Fan Blade
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/fan-blade/" 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/fan-blade/
Add a dynamic SVG badge to your README or docs.
[](https://planefyi.com/glossary/fan-blade/)
Use the native HTML custom element.
Definition
The large rotating aerofoil blades at the front of a turbofan engine that accelerate air to generate bypass thrust and feed the engine core.
What Is a Fan Blade?
Fan blades are the large, swept aerofoil structures at the front of a Turbofan Engine that rotate at high speed to accelerate incoming air. They are simultaneously the first compressor stage for the engine core and the primary thrust-generating component via the bypass stream. Modern fan blades represent some of the most advanced manufacturing achievements in aerospace, combining extreme performance demands — high aerodynamic loading, bird-strike resistance, fatigue tolerance — with minimal weight.
How It Works
Fan blades rotate at typically 2,500–4,000 RPM in large commercial turbofans, with blade tip speeds approaching Mach 1.0–1.4. Each blade acts as an aerofoil, generating lift in the rotational plane to accelerate airflow rearward. Key engineering features:
- Sweep and twist: Blades are swept back and twisted along their span to manage shockwave formation at transonic tip speeds and optimize pressure rise across the whole blade.
- Wide-chord design: Wider chord blades (first introduced on the Rolls-Royce RB211) eliminate the need for inter-blade snubbers (tie wires), reducing drag and weight.
- Hollow titanium or carbon fiber composite: LEAP-1B uses 3D-woven carbon fiber composite fan blades; GE90 and GE9X use carbon fiber composites with titanium leading-edge armor.
- Bird-strike certification: Must withstand ingestion of a 4 lb (1.8 kg) bird at takeoff speed without causing uncontained engine failure — tested to FAA FAR 33.76 standards.
Performance Specifications
- Diameter: 61 inches (CFM56-7B) → 69 inches (LEAP-1B) → 134 inches (GE9X)
- Blade count: 18 blades (LEAP-1B, vs 24 on CFM56) — fewer, wider blades reduce weight and improve efficiency
- Tip speed: 450–550 m/s (Mach 1.2–1.5 at tip)
- Material weight saving: Carbon fiber composite blades are 30–40% lighter than equivalent titanium blades
- Centrifugal force at tip: Each blade experiences tens of tonnes of centrifugal force during operation
Aircraft Examples
- Boeing 737 MAX / LEAP-1B: 18 carbon fiber 3D-woven composite fan blades, 69-inch diameter — 15% lighter than titanium equivalent
- Boeing 777X / GE9X: 16 composite fan blades in a 134-inch diameter fan — largest commercial engine fan ever produced
- Airbus A380 / Trent 970: 24 titanium wide-chord fan blades in 116-inch diameter fan
- Pratt & Whitney PW1000G series: 20 composite fan blades with geared architecture spinning at lower RPM for efficiency
Fan blades are enclosed within the Nacelle, which shapes the incoming airflow and provides containment in the event of a blade failure event. The Bypass Ratio determines fan diameter and, therefore, blade size.
Related Terms
Bypass Ratio
The ratio of air mass flowing around the engine core to air flowing through the core, a key indicator of fuel efficiency.
High-Bypass Turbofan
A turbofan engine with a bypass ratio above 5:1, routing most intake air around the engine core for maximum fuel efficiency and minimum noise.
Nacelle
The aerodynamic housing that surrounds and protects an aircraft engine, reducing drag and noise while directing airflow.
Turbofan Engine
The most common jet engine type used in commercial aviation, using a large fan to generate most of its thrust.
Mentioned In
Aircraft Noise Reduction Technology
…source on high-bypass ratio turbofans; generated by fan blade interaction with inlet and outlet guide vanes. Higher…
Bird Strikes: How Aircraft Survive
…impact energy through controlled deformation. The CFM56 fan blade, for example, has a hollow titanium core with a swept…