Battery Weight Fraction Formula:
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Battery Weight Fraction is the ratio between battery weight to gross weight of an aircraft. It is a dimensionless number that indicates what portion of the total aircraft weight is occupied by the battery system.
The calculator uses the Battery Weight Fraction formula:
Where:
Explanation: The formula calculates the fraction of aircraft weight that must be allocated to batteries to achieve a specified range, considering battery energy density, system efficiency, and aerodynamic performance.
Details: Battery weight fraction is crucial for electric aircraft design as it directly impacts the aircraft's range, payload capacity, and overall performance. A lower battery weight fraction allows for more payload or better performance.
Tips: Enter range in meters, battery specific energy capacity in J/kg, efficiency as a decimal between 0-1, and maximum lift to drag ratio. All values must be positive numbers.
Q1: What is a typical battery weight fraction for electric aircraft?
A: Battery weight fraction typically ranges from 0.2 to 0.5 for most electric aircraft, depending on the desired range and battery technology.
Q2: How does battery technology affect the weight fraction?
A: Higher specific energy capacity batteries (more J/kg) result in lower weight fractions for the same range, or longer range for the same weight fraction.
Q3: Why is efficiency important in this calculation?
A: Efficiency accounts for energy losses in the propulsion system, including motor, controller, and transmission losses.
Q4: How does lift-to-drag ratio affect battery weight?
A: A higher lift-to-drag ratio means the aircraft can fly more efficiently, requiring less energy and therefore less battery weight for the same range.
Q5: Can this formula be used for other electric vehicles?
A: While the basic principles apply, this specific formula is optimized for aircraft where lift-to-drag ratio is a critical aerodynamic parameter.