| > DC motors are multiple times smaller and lighter than the equivalent powered turbine engine when you consider the entire system. Airplanes this size can use cruise missile engines, which are very light. See the F-5 for more info (7:1 thrust to weight ratio.) > On top of that you totally eliminate the need for variable pitch props Why is that? Variable pitch props have nothing to do with engine type. They're variable to be more efficient depending on RPM and speed. > You also negate a lot of hydraulic systems (and their redundant backups) without the need for things like fuel pumps, thrust reversers, Not really. A lot of flight controls are boosted with hydraulics, and thrust reversers are for increasing drag (descending faster or slowing down.) None of these depend on engine type. The real issue with electric planes is that they're a fire hazard. Already people have been killed when their electric plane's battery caught fire mid-air: https://www.flyingmag.com/two-people-killed-in-first-crash-e... The JAL 787 battery fire was a near-tragedy and resulted in interruption of service to SJC for 2 months: https://en.wikipedia.org/wiki/Boeing_787_Dreamliner_battery_... I find the most erroneous posts on HN to be about airplanes and databases. |
Variable pitch props have everything to do with engine type. They exist because turbine and piston engines have a very specific power/torque curve which requires them to operate at certain RPMs for certain conditions to achieve peak efficiency. With electric motors you have no need for this because you get a constant increase of efficiency across the entire power curve.
>Not really. A lot of flight controls are boosted with hydraulics, and thrust reversers are for increasing drag (descending faster or slowing down.) None of these depend on engine type.
Thrust reversers have nothing to do with descending faster or slowing down in flight, they are used solely for landing retardation. But an electric aircraft wouldn't even need thrust reversers. You literally just reverse the propeller immediately at full power when touching down. You can even save on less flaps required because the motors will be able to "windmill" on the descent and slow the aircraft as well as regen power.