Pax hate turboprops because of the noise and a misconception that they're not jet engines.
There's no inherent safety difference, except that there used to be regional airlines flying with inexperienced pilots like cough Colgan.
They can provide fine-controlled reverse thrust, so they have that going for them. And they’re less complicated (and lighter) than a traditional piston engine, making them a win over normal engines in mid-sized aircraft.
EDIT: "Jets" in the above is a poor reference to turbofans, as pointed out by replies. Thanks for the clarification.
A Turbofan still has a turbine being powered by a jet engine, similar to a turboprop, but it does not have the complexity associated with being able to change the pitch of the props.
Combat jets often have very low-bypass ratio turbofan engines though. A true turbojet has a 0 bypass-ratio; a lot of turbofan fighter jets have bypass-ratios under 1, while the engines on a 787 have a bypass-ratio of 10.
https://en.wikipedia.org/wiki/Bypass_ratio#Engine_bypass_rat...
Related to turboprops are turboshaft engines, which turn a power transmission shaft instead of a propeller directly. In some cases, like the V-22 Osprey, the line between a turboprop and a turboshaft is blurred. But some clear examples of turboshaft engines are in modern helicopters and Abrams tanks.
There are some kinds of jet engines that don't use turbines. Ramjets and scramjets don't use turbines, but have 'jet' in the name because they produce their thrust using a jet of hot exhaust gas. Rocket engines produce jets of hot exhaust gas, but aren't called jet engines because.. reasons.
> jet: A collimated stream, spurt or flow of liquid or gas from a pressurized container, an engine, etc.
(Note that this makes turboprop engines not jet engines, but turbojet and turboprop engines are both gas turbine engines.)
If they are so simple can you explain to me how interlaced rows of stator and rotor blades turn pressure into gas speed? That one always stumped me. Or how do I make monocrystalline blades, and how can I QA them? Or what exactly a FADEC do during startup, and how do the controlled parameters change depending on atmospheric conditions? Also I heard that the injectors and the air flow in the combustion chambers is designed such that there is an outside layer of incomplete combustion creating a colder laminar gasflow to protect the chamber wall itself. How do I go about designing that? How do I cool the bearings? How does one get the rotational energy out from the centre shaft to drive an oil pump on the side of the engine?
I mean these are just the first questions which pop up in my mind when I think about jet engines. And I'm not even a jet mechanic. If you truly think that jet engines are simple, then I envy your intellect.
Jet engines are used on some older oil pumps because they can run for decades with minimal maintenance.
This Genius Invention Could Transform Jet Engines, 2015, 3m51s, Bloomberg QuickTake Originals
[2] https://www.youtube.com./watch?v=8aPIEsnKb6o
Rolls-Royce UltraFan technology, 3 shaft geared turbofan jet engine, 2018, 2m29s, MDx media
The 'jet' engines used on oil pumps etc. are actually not jet engines: they are gas turbines in which an additional turbine or turbine stage is used to extract rotational power - in other words, they are more like turboprop engines than jet engines.
Nevertheless, I do disagree with the suggestion that turboprops are much less safe than turbojets, and I suspect that the author of that comment was confusing them with piston engines, which also (almost always) use propellers (increasingly, we are seeing turboprop singles replacing piston twins.) Finally, piston engines themselves have become much more reliable since the days when they were the only option.
Pedant.
There is every reason to anticipate China taking a big share of that industry away from Boeing and Airbus. They only need to buy their own supply (which they will) to do that.
Further, Japan is also very obviously about to successfully unleash the Mitsubishi SpaceJet.
It's like people that were still pointing out up to the last moments in May that the US had no human space launch capability, trying to wring that last bit of satisfaction from the context.
They then built the factory for the C919 in Shanghai, and there went most of the people who previously worked at the Airbus factory. :)
not certified, a decade late
> about to successfully unleash the Mitsubishi SpaceJet.
wasn't that cancelled last week?
https://www.avweb.com/aviation-news/mitsubishi-pulls-back-sp...