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#Electric Variable Pitch Rotor Mk. II
Multi-rotor vehicles are opening up new possibilities everyday. While much of what's promised regarding agriculture, shipping, flying cars, etc. is years, or even decades away, if just some of their capabilities can be achieved, the world will be a different place. Variable pitch rotors can make the promises of multi-rotors come to fruition.
Fixed pitch rotors are typically optimized for a single condition, namely hovering. This means that for other conditions, the design is less than optimal. Variable pitch rotors change the pitch of the blades as required and provide better overall efficiency.
Variable Pitch Examples
Most multi-rotor vehicles use fixed pitch rotors, but there are a few exceptions. The Stingray 500 and the MIT ACL Variable Pitch Quadrotor are two such examples. The maneuvering capabilities of these two vehicles are simply amazing.
EVPR: Electric Variable Pitch Rotor
The main idea behind the EVPR is to put all of the components inside the rotor hub, eliminating the need for swash plates or slip rings, which can cost upwards of a thousand dollars. Servos inside the hub are used to actuate the blade pitch and power for the servos is provided by batteries. Control of the servos is provided via wireless signals. The first application of the EVPR will be on #Goliath - A Gas Powered Quadcopter.
Currently, the nominal battery life is 30 mins. In the the future, an axial flux generator will built into the hub and the batteries will act as a backup. In the future, the design can also be used to create variable pitch propellers for small aircraft that can simply be bolted on and require minimal modifications to the aircraft. Hovercraft could also be fitted with a with a variable pitch fan that not only increases efficiency, but could also provided a braking thrust to slow down. The EVPR design could even be used to create cheaper low frequency subwoofers!
In an effort to make a design that was more easily manufactured, off-the-shelf components are used when available. The design utilizes servo mounts, pillow blocks and servo gears available from Servo City.
Each blade is mounted to a shaft, held in place by two pillow-blocks which carry the radial loads on the shaft. The shaft is actuated using a geared servo. To counteract the centrifugal force pulling the blades outwards, two thrust bearings are utilized and heavy-duty retaining rings hold the shaft in place.
Gear drive in action
The EVPR design uses standard size servos. The specific application will drive the servo and gear ratio selection. For #Goliath - A Gas Powered Quadcopter, the required torque and a variety of servos considered are shown in the figure below.
Almost all of the servos considered have sufficient torque with a gear ratio of 5:3. However, required torque isn't the only consideration. Early testing with the Hitec HS-5685MH found that while the servo had sufficient torque, the gears would strip. The brass gears were unable to handle the the shock and vibration environments and so a steel or titanium gear servo was required. The HSB-9475SH with steel gears was then selected since it's one of the cheapest servos with the required type of gear.
The heart of the EVPR is the ESP32 micro-controller. Currently a Sparkfun ESP32 Dev Board is used. The electronics are placed as close to the center of the hub as possible to lower the centrifugal forces experienced.
For now, a minimum of two ESP32s are required for the EVPR. The first is connected to the flight controller via a UART connection and acts as a master node. It's purpose is to act as the access point and broadcast the servo commands from the flight controller....Read more »