4 ms·
The main difference between a turboprop and a turbofan is the speed of sound. A propeller needs to avoid breaking the speed of sound, otherwise you get obscene
by mnw21cam 4y ago
The main difference between a turboprop and a turbofan is the speed of sound. A propeller needs to avoid breaking the speed of sound, otherwise you get obscene noise, a reduction in efficiency, and potentially damage to the propeller (although there are some rare propellers that do regularly break the sound barrier). This means that propeller-driven planes must have a speed limit that is quite a lot lower than the speed of sound, to avoid the propeller tips breaking that speed barrier.
A turbofan however is typically installed on planes that want to fly around 80% of the speed of sound. That's really close to the limit, and there isn't enough leeway there for a propeller to get away with it. A turbofan manages by using lots of blades to more gently push the air back, and then the cowling helps by preventing blade-tip vortices, and by constricting the airflow slightly, which increases the air's backwards speed.
So a propeller and a turbofan are suitable for different plane speed regimes. When you're travelling slowly, it is most efficient to push a very large amount of air back just a little bit faster than the plane is moving, and a propeller is great at doing that. As you approach the speed of sound, that becomes infeasible, and a turbofan becomes more efficient. If you're trying to break the speed barrier, then you need a lower bypass ratio, or you may even need to switch to a turbojet.
- deleted 4y ago[deleted]
- kloch 4y agoVirtually all turbofan engine blades exceed the speed of sound at high N1% even when moving slow (like during takeoff). This is part of what generates the distinct "buzzsaw" sound at or near max thrust when seated forward of the engines. The pitch/tone of the buzzsaw sound depends on the number of fan blades and rpm of the main fan (and likely stator design). In this video of an Iran Air 747SP the buzzsaw effect is particularly isolated/exaggerated due to the camera/mic placement, the use of 1970's design (louder) JT9D engines, and the shorter length of the 747SP. https://youtu.be/3lhHwKK-6ms https://youtu.be/3lhHwKK-6ms On a 737 the pitch is higher due to the smaller diameter fan (higher max RPM), while a 777 has the lowest buzzsaw pitch due to having the largest fan diameter. The most recent jet engines (like on the 747-8) have highly suppressed this sound with contoured fan blades.
- bilsbie 4y agoSo if we ever switch to electric we’ll have ducted fans powered by a motor? Assuming we want Mach .8+