Triebwerksgondel (Nacelle) (Nacelle)
Embed This Widget
Add the script tag and a data attribute to embed this widget.
Embed via iframe for maximum compatibility.
<iframe src="https://planefyi.com/iframe/glossary/nacelle/" width="420" height="400" frameborder="0" style="border:0;border-radius:10px;max-width:100%" loading="lazy"></iframe>
Paste this URL in WordPress, Medium, or any oEmbed-compatible platform.
https://planefyi.com/glossary/nacelle/
Add a dynamic SVG badge to your README or docs.
[](https://planefyi.com/glossary/nacelle/)
Use the native HTML custom element.
Definition
Die aerodynamische Verkleidung, die ein Flugzeugtriebwerk umgibt und schützt, Widerstand und Lärm reduziert.
Was ist eine Triebwerksgondel?
A nacelle is the streamlined enclosure surrounding an aircraft engine. Mounted on pylons beneath the wings or integrated into the fuselage (as on the Boeing 727 or some regional jets), nacelles serve multiple critical functions: they reduce aerodynamic drag, direct airflow into and through the engine, contain engine noise, and house Thrust Reverser mechanisms. Modern nacelles are complex structures engineered to exacting tolerances.
Funktionsweise
A nacelle consists of several structural and functional components:
- Inlet (intake cowl): The forward lip that captures incoming air and smoothly accelerates it into the fan. Design is critical — lip shape affects engine stability across all flight attitudes and crosswind conditions.
- Fan cowl: Surrounds the fan and booster stages. Contains fire suppression ports and engine access panels for maintenance.
- Thrust reverser cowl: The aft section that translates rearward on cascade-type designs to open reverser cascade vanes.
- Core cowl: Surrounds the engine core, providing a duct for bypass air and housing fire detection systems.
- Exhaust nozzle: The convergent duct at the rear where bypass and core airstreams mix before expulsion.
Acoustic liners bonded to the inner surfaces of the nacelle absorb fan and turbine noise. Modern nacelles achieve 20–30 dB noise reduction compared to unlined structures. Materials are predominantly carbon-fiber-reinforced polymer (CFRP), aluminum alloys, and titanium for heat-exposed sections.
Leistungsdaten
- Fan diameter (determines nacelle diameter): CFM56: 61 in → LEAP-1B: 69 in → GE9X: 134 in
- Weight: A CFM LEAP nacelle system weighs approximately 1,200–1,500 kg per engine
- Noise attenuation: Up to 30 EPNdB (effective perceived noise) reduction via acoustic liners
- Ground clearance constraint: Nacelle diameter limits bypass ratio on underwing engines (key reason 737 MAX LEAP engines sit forward and above wing centerline)
Flugzeugbeispiele
- Boeing 737 MAX: Distinctive "D-shaped" nacelle inlet due to ground clearance limitations — LEAP-1B engine moved forward and up to fit under the wing
- Airbus A320neo: Circular nacelle for CFM LEAP-1A or PW1100G, lower-slung than 737 MAX
- Boeing 777X: World's largest commercial nacelle for the 134-inch diameter GE9X fan
- Boeing 727: Center engine embedded in tail — nacelle integrated into fuselage S-duct rather than underwing pylon
Nacelles are mounted via pylons to the wing structure. The Fan Blades inside are precisely matched to the nacelle inlet geometry for optimal airflow management.
Related Terms
Fan-Blatt
Die großen rotierenden Schaufeln vorne am Turbofan-Triebwerk, die Luft beschleunigen, um Nebenstromschub zu erzeugen.
Getriebe-Turbofan
Ein Turbofan-Design, das ein Untersetzungsgetriebe zwischen Gebläse und Niederdruckturbine verwendet, sodass jedes mit optimaler Drehzahl laufen kann.
Nebenstromverhältnis (Bypass Ratio)
Das Verhältnis des Luftmassenstroms um den Triebwerkskern zum Strom durch den Kern, ein wichtiger Effizienzindikator.
Schubumkehr
Eine mechanische Vorrichtung, die den Triebwerksabgasstrahl vorübergehend nach vorne umlenkt, um nach der Landung zu bremsen.
Turbofan-Triebwerk
Der häufigste Triebwerkstyp in der kommerziellen Luftfahrt, der mit einem großen Fan den Großteil des Schubs erzeugt.