Comment by dombar1 on 19/10/2021 at 14:10 UTC

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)

Replies

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]