Nasel (Nacelle)
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Definition
Bir uçak motorunu çevreleyen ve koruyan, sürtünmeyi ve gürültüyü azaltırken hava akışını yönlendiren aerodinamik muhafaza.
Nedir 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.
Nasıl Çalışır
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.
Performans Özellikleri
- 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)
Uçak Örnekleri
- 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
Baypas Oranı
Motor çekirdeğinin etrafından geçen hava kütlesinin çekirdekten geçen havaya oranı; yakıt verimliliğinin temel göstergesi.
Dişlili Turbofan
Fan ile alçak basınçlı türbin arasında bir redüksiyon dişli kutusu kullanan; her birinin optimum hızda dönmesine izin veren turbofan tasarımı.
Fan Kanadı
Baypas itmesi üretmek için havayı hızlandıran ve motor çekirdeğini besleyen türbofan motorunun ön tarafındaki büyük dönen kanat profilleri.
Ters İtme
İniş sonrası fren kuvveti sağlamak için motor egzozunu geçici olarak ileriye yönlendiren mekanik cihaz.
Türbofan Motor
Ticari havacılıkta kullanılan en yaygın jet motor tipi; itmesinin çoğunu üretmek için büyük bir fan kullanır.