AIR GUIDING DEVICE AND AIRCRAFT ENGINE WITH AIR GUIDING DEVICE
An air guiding device in an aircraft engine, comprising at least one connection device of a core engine shroud with an external wall of a bypass duct of the aircraft engine is provided. At least one first air inlet opening for inflowing air is connected to a connection device or is arranged inside t...
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Format: | Patent |
Sprache: | eng |
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Zusammenfassung: | An air guiding device in an aircraft engine, comprising at least one connection device of a core engine shroud with an external wall of a bypass duct of the aircraft engine is provided. At least one first air inlet opening for inflowing air is connected to a connection device or is arranged inside the connection device. |
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