고바이패스 터보팬 (High-Bypass Turbofan) (HBT: High-Bypass Turbofan)
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Definition
바이패스비가 5:1 이상인 터보팬 엔진으로, 흡입 공기의 대부분을 엔진 코어 주변으로 우회시켜 연료 효율을 극대화하고 소음을 최소화한다.
What Is a High-Bypass Turbofan?
A high-bypass turbofan is a jet engine where the large front fan moves far more air around the engine core than through it. The bypass ratio — the ratio of bypassed air to core air — exceeds 5:1, with modern commercial engines reaching 12:1 or higher. This configuration makes high-bypass turbofans the dominant propulsion system for commercial airliners and widebody freighters worldwide.
How It Works
Incoming air enters through the large-diameter fan, typically 2.8–3.5 m (110–140 in) across on widebody engines. A small fraction — perhaps 10–20% — passes through the engine core, where it is compressed by the compressor stages, mixed with fuel in the combustion chamber, and expelled through the turbine and exhaust nozzle. The remaining 80–90% bypasses the core entirely, accelerated only modestly by the fan and discharged as a large, slow-moving jet.
This bypass stream generates the majority of thrust while consuming far less fuel than accelerating a small mass of air to high velocity. The principle follows Newton's second law: a large mass flow at low velocity is thermodynamically more efficient than a small mass flow at high velocity, particularly below Mach 0.9.
Performance Specifications
- Bypass ratio: 5:1 to 13:1 (GE9X reaches 10:1; CFM LEAP-1B approximately 9:1)
- Thrust range: 100 kN to 500 kN (22,500 lbf to 112,000 lbf) for commercial variants
- Specific fuel consumption (SFC): approximately 0.50–0.55 lb/lbf/hr at cruise, 15–20% better than low-bypass predecessors
- Noise reduction: 20–30 EPNdB quieter than 1960s-era turbojets
- Cruise speed compatibility: Mach 0.78–0.90
Aircraft Examples
- GE90-115B on the Boeing 777-300ER — rated at 513 kN (115,300 lbf), the most powerful certified commercial turbofan
- GEnx-1B on the Boeing 787-9 — bypass ratio approximately 9.3:1
- Trent XWB-97 on the Airbus A350-1000 — rated at 430 kN (97,000 lbf)
- CFM56-7B on the Boeing 737-800 — bypass ratio 5.1:1, older but widely deployed
The high-bypass architecture's efficiency gains have enabled non-stop ultra-long-haul routes exceeding 17,000 km (10,500 mi), such as Singapore–New York operated by Airbus A350-900ULR.
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.
비연료소비율 (SFC)
엔진 연료 효율의 척도: 시간당 생산된 추력 단위당 소비되는 연료 질량으로, lb/(lbf·h) 또는 kg/(kN·h)로 표시된다.
터보팬 엔진 (Turbofan Engine)
대형 팬을 사용하여 대부분의 추력을 생성하는, 상용 항공에서 가장 일반적인 제트 엔진 유형.