Airbus has lifted the curtain just a tad and given us a glimpse at the future of commercial aviation. At the Airbus Summit 2025 in Toulouse, the company presented a view of the technology that will create the single-aisle airliner of tomorrow.
I’ve seen turboprops in museums and on the internet with around six or eight blades. When I looked on the Wikipedia page for propfan engines, which seems to be another name for an open turbofan, the distinction seemed to be mainly how the blades were shaped (like propellor blades or turbine blades) and how tightly-integrated everything is (you can swap the propeller out on a turboprop).
I don’t think the number of blades is really important. After all if you just keep adding blades eventually you would get to a point of diminishing returns. That’s around four blades which is why most only have four blades, unless they’re made out of incredibly light material.
So if you have a lot of extra blades there probably is some additional engineering going on to make use of those extra blades in some way.
I was meaning that the blade count and detachability was the difference in definition between turboprop and propfan/open turbofan, not that it was necessarily the thing making the engine more efficient.
I’ve seen turboprops in museums and on the internet with around six or eight blades. When I looked on the Wikipedia page for propfan engines, which seems to be another name for an open turbofan, the distinction seemed to be mainly how the blades were shaped (like propellor blades or turbine blades) and how tightly-integrated everything is (you can swap the propeller out on a turboprop).
I don’t think the number of blades is really important. After all if you just keep adding blades eventually you would get to a point of diminishing returns. That’s around four blades which is why most only have four blades, unless they’re made out of incredibly light material.
So if you have a lot of extra blades there probably is some additional engineering going on to make use of those extra blades in some way.
I was meaning that the blade count and detachability was the difference in definition between turboprop and propfan/open turbofan, not that it was necessarily the thing making the engine more efficient.