나셀 (Nacelle) (Nacelle)
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Definition
항공기 엔진을 둘러싸고 보호하며, 항력과 소음을 줄이면서 기류를 유도하는 공기역학적 외피.
What Is a Nacelle?
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.
How It Works
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.
Performance Specifications
- 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)
Aircraft Examples
- 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
바이패스비 (BPR)
엔진 코어를 우회하는 공기 질량과 코어를 통과하는 공기의 비율로, 연료 효율의 핵심 지표.
팬 블레이드 (Fan Blade)
터보팬 엔진 전면의 대형 회전 에어포일 블레이드로, 공기를 가속하여 바이패스 추력을 생성하고 엔진 코어에 공기를 공급한다.
기어드 터보팬 (Geared Turbofan)
팬과 저압 터빈 사이에 감속 기어박스를 사용하여 각각 최적 속도로 회전할 수 있도록 한 터보팬 설계.
역추력 장치 (Thrust Reverser)
착륙 후 접지 시 엔진 배기를 일시적으로 전방으로 전환하여 제동력을 제공하는 기계 장치.
터보팬 엔진 (Turbofan Engine)
대형 팬을 사용하여 대부분의 추력을 생성하는, 상용 항공에서 가장 일반적인 제트 엔진 유형.