jet engine, any of a class of internal-combustion engines that propel aircraft by means of the rearward discharge of a jet of fluid, usually hot exhaust gases generated by burning fuel with air drawn in from the atmosphere.
The prime mover of virtually all jet engines is a gas turbine. Variously called the core, gas producer, gasified, or gas generator, the gas turbine converts the energy derived from the combustion of a liquid hydrocarbon fuel to mechanical in the form of a high-pressure, high-temperature airstream. This energy is then harnessed by what is termed the propulsion (e.g., airplane propeller and helicopter rotor) to generate a thrust with which to propel the aircraft.
Basic engine types
Achieving a high propulsive efficiency for a jet engine is dependent on designing it so that the exiting jet velocity is not greatly in excess of the flight speed. At the same time, the amount of thrust generated is proportional to that very same velocity excess that must be minimized. This set of restrictive requirements has led to the evolution of a large number of specialized variations of the basic turbojet engine, each tailored to achieve a balance of good fuel efficiency, low weight, and compact size for duty in some band of the flight speed–altitude–mission spectrum. There are two features characteristic of all the different engine types, however. First, in order to achieve a high propulsive efficiency, the jet velocity, or the velocity of the gas stream exiting the propulsor, is matched to the flight speed of the aircraft—slow aircraft have engines with low jet velocities and fast aircraft have engines with high jet velocities. Second, as a result of designing the jet velocity to match the flight speed, the size of the propulsor varies inversely with the flight speed of the aircraft—slow aircraft have very large propulsors, as, for example, the helicopter rotor—and the relative size of the propulsor decreases with increasing design flight speed—turboprop propellers are relatively small and turbofan fans even smaller.
The helicopter is designed to operate for substantial periods of time hovering at zero flight speed. Even in forward flight, helicopters rarely exceed 240 kilometers per hour or a Mach number of 0.22. (The Mach number is the ratio of the velocity of the aircraft to the speed of sound.) The principal propulsor is the helicopter rotor, which is driven by one or more turboshaft engines
in all modern helicopters of large size. As was previously noted, the propulsor is designed to give a very low discharge or jet velocity and is by the same token very large for a given size aircraft when compared to the propulsors of higher-speed aircraft. The prime mover of a helicopter is a core engine whose gas horsepower is extracted by a power turbine, which then drives the helicopter rotor via a speed-reducing (and combining) gearbox. The power turbine is usually located on a spool separate from the gas generator; thus its rotative speed and that of the helicopter rotor which it drives are independent of the rotative speed of the gas generator. This allows the rotor speed to be varied or kept constant independently of the gas-generator speed, which must be varied to modulate the amount of power generated.
The turboprop is the power plant that occupies the next band of flight speeds in the flight spectrum, from a Mach number of 0.2 to 0.7. The propulsor is propeller with a somewhat higher discharge, or jet velocity, than that of the helicopter rotor to match the flight speed, and it has a proportionately smaller area than the latter for a similarly sized aircraft. The prime mover is a turbo shaft engine. It’s very similar to the one that drives a helicopter rotor except for a different gearbox
designed to provide a somewhat higher rotative speed for the propeller, which turns faster than the helicopter rotor having a much larger diameter. The control mode of the turboprop also is somewhat different from that of a helicopter’s turboshaft engine. In a helicopter the pilot calls for power by manipulating the pitch of the rotor blades (a greater pitch taking a bigger “bite” of air and so demanding more power to maintain rotative speed). The engine’s control responds by increasing fuel to the engine to maintain output shaft speed. In a turboprop the pilot calls for power by selecting fuel flow to the prime mover. The propeller control responds by varying propeller pitch to attain a greater “pull” while maintaining a preselected propeller rotative speed.
Moving up in the spectrum of flight speeds to the transonic regime—Mach numbers from 0.75 to 0.9—the most common engine configurations are turbofan engines, such as those shown in
In a turbofan, only a part of the gas horsepower generated by the core is extracted to drive a propulsor, which usually consists of a single low-pressure-ratio, shrouded turbocompression stage. The fan is generally placed in front of the core inlet so that the air entering the core first passes through the fan and is partially compressed by it. Most of the air, however, bypasses the core (hence the designation bypass stream) and goes directly to an exhaust nozzle. The core stream, with some modest fraction of the gas horsepower remaining (not extracted to drive the fan) proceeds directly to its own exhaust nozzle.
![Description: Figure 2: Turboshaft engine driving a helicopter rotor as propulsor.
[Credit: Encyclopædia Britannica, Inc.]](file:///C:/Users/DOANHA~1/AppData/Local/Temp/msohtmlclip1/01/clip_image002.jpg)
![Description: Figure 3: Turboprop engine driving a single rotation propeller as propulsor; tractor arrangement.
[Credit: Encyclopædia Britannica, Inc.]](file:///C:/Users/DOANHA~1/AppData/Local/Temp/msohtmlclip1/01/clip_image004.jpg)
![Description: Figure 4: Ultrahigh-bypass engine (UBE) with geared fan and variable-pitch blading for thrust …
[Credit: Encyclopædia Britannica, Inc.]](file:///C:/Users/DOANHA~1/AppData/Local/Temp/msohtmlclip1/01/clip_image006.jpg)
![Description: Figure 5: High-bypass turbofan with two-spool core and mixed-flow jet.
[Credit: Encyclopædia Britannica, Inc.]](file:///C:/Users/DOANHA~1/AppData/Local/Temp/msohtmlclip1/01/clip_image008.jpg)





