• Welcome aboard HomebuiltAirplanes.com, your destination for connecting with a thriving community of more than 10,000 active members, all passionate about home-built aviation. Dive into our comprehensive repository of knowledge, exchange technical insights, arrange get-togethers, and trade aircrafts/parts with like-minded enthusiasts. Unearth a wide-ranging collection of general and kit plane aviation subjects, enriched with engaging imagery, in-depth technical manuals, and rare archives.

    For a nominal fee of $99.99/year or $12.99/month, you can immerse yourself in this dynamic community and unparalleled treasure-trove of aviation knowledge.

    Embark on your journey now!

    Click Here to Become a Premium Member and Experience Homebuilt Airplanes to the Fullest!

Gear reductions - how to calculate ratio required

This site may earn a commission from merchant affiliate links, including eBay, Amazon, and others.

rtfm

Well-Known Member
Joined
Jan 3, 2008
Messages
3,900
Location
Brisbane, Australia
Hi,
I'm a bit confused about gear reduction units...

Let's take engine "A", for example. Max RPM = 7250, producing 100hp. At 75% power (we assume a linear power curve) it will be doing about 5500 RPM. If we assume that we are aiming for about 2800 prop RPM, we would need a reduction unit of about 1:1.95

It this right?

What if we wanted to cruise at 85% power on a fixed pitch prop? Would we need to fly at almost 3200 prop RPM?

How do in-flight adjustable (or constant-speed) props handle this?

Duncan
 
Back
Top