
The GEnx engine is an advanced dual rotor, axial flow, high-bypass turbofan jet engine in production by GE Aerospace for the Boeing 747-8 and 787. The GEnx-1B engine fan has a diameter of 111 inches and produces about 70,000 pounds of thrust. The engine has been designed to reduce weight, improve performance, and deliver a more fuel-efficient aircraft engine. While I could not find the exact amount of fuel consumed per hour, sources suggest that the GEnx engine delivers up to 15% better specific fuel consumption than its predecessor, a 2% fuel burn advantage over its competition, and a 1% advantage with respect to fuel burn retention.
| Characteristics | Values |
|---|---|
| Fuel consumption | 15% better specific fuel consumption than its predecessor, a 2% fuel burn advantage over its competition and a 1% advantage with respect to fuel burn retention |
| Diameter | 111 inches |
| Thrust | 70,000 pounds |
| Weight | 300 lbs lighter than its predecessor |
| Fan blade count | 18 fan blades, down from 22 |
| Fan case | Carbon-fibre composite |
| Combustor | Twin-annular pre-swirl (TAPS) |
| NOx gases | 15% reduction |
| EGT retention | 35% improvement |
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What You'll Learn
- The GEnx-1B engine delivers up to 15% better specific fuel consumption than its predecessor
- The engine has a twin annular, pre-swirl (TAPS) combustor which enables the fuel-air mixture to burn at a significantly lower temperature
- The GEnx-1B engine fan is 111 inches in diameter and produces about 70,000 pounds of thrust
- The GEnx engine is the world's first commercial jet engine with both a front fan case and fan blades made of carbon-fiber composites
- The GEnx engine is designed to replace previously hydraulic and pneumatic systems with electrical ones to reduce weight and increase efficiency

The GEnx-1B engine delivers up to 15% better specific fuel consumption than its predecessor
The GEnx-1B engine is a jet engine designed specifically for the Boeing 787 Dreamliner family. It is the fastest-selling, high-thrust jet engine in GE Aviation history, with over 2,700 engines in service and on order. The engine is designed to power the four-engine Boeing 747-8 and is based on proven GE90 architecture.
The GEnx-1B engine offers up to 15% better specific fuel consumption than its predecessor, the GE CF6 engine. This improvement in fuel efficiency is achieved through various innovative features and technological advancements. One key feature is the twin-annular pre-swirl (TAPS) combustor, which dramatically reduces NOx gases. The TAPS combustor premixes air and fuel to create a leaner mixture that burns at lower temperatures, resulting in lower NOx emissions.
The GEnx-1B engine also features larger, more efficient fan blades. These fan blades are made of carbon-fiber composites, making the GEnx engine the world's first commercial jet engine with both a front fan case and fan blades constructed from these materials. This contributes to the engine's improved fuel efficiency and also makes it the quietest commercial aircraft engine GE has ever produced.
In addition to the advancements in the engine's design, the GEnx-1B also benefits from improvements in the manufacturing process. The engine utilizes lightweight, durable composite materials, reducing its weight and further enhancing its performance. The GEnx-1B engine's high-pressure compressor, lean-burning combustor, and composite fan case and blades work together to deliver a more fuel-efficient and environmentally friendly commercial aircraft engine.
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The engine has a twin annular, pre-swirl (TAPS) combustor which enables the fuel-air mixture to burn at a significantly lower temperature
The General Electric GEnx is an advanced dual rotor, axial flow, high-bypass turbofan jet engine. The GEnx engine represents a significant advancement in propulsion technology, utilising cutting-edge materials and design processes to enhance performance, reduce weight, and improve fuel efficiency.
One of the key innovations of the GEnx engine is its twin-annular pre-swirl (TAPS) combustor, also known as the Lean TAPS combustor. This combustor enables the fuel-air mixture to burn at a significantly lower temperature. The TAPS combustor is a single annular combustor with one ring of full nozzles. The "twin" in its name refers to the two distinct fuel streams within each fuel nozzle: the main stream and the pilot stream.
By utilising this twin annular design, the TAPS combustor offers several advantages. Firstly, it dramatically reduces the emission of NOx gases and other regulated gases, ensuring compliance with regulatory limits. This reduction in NOx emissions is achieved through the required pressure loss and backflow margin in the combustion process.
Additionally, the TAPS combustor enhances the durability of the engine. The GEnx engine's low-pressure turbine (LPT) benefits from this design, as it is not only lighter but also more efficient than its predecessor. The incorporation of titanium aluminide blades in stages 6 and 7 further contributes to a weight reduction of approximately 300 lbs.
The GEnx engine also incorporates larger, more efficient fan blades. These blades, made from composite materials, contribute to a quieter engine, making the GEnx the quietest commercial aircraft engine GE has ever produced. The composite fan blades also help to reduce thermal expansion, further enhancing the engine's performance and durability.
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The GEnx-1B engine fan is 111 inches in diameter and produces about 70,000 pounds of thrust
The GEnx engine is an advanced dual rotor, axial flow, high-bypass turbofan jet engine produced by GE Aerospace for the Boeing 747-8 and 787. The GEnx-1B engine fan is specifically designed for the Boeing 787 Dreamliner family.
The GEnx-1B engine fan has a diameter of 111 inches and produces about 70,000 pounds of thrust. The fan blades are made of composite material, which makes them lighter in weight than those of its predecessor. They also have steel alloy leading edges, and the composite fan case reduces thermal expansion. The fan blades are also protected by a titanium shield on the leading edge to protect them from impact damage. The fan case is manufactured from a fiber-braided composite-matrix material, which provides better containment and is highly resistant to damage, fatigue, temperature extremes, and corrosion.
The GEnx engine represents a significant advancement in propulsion technology, utilising the latest materials and design processes to enhance performance and fuel efficiency. It is designed to be quieter than current turbofans and features a twin-annular pre-swirl (TAPS) combustor that reduces NOx gas emissions. The engine also incorporates a high-pressure compressor based on the GE90-94B to reduce fuel burn, as well as shrouded guide vanes and counter-rotating spools for the reaction turbines, which reduce load and improve engine life.
The modular design of the GEnx engine allows for efficient maintenance. The fan assembly can be separated from the propulsor, enabling repairs to be conducted while keeping the fan in service and installing it on another propulsor if needed. GE has developed a comprehensive set of repair procedures and continues to develop additional ones, demonstrating their commitment to proactive engine maintenance throughout its life cycle.
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The GEnx engine is the world's first commercial jet engine with both a front fan case and fan blades made of carbon-fiber composites
The GEnx engine is a widebody jet engine that powers the Boeing 787 Dreamliner and Boeing 747-8. The GEnx engine is also used in the initial Airbus A350 aircraft. The engine is an advanced dual rotor, axial flow, high-bypass turbofan jet engine.
The use of carbon-fiber composites in the GEnx engine is the result of more than 20 years of research and development by GE. The company has been advancing the use of composites in jet engines in unprecedented ways. The GEnx engine also incorporates composite technology in other areas, such as the fan stator case, fan platforms, and acoustic panels. The engine's airflow path surfaces could also potentially be made of composite materials, according to Kray, who believes that hybrid materials are not limited to the fan section.
The GEnx engine offers superior efficiency and has been selected for its fuel efficiency by both Boeing and Airbus. The engine delivers up to 15% better specific fuel consumption than its predecessor and provides a 2% fuel burn advantage over its competition. The weight reduction achieved through the use of composites directly contributes to fuel burn savings, increased payload, and greater aircraft range.
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The GEnx engine is designed to replace previously hydraulic and pneumatic systems with electrical ones to reduce weight and increase efficiency
The GEnx engine is a significant advancement in propulsion technology, employing cutting-edge materials and innovative design processes to enhance performance and fuel efficiency. One of its key features is the replacement of traditional hydraulic and pneumatic systems with electrical systems, marking a shift towards the More Electric Aircraft concept. This transformation brings about several advantages, including weight reduction, improved efficiency, and lower maintenance requirements.
The GEnx engine's electrical systems contribute to weight reduction by eliminating the need for hydraulic fluids and the associated plumbing and hardware. This weight reduction has a positive cascade effect on the aircraft's overall efficiency and performance. The electrical systems also enhance efficiency by providing more precise control over various aircraft functions, resulting in optimized operations and reduced fuel consumption.
The GEnx engine's move towards electrical systems is particularly evident in the GEnx-1B engine variant. This version utilizes electrical power from starter-generators to perform functions previously accomplished by bleed air. By contrast, the GEnx-2B engine retains a traditional bleed air system to power internal pneumatic and ventilation systems.
The GEnx engine's fan blades also contribute significantly to weight reduction. They are crafted from composite materials, making them lighter and less dense than traditional fan blades. This design choice not only reduces the overall engine weight but also improves blade durability and maintenance requirements. The GEnx engine's fan case is also constructed from composite materials, further enhancing weight reduction and providing superior containment capabilities.
The GEnx engine's innovative design has resulted in notable improvements in fuel efficiency. Boeing predicts that the GEnx engine will deliver up to a 20% reduction in fuel consumption compared to current turbofan engines. Additionally, the GEnx engine is expected to produce thrust ranging from 53,000 to 75,000 lbf, with the GEnx-1B engine specifically generating approximately 70,000 pounds of thrust.
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