팬 블레이드 (Fan Blade) (Fan Blade)
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Definition
터보팬 엔진 전면의 대형 회전 에어포일 블레이드로, 공기를 가속하여 바이패스 추력을 생성하고 엔진 코어에 공기를 공급한다.
What Is a Fan Blade?
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.
How It Works
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.
Performance Specifications
- 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
Aircraft Examples
- 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
바이패스비 (BPR)
엔진 코어를 우회하는 공기 질량과 코어를 통과하는 공기의 비율로, 연료 효율의 핵심 지표.
고바이패스 터보팬 (High-Bypass Turbofan)
바이패스비가 5:1 이상인 터보팬 엔진으로, 흡입 공기의 대부분을 엔진 코어 주변으로 우회시켜 연료 효율을 극대화하고 소음을 최소화한다.
나셀 (Nacelle)
항공기 엔진을 둘러싸고 보호하며, 항력과 소음을 줄이면서 기류를 유도하는 공기역학적 외피.
터보팬 엔진 (Turbofan Engine)
대형 팬을 사용하여 대부분의 추력을 생성하는, 상용 항공에서 가장 일반적인 제트 엔진 유형.