Nacele (Nacelle)
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Definition
A carenagem aerodinâmica que envolve e protege um motor de aeronave, reduzindo arrasto e ruído.
O que é uma nacele?
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.
Como funciona
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.
Especificações de desempenho
- 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)
Exemplos de aeronaves
- 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
Motor turbofan
O tipo de motor a jato mais comum na aviação comercial, utilizando um grande fan para gerar a maior parte do empuxo.
Pá do fan
As grandes pás aerodinâmicas rotativas na frente de um motor turbofan que aceleram o ar para gerar empuxo.
Razão de bypass
A razão entre a massa de ar que flui ao redor do núcleo do motor e a que flui através dele, indicador-chave de eficiência.
Reversor de empuxo
Um dispositivo mecânico que redireciona temporariamente o escapamento do motor para frente, fornecendo força de frenagem após o pouso.
Turbofan com Redutor
Um projeto de turbofan que usa uma caixa de redução entre o fan e a turbina de baixa pressão, permitindo que cada um gire na velocidade ideal.