Turbofan à Fort Taux de Dilution (HBT: High-Bypass Turbofan)
Embed This Widget
Add the script tag and a data attribute to embed this widget.
Embed via iframe for maximum compatibility.
<iframe src="https://planefyi.com/iframe/glossary/high-bypass-turbofan/" width="420" height="400" frameborder="0" style="border:0;border-radius:10px;max-width:100%" loading="lazy"></iframe>
Paste this URL in WordPress, Medium, or any oEmbed-compatible platform.
https://planefyi.com/glossary/high-bypass-turbofan/
Add a dynamic SVG badge to your README or docs.
[](https://planefyi.com/glossary/high-bypass-turbofan/)
Use the native HTML custom element.
Definition
Un moteur turbofan avec un taux de dilution supérieur à 5:1, acheminant la majeure partie de l'air entrant autour du cœur du moteur pour une efficacité maximale en carburant et un bruit minimal.
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
Aube de soufflante
Les grandes aubes aérodynamiques rotatives à l'avant d'un moteur turboréacteur à double flux accélérant l'air pour générer la poussée.
Consommation spécifique de carburant
Une mesure de l'efficacité en carburant du moteur : la masse de carburant consommée par unité de poussée par heure.
Moteur turboréacteur à double flux
Le type de moteur à réaction le plus courant en aviation commerciale, utilisant une grande soufflante pour générer l'essentiel de sa poussée.
Taux de dilution
Le rapport entre le débit d'air contournant le cœur du moteur et celui traversant le cœur, indicateur clé d'efficacité en carburant.