I was just wondering why some people go for 5 & 6 bladed props?
Does it help in any way

I personally don't like the look but statistics...
A well-designed propeller typically has an efficiency of around 80% when operating in the best regime.[1] Changes to a propeller's efficiency are produced by a number of factors, notably adjustments to the helix angle(θ), the angle between the resultant relative velocity and the blade rotation direction, and to blade pitch (where θ = Φ + α) . Very small pitch and helix angles give a good performance against resistance but provide little thrust, while larger angles have the opposite effect. The best helix angle is when the blade is acting as a wing producing much more lift than drag.
A further consideration is the number and the shape of the blades used. Increasing the aspect ratio of the blades reduces drag but the amount of thrust produced depends on blade area, so using high aspect blades can lead to the need for a propeller diameter which is unusable. A further balance is that using a smaller number of blades reduces interference effects between the blades, but to have sufficient blade area to transmit the available power within a set diameter means a compromise is needed. Increasing the number of blades also decreases the amount of work each blade is required to perform, limiting the local Mach number - a significant performance limit on propellers. Wikipedia
I have just done a few calculations, help if im wrong.Bad Nav wrote:Okay..... so why do WE use 2 / 3 / 4 / 5 / 6 blade props?
To 'put the power down on the road' so to speak.Bad Nav wrote:Okay..... so why do WE use 2 / 3 / 4 / 5 / 6 blade props?
No, but I understand where you are coming from. In order to compare you have to use the same engine, same gearbox ratio. A 912ULS only has one gearbox ratio any wayWargames wrote:I have just done a few calculations, help if im wrong.
Normally with 2 blade - we use a b-box with 2.58 ratio. So at engine revs of 6600 we get prop revs of 2558 if ratio is 2.58. Times 2 we get 5116 blades through the air at top of flange.
Remember that the prop tip speed is not allowed to exceed to sound barrier. This speed is determined by the distance the blade tip moves in one revolution X revs per second. A 72 " (1.829m diameter)blade will travel 5.7460 meters in one revolution. It would require 3445 rpm to break the sound barrier. A shorter prop travels a shorter distance, i.e. 62" (1.574m diameter) will travel 4.947m per revolution. Here 4002 rpm will break the sound barrierWargames wrote:Normally with 2 blade - we use a b-box with 2.58 ratio. So at engine revs of 6600 we get prop revs of 2558 if ratio is 2.58.
Normally with 3 blades we use a c/e -box with 3.47 ratio. So at 6600 revs the prop revs will be 1902.
Users browsing this forum: No registered users and 6 guests