Can someone explain why turboprops are less effective in terms of thrust than turbofans? But at the same time, why turboprops burn less fuel? For example, the Bombardier Q400/De Havilland Dash 8 has a fuel burn of 2.79L/seat/100km, whilst the 737 MAX 8 with the same number of engines burns 2.93L/seat/100km, but the Bombardier has a max. cruising speed of 360 knots and the Boeing plane can go up to 526-527 knots, even though it's heavier.
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1$\begingroup$ Most, if not all, turboprops can put the propellers in beta and generate reverse thrust. $\endgroup$– Ron BeyerApr 21, 2020 at 15:16
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2$\begingroup$ For your second question: How does propellers' pitch change during the use of reverse thrust in turboprop/propfan propelled planes? -- and others -- Note: it's advised to search the site before asking. $\endgroup$– user14897Apr 21, 2020 at 16:44
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$\begingroup$ Because they are attached to faster airplanes? $\endgroup$– quiet flyerApr 21, 2020 at 23:59
3 Answers
To generate a given thrust, a turbofan accelerates less air but faster than a turboprop. This means that turbofans can fly faster. However thermodynamically it is more efficient to accelerate a greater mass of air slower, so turboprops are more efficient and that translates into lower fuel burn.
It’s all dependent upon what operating speeds your aircraft will be in. Propellers can move a great volume of air at slow speeds but accelerate the gas to a lower exit speed than does a turbojet or a turbofan. This is the principal reason that a helicopter is the most efficient means of VTOL flight out there for a heavier than air aircraft. But as speeds increase, the the specific impulse drops and the propeller efficiency drops off with it. At around 400-500 mph, the specific impulse of a high bypass turbofan becomes superior to the turboprop, as, while it moves less air than a turboprop, it can accelerate the smaller air mass to a much higher exit velocity. This trend continues through low bypass turbofan engines, turbojets and then ramjets.
And as pointed out turboprops have a beta and reverse pitch range which can produce reverse thrust.
Turboprops are less fast because of the mechanical constrainsts at the blade tips,efficiency and noise near the speed of sound.
For reverse thrust:yes
related : How does a turboprop engine keep running during thrust reversal?