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# Brushless Motor Power and Efficiency Analysis

Published: 13-06-2021, Last updated:19-10-2021

## Introduction:

Understanding efficiency is the first step to improving the performance of devices and vehicles containing brushless DC (BLDC) motors. This article explains the key formulas for calculating brushless motor efficiency and demonstrates how they can be used in experimental situations.

This article will help you gain an understanding of how a brushless DC motor operates by providing examples with real data. If you are a drone designer, this knowledge will also help you develop strategies to maximize the flight time and payload of your vehicle.

1. Assumptions
2. Brushless motor power and efficiency formulas
3. The relationship between torque, speed and mechanical power
4. The relationship between torque, speed and electrical power
5. Overall motor efficiency
6. Heat losses and the best operating point

In the experiments described, we used a Series 1580 test stand for data acquisition and powertrain control. The theoretical analysis is done in Octave. ## Assumptions:

There are two main efficiencies to consider in a brushless system: motor efficiency and propeller efficiency. In order to focus on motor efficiency, we will simplify propeller efficiency and say that the bigger the propeller, the higher its efficiency. Motors, on the other hand, have a high efficiency when spinning at high speed with relatively low torque. Operating at high torque results in the motor heating up and losing efficiency. That said, the reduced efficiency might be a worthy compromise in order to use a larger, more efficient propeller and to avoid using a gear box, which adds complexity and leads to heat losses.

The theoretical model we use assumes that motor Kv does not change, though this is not exactly true due to the electronic speed controller (ESC). We also simplify heat losses as a simple resistance for use in the calculations, while in a real circuit there is a more complex impedance.

These assumptions and simplifications lead to differences between the theoretical and experimental results, which are interesting to observe through testing.

Further reading: How to Measure Motor Torque and Why You Should

## Formula Explanation:

There are several key formulas for understanding brushless motor performance. You can see how motor power and efficiency are closely related and dependent on factors such as torque, RPM, current and voltage. ### The Torque-Speed Plot and Mechanical Power:

The torque-speed plot helps us to understand how these two factors are related, as well as what happens when one of them is intentionally set to '0'. Let’s first look at formula 2, which relates the two parameters and describes how to calculate mechanical power: Mechanical power is the product of torque and RPM, so when there is either no torque or no rotation, no power is produced. Figure 1 provides a visual reference for what this looks like in practice, where we present data from several motor tests. Figure 1: Mechanical power for a 1500 Kv brushless DC motor

Along the horizontal axis you’ll see several blue circles, these data points were recorded during a no-load motor test. As you can see, when the motor is spinning freely with no load (i.e. no propeller), no torque is generated. An increase in voltage increases the motor’s speed along the horizontal axis, but the mechanical wattage remains at zero. The dynamometer used for the test confirmed the results, also indicating zero torque and zero mechanical power.

The other extreme is to have no rotation speed while slowly increasing the torque, achieved by sending power to the motor but not letting it spin. In theory, this mode of operation would produce a vertical line of data points along the vertical axis with increasing torque but no speed. In practice, motors used by UAVs and drones are not designed to work at very low speeds and would overheat with high torque. We did not want to subject our motors to this much stress, so we only performed this test at low torque, which is why there is only one data point above zero on the vertical axis.

In reality, your motor will operate between these two extremes. The six other power curves in figure 1 demonstrate the results of tests performed with unobstructed motors with propellers. Each dataset represents a different propeller, with the corresponding sizes listed in the legend on the right-hand side (diameter, pitch). As you can see, these propulsion systems occupy the middle of the graph between the two extremes, where regular operation occurs.

### The Torque-Speed Plot and Electrical Power:

Electrical power can be determined experimentally or theoretically, and it can be a fun exercise to compare your test results to your theoretical calculations.

#### Experimental Approach:

When calculating electrical power we can use formula 3, where electrical power is the product of current and voltage. We can also calculate electrical power using formula 4, where it is the sum of mechanical power (RPM*torque) and heat losses.

Figure 3 shows how electrical power relates to torque and RPM. The data points represent the test result from motors equipped with propellers of different sizes and pitch. Similarly to the 3D display of mechanical power in figure 1, the electrical power is proportional to the motor’s torque. However, even when there is no rotation (RPM = 0) and torque is applied, there is still production of electrical power. This is unlike mechanical power, where for all torque values at 0 RPM no power is produced.

Further reading: Drone Design Calculations and Assumptions

Each curve represents a different load (propeller) with speed and torque values plotted. The theoretical values are displayed as a 3D plot represented as a coloured surface, the brighter the shade, the higher the electrical power at that point. Figure 3: Electrical power for a 1500Kv brushless DC motor

#### Theoretical Approach:

To calculate a motor’s electrical power theoretically we use formula 4. To allow us to input values into the formula, we replace ‘mechanical power’ with the right side of formula 2, and ‘heat losses’ with the right side of formula 5, to give formula 6. Here, R represents the resistance in the circuit generated by the motor (inversely proportional to the torque). The theoretical model assumes that the Kv does not change, which is not exactly true due to the electronic speed controller (ESC). We also simplify heat losses as a simple resistance, while in a real circuit there is a more complex impedance. These distinctions lead to differences between the theoretical and experimental results. Using the test results we are able to make a 3D plot and fill in most of the variables in formula 7 (torque, RPM, current, and voltage), then we can use this information to find the R value closest to that observed in the experiments. The software Octave makes the 3D representation so the error between the estimated power usage and the real power usage is as small as possible, giving the R value. Technically, Octave performs a linear regression with the cost function defined as the error of the estimated electrical power used. Formula 7 can also be rearranged to solve for R. Now that we have the R value for our motor, we plug in the values to formula 6 to calculate electrical power.

#### Overall Efficiency:

The efficiency of a motor is determined by dividing the mechanical power output by the electrical power input (formula 1). A goal for vehicle design is therefore to maximize this ratio and optimize the overall system efficiency by using the biggest propeller possible without overloading the motor.

This is why testing is so important. Using a giant propeller would drastically increase the propeller efficiency, but the motor would struggle so much to make it spin that its efficiency would be ridiculously low. Doing the opposite isn’t great either as making a tiny propeller spin very fast would lower both the motor and the propeller efficiency. The best solution is to balance both efficiencies to get the highest overall performance and system efficiency.

To achieve the highest efficiency the motor has to operate in the yellow zones of Figure 4 and 5 where there is a balance between torque and RPM. Testing various motors can help you figure out which size, Kv, and brand of motor will get you to that sweet spot for your operations. Figure 4: Motor efficiency for a 1500 Kv brushless DC motor Figure 5: Motor efficiency for a 1500 Kv brushless DC motor in 3D

## Interpretation - Best Operating Point

The three graphs in figure 6 demonstrate how motor parameters vary and how to optimize them to achieve higher performance. Figure 6: Parameters contributing to motor performance

The trend lines on these graphs can help you understand how to optimize your motor’s performance and operating conditions, whether you’re aiming for maximum flight time for your transport drone or maximum power for your racing drone.

In the left-most graph, the horizontal lines represent heat losses, which are dependent only on torque and current, not RPM. The lower torque and current your motor operates at, the lower the heat losses.

The graph in the middle shows the maximum power curve originating from the origin. If the motor does not operate along this line, it is operating at less than full power potential. A max power condition is ideal for winning a race, but not for increasing flight time or endurance.

Finally, the right-most graph shows the maximum efficiency curve. A motor operating on this line will use it’s battery more efficiently than anywhere else on the graph, thus increasing the flight time and endurance.

The location on the graph where you choose to operate depends greatly on the type of operations you are performing. The objectives of your flight should guide your design process and help you make decisions on which components to use.

When modifying the operating range of your motor, you will be looking at changing either your motor size, propeller size or both. In other words, you will be trying to optimize the load of the motor for its size. An easy way to tell if a motor isn’t efficient is to measure it’s temperature. A motor heating up too much is probably overloaded, AKA it is too small for its load. Furthermore, a motor not warming at all is probably too heavy or too big for its load, thus inefficient in that setup. Your needs will help you determine if you should start by modifying your motor or propeller size first.

## Conclusion

When evaluating the performance of a motor, using both theoretical and experimental methods will give you the best understanding of your device. The difference between theoretical and experimental results comes from incorporating theoretical assumptions in your calculations, and also from imperfections in your measuring devices. For example, the ESC isn’t perfect and might sometimes activate at the wrong time. Bearing friction is also not taken into account and the measuring instrument’s precision comes with an expected error.

The theoretical model is a good tool to understand intuitively how a change will affect the motor performance. To confirm your assumptions and optimize your system, you need to perform actual measurements in a systematic way. Motor performance can be improved in several ways and the best way to determine them is to compare theory with test results to get a better understanding of your whole system.

The challenges explained above and throughout this article highlight the need for both approaches to achieve a well-rounded understanding of the components you’re working with and a respect for their limitations. Having several reiterations of a design is very normal as the drone building process operates as a loop: Assume → Build → Test → Repeat.

For a practical extension on how to apply these concepts to your drone design, we recommend reading another one of our articles on How to Increase a Drone's Flight Time and Lift Capacity.

If you have any questions about the contents of this article or the tools we used, don’t hesitate to leave us a comment and we will be sure to respond. If there are any concepts you would like us to cover that we haven’t already, just leave us a note below.

### John

January 24, 2023

@Elvis P,
The far-right graph (which shows the efficiency curve), shows power consumption with the red-gradient. The “max efficiency” line are the RPM-torque combinations which procures the highest electrical efficiency.

When designing a drone, you’re not choosing an operating point on that graph, you’re choosing a propeller/motor combination that, for the thrust required for your drone, has a RPM and torque as close as possible to that max efficiency line.

Let’s say you want high hover efficiency for your 4 kg quadcopter. You’re therefore trying to find a motor and propeller that can produce at least 1 kg. Let’s say you find a KDE motor, and a 9×6 propeller. For 1 kg of thrust, that motor/prop combination has a torque and RPM far from the motor’s max efficiency line, meaning that you’re consuming more current than you need to for 1kg of thrust. You decide to switch to a 10×5 propeller, and now the torque and RPM needed for 1 kg of thrust is closer to the max efficiency curve, meaning you consume less current for the same thrust.

### Elvis P

January 16, 2023

Disagree with far right graph idea.

Drone needs X lifting capacity to fly and move.

To achieve this optimal flight mode, 100A consumed at 10k rpm
or
50A Consumed at 5k rpm, what makes your battery last longer ?

50A yes or no ?

So tork is king, leaving excess performance if crap happens.

Less power used = longer flying time at lower rpm.

So achieving on your middle graph 1000rpm or on the right graph 6000rpm is the same flight.

Example same end results:
1000rpm at 15A middle graph
or
6000 rpm at 60A right graph,
what would you choose?

### Lauren Nagel

December 12, 2022

Hi Paul,
That’s a good question. If you want mechanical power to be expressed in watts, then yes you should convert RPM to radians/s (by multiplying by 2*pi/60). We have found that RPM is more commonly used in the industry, so that’s why we used it in this article. The RPM calculations still allow you to compare mechanical power between propulsion systems, but you can do the extra conversion step if you prefer having results in watts.
Good catch!
- Lauren at Tyto Robotics

### Paul Martin

December 12, 2022

rpm? dont you mean radians/s if you want to get Nm

### MK

November 01, 2022

Hi Charles,

M

### Charles Blouin - Tyto Robotics staff

October 31, 2022

@MK: Good question. The current is measured at the ESC input, so the motor efficiency is the combined ESC+motor efficiency.

We recommend doing motor and propeller optimization first before working on ESC optimization. The gains that can be made with ESC optimization are much smaller than with proper motor and propeller optimization. Many parameters of the ESC can be optimized without measuring each phase voltage and current. For example, it is possible to measure the total current and ESC heat produced while varying the ESC switching frequency and control parameters.

### MK

October 27, 2022

Nice article, thanks!

However, you say say to get electrical power, simply multiply motor power by current (P=IV), but since the motor is seeing a 3-phase PWM voltage, I think it’s not so simple. Where are how are you measuring motor voltage and current?

Thanks!

### Lauren Nagel

May 19, 2022

Hi David,
I’m pleased to let you know that we actually host a database of motor, propeller, and ESC performance data: https://database.tytorobotics.com/tests
You can check out this article for instructions on how to apply filters to searches and make the most of it: https://www.tytorobotics.com/blogs/articles/how-to-use-the-database-for-drone-motors-propellers-and-escs
- Lauren at Tyto Robotics

### David

May 19, 2022

Hi,
I have a question: Is there a database I could lookup wide variety of motors efficiency instead of going into product sheets of one by one (and some don’t have it).
Not asking for a concrete model recommendation (even though you are welcome to give me), at least point me to the direction of consolidated info.

### mustafa

January 03, 2022

A 3 phase brushless motor has the following values. The maximum current drawn from the battery is 4.62 amps.. The highest lifting force is 4025 grams with a three-bladed fan 18 * 8.. The speed at the maximum lifting force is 2780 rpm. The battery voltage is 23.46 volts. How much is the output power? How much is the efficiency?

### Mustafa Ali

December 28, 2021

Thank u very much sir ..

### Charles Blouin - Tyto Robotics staff

December 16, 2021

@Alexandre Borowczyk When you look at the bottom of the motor efficiency graph, you see that the efficiency is going toward zero. This is because the mechanical power goes to zero, but the electrical power goes to the no load power. If we did not have this no load power, the efficiency would be undefined mathematically (0W/0W). The no-load current represents the inefficiencies in the motor due to bearing resistance, air resistance on the motor, and electrical switching losses.

### Alexandre Borowczyk

December 13, 2021

Thank for the great article, it is now cleaner for me why the manufacturer of bldc provide the winding resistance but I’m still trying to understand what is the purpose of providing de no load current (often taking the form of 0.2 A @ 10 V)

### Charles Blouin - RCbenchmark staff

February 22, 2021

@Shawn: We describe the process here: https://www.rcbenchmark.com/blogs/articles/how-to-increase-drone-flight-time-and-lift-capacity

Usually, you first define the operating parameters (weight, flight speed, and desired thrust). You then find the most efficient propeller for those conditions. After, you find the most efficient motor to generate the torque and speed required by the propeller. Finally, you may have to change the weight of the vehicle if you find that a different battery size or airframe is preferable. Those changes may require you to perform the optimization loop again.

### Shawn Shepard

February 22, 2021

Great article. I do have a question. I have run a tests on a motor with several different props for a fixed wing aircraft. I am still trying to figure out the best combination. I am looking at the overall efficiency vs Pitch Speed to find the most efficient combination at my anticipated cruising speed. Is this the appropriate approach? This will be a VTOL so I will need to look at the thrust for the vertical portion of flight and make a determination based on both flight modes