding having a separate closing element and lying in the secondary flow channel
Turbine à double flux comprenant un habillage présentant un élément de raccord séparé et se trouvant dand un canal d'écoulement secondaire
2018-12-12
Patent
Electronic Resource
German
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 |
TURBOFAN-TRIEBWERK MIT ÜBERDRUCKKLAPPE AN EINER IM SEKUNDÄRSTROMKANAL LIEGENDEN VERKLEIDUNG
European Patent Office | 2019
|Turbofan-Triebwerk mit Überdruckklappe an einer im Sekundärstromkanal liegenden Verkleidung
European Patent Office | 2018
|Vergleichende Kreisprozessrechnungen fuer ein Propfan-/Turbofan-Triebwerk
Tema Archive | 1982
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