I look forward to aircraft that don't require complex and expensive to maintain gas turbine engines. It's going to be a while though, as battery density has a ways to go, and recharge rates with the current generation are still lacking. Though the trend may accelerate if we stop externalizing the costs of carbon fueled flight.
Some interesting numbers. Jet A has an energy density of 12500 watt-hours per kg. Typical lithium ion is about 200 watt-hours per kg.
Typical single cycle gas turbine engines are about 30% efficient, so that's about 3750 watt-hours per kg adjusted. So about 200/3750. However, the weight of the engine itself is a big deal.
A v2500A5 engine (737/A320F) weighs about 2500kg. An equivalent electric motor would weigh about 300kg. Thats 4,000kg more payload, or lighter weight. With AC each extra KG you carry means more energy to go the same distance. Its a compounding problem, so any saved weight is a big deal. So the electric option may see practical use sooner than the raw energy numbers would predict.
The other interesting aspect, is that instead of 2-4 large ducted turbofans, an electric aircraft could use numerous distributed electric ducted fans. They could be integrated into the fuselage, or spread over an unusual wing structure. These newer designs have shown promise in modeling, and could reduce the energy required for flight significantly. Since aircraft design and certification is done over the timespan of decades, its going to be 20-30 years before they reach mainstream though.