Fan-Blatt (Fan Blade)
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Definition
Die großen rotierenden Schaufeln vorne am Turbofan-Triebwerk, die Luft beschleunigen, um Nebenstromschub zu erzeugen.
Was ist ein Fan-Blatt?
Fan blades are the large, swept aerofoil structures at the front of a Turbofan Engine that rotate at high speed to accelerate incoming air. They are simultaneously the first compressor stage for the engine core and the primary thrust-generating component via the bypass stream. Modern fan blades represent some of the most advanced manufacturing achievements in aerospace, combining extreme performance demands — high aerodynamic loading, bird-strike resistance, fatigue tolerance — with minimal weight.
Funktionsweise
Fan blades rotate at typically 2,500–4,000 RPM in large commercial turbofans, with blade tip speeds approaching Mach 1.0–1.4. Each blade acts as an aerofoil, generating lift in the rotational plane to accelerate airflow rearward. Key engineering features:
- Sweep and twist: Blades are swept back and twisted along their span to manage shockwave formation at transonic tip speeds and optimize pressure rise across the whole blade.
- Wide-chord design: Wider chord blades (first introduced on the Rolls-Royce RB211) eliminate the need for inter-blade snubbers (tie wires), reducing drag and weight.
- Hollow titanium or carbon fiber composite: LEAP-1B uses 3D-woven carbon fiber composite fan blades; GE90 and GE9X use carbon fiber composites with titanium leading-edge armor.
- Bird-strike certification: Must withstand ingestion of a 4 lb (1.8 kg) bird at takeoff speed without causing uncontained engine failure — tested to FAA FAR 33.76 standards.
Leistungsdaten
- Diameter: 61 inches (CFM56-7B) → 69 inches (LEAP-1B) → 134 inches (GE9X)
- Blade count: 18 blades (LEAP-1B, vs 24 on CFM56) — fewer, wider blades reduce weight and improve efficiency
- Tip speed: 450–550 m/s (Mach 1.2–1.5 at tip)
- Material weight saving: Carbon fiber composite blades are 30–40% lighter than equivalent titanium blades
- Centrifugal force at tip: Each blade experiences tens of tonnes of centrifugal force during operation
Flugzeugbeispiele
- Boeing 737 MAX / LEAP-1B: 18 carbon fiber 3D-woven composite fan blades, 69-inch diameter — 15% lighter than titanium equivalent
- Boeing 777X / GE9X: 16 composite fan blades in a 134-inch diameter fan — largest commercial engine fan ever produced
- Airbus A380 / Trent 970: 24 titanium wide-chord fan blades in 116-inch diameter fan
- Pratt & Whitney PW1000G series: 20 composite fan blades with geared architecture spinning at lower RPM for efficiency
Fan blades are enclosed within the Nacelle, which shapes the incoming airflow and provides containment in the event of a blade failure event. The Bypass Ratio determines fan diameter and, therefore, blade size.
Related Terms
Nebenstromverhältnis (Bypass Ratio)
Das Verhältnis des Luftmassenstroms um den Triebwerkskern zum Strom durch den Kern, ein wichtiger Effizienzindikator.
Triebwerksgondel (Nacelle)
Die aerodynamische Verkleidung, die ein Flugzeugtriebwerk umgibt und schützt, Widerstand und Lärm reduziert.
Turbofan mit hohem Nebenstromverhältnis
Ein Turbofan-Triebwerk mit einem Nebenstromverhältnis über 5:1, das den größten Teil der Einlassluft um den Triebwerkskern leitet, um maximale Kraftstoffeffizienz und minimalen Lärm zu erzielen.
Turbofan-Triebwerk
Der häufigste Triebwerkstyp in der kommerziellen Luftfahrt, der mit einem großen Fan den Großteil des Schubs erzeugt.