103 upvotes, 4 direct replies (showing 4)
View submission: Is there an upper limit to the highest possible bypass ratio of a turbofan engine?
Theoretically, no. Practically, there are many limits.
One quick example, as a fan becomes larger it would become a propeller.
There are several limits to the overall diameter of both propellers and fans, in no particular order (it will be different for every airplane)
Comment by Barfmeister at 19/10/2021 at 14:56 UTC
68 upvotes, 1 direct replies
Just latching on to this explanation to add: Another factor limiting the possible bypass ratio is the fan tip speed. The larger the outer diameter, the lower the possible RPM of the fan is before reaching Mach 1 at the tips and encountering problematic compressibility effects. This is currently addressed in (Ultra) High Bypass Ratio engines by implementing a gearbox between fan and the inner shaft, but that is also added complexity and weight, and has its limitations.
Comment by gargravarr2112 at 19/10/2021 at 21:01 UTC
20 upvotes, 0 direct replies
There is actually an example of this, the propfan[1]. Also known as an ultra-high-bypass turbofan engine.
1: https://en.wikipedia.org/wiki/Propfan
Comment by williamwchuang at 19/10/2021 at 21:05 UTC
7 upvotes, 0 direct replies
To expand on the second point, the FAA requires blades to survive a bird strike without having an uncontained failure. If a bird hits the spinning blades, the engine must survive without spewing its contents out of the cowling around the engine. Currently, carbon fiber blades have a titanium edge to help resist bird strikes.
Comment by [deleted] at 19/10/2021 at 17:31 UTC
2 upvotes, 2 direct replies
[deleted]