A fan engine helps planes fly. 

A fan engine helps big planes fly. 


A turbofan is a type of jet engine. It helps many planes fly. 
This engine has two main parts. One part is a gas turbine engine. This is the core. The core burns fuel to make power. The second part is a ducted fan. This is a fan inside a tube. The core spins the fan. 
When air enters the engine, it splits. Some air goes into the hot core. Other air goes around the core. We call this bypass air. The ratio of these two flows is the bypass ratio.
High-bypass engines move a lot of bypass air. Most big planes use these. They are very good at saving fuel. Low-bypass engines move less bypass air. Most fighter jets use these. They can use an afterburner. An afterburner adds more power for combat.
Turbofans are a middle ground. They sit between turbojets and propellers. Turbojets use only hot exhaust for thrust. Propellers use mostly air from a blade. Turbofans use both the core and the fan to push the plane forward.
A turbofan is a special kind of jet engine used to move aircraft. It is a mix of two different engine ideas. The name comes from the turbojet and the extra fan stage. 
Inside the engine, the air follows two different paths. One part of the air enters the core of the engine. In the core, fuel is burned to create energy. This energy spins a turbine, which is a set of spinning blades. 
Engineers use a number called the bypass ratio to describe these engines. This ratio compares the amount of bypass air to the core air. For example, a ratio of 6 means six times more air goes around the core. 
People have worked on these engines for a long time. In March 1936, Frank Whittle wrote a patent in the UK. He described the ideas that would lead to the turbofan.
You can think of a turbofan as a middle ground in flight technology. It sits between a turbojet and a propeller engine. 
A turbofan is a sophisticated type of airbreathing jet engine used for aircraft propulsion. The name combines the concept of a turbojet with an additional fan stage. This engine design is vital because it improves fuel efficiency for many types of flight. It functions by using a gas turbine engine to add kinetic energy to passing air. 
The mechanism of a turbofan relies on splitting airflow into two distinct paths. First, some air enters the engine core to undergo a thermodynamic cycle. In this core, fuel is burned to create high-energy gas. This gas spins turbines, which extract energy to power the engine's internal components. 
Engineers categorize these engines using the bypass ratio, or BPR. The BPR is the ratio between the mass flow of the bypass stream and the mass flow entering the core. For example, a bypass ratio of 6 means six times more air bypasses the core than enters it. 
The history of this technology traces back to the early ideas of Frank Whittle. In March 1936, Whittle filed a UK patent describing principles that would lead to the turbofan.
Efficiency is a major reason why the turbofan is so successful. In a turbojet, all thrust comes from accelerating a small amount of air to very high speeds. This can lead to wasted kinetic energy in the exhaust wake. A turbofan improves propulsive efficiency by accelerating a larger mass of air at lower speeds. 
Different engine configurations serve different mission requirements. High-bypass engines are optimized for the subsonic speeds used by commercial airliners. Low-bypass engines are better suited for the high speeds required by combat aircraft. Some low-bypass engines even use afterburners to increase thrust. An afterburner is a component where bypass and core air mix before combustion. 
Ultimately, the turbofan represents a critical middle ground in aerospace engineering. It sits between the turbojet, which uses only hot exhaust, and the turboprop, which uses a propeller. 
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