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General Electric · Case study

General Electric GE90

The most powerful jet engine ever flown, and the one that made composite fan blades mainstream. Built exclusively for the Boeing 777, the GE90 set a thrust record that still stands.

Family
High-bypass turbofan
Bypass ratio
≈ 8 – 9
Overall PR
≈ 40 – 42
Max thrust
330 – 510 kN
Fan diameter
≈ 3.1 – 3.4 m
Entered service
1995

Architecture

The GE90 is a two-spool high-bypass turbofan built around an enormous fan — over three metres in diameter on the largest variant. Its defining innovation was the fan blade itself: swept, wide-chord and made of carbon-fibre composite rather than titanium, a first for a commercial engine and the technology that let the fan grow so large without becoming impossibly heavy.

Behind the fan sits a high-pressure-ratio core with an advanced high-pressure compressor and a cooled high-pressure turbine, giving an overall pressure ratio around forty and a bypass ratio approaching nine.

The cycle

A very high bypass ratio gives the GE90 excellent propulsive efficiency, while the high overall pressure ratio lifts thermal efficiency — the combination behind its strong long-haul fuel economy. The largest member, the GE90-115B, is certified above 110,000 pounds of thrust, a level no other turbofan has matched.

Engineering significance

The GE90 proved that composite fan blades could be safe, durable and manufacturable at scale, a lesson that flowed directly into the GEnx and LEAP. As the exclusive engine on the 777-300ER and 777-200LR, it also tied one of the most successful long-haul twins to a single powerplant family.

Applications

Boeing 777

Explore a representative turbofan cycle for this engine class in the interactive console.

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All figures are public-estimated and approximate, given for a representative variant; exact values vary by sub-model and rating. PropulsionLab is an educational project and is not affiliated with any engine manufacturer. Engine names are the trademarks of their respective owners.