Interesting decision to build the whole aircraft instead of the propulsion system only. I wonder what the decision process was between retrofit of existing turboprop frame vs. build from the ground up? I would expect the level of effort and certification to be much higher building from scratch even though you get complete control.
It may be too hard to do a good retrofit. If you basically have to tear the entire plane apart and rebuild and recertify it to put batteries in the right places, maybe the costs aren’t worth it for potential customers.
I know many planes use their wings as fuel tanks but given the weight of batteries maybe that doesn’t work.
I agree it’s interesting. Not a small undertaking.
Generally all the weight of the fusaage has to go through the wings anyway so it is structurally more efficient to put weight on the wings in the first place.
Judging by the seats, perhaps making it as light as possible. Existing airframes are relatively light but let's be honest, they aren't trying to save 500g here and there when they have massive jet engines to get everything airborne.
I discussed with people working on aircraft components, and my understanding is that weight is a constant obsession for them. Propose a new system to Airbus/Boeing, and the first question they'll ask is "how much does it weight?"
Every kg saved is a kg more of freight that can be transported (or a little less fuel used to keep the plane in the air); save 500g for each seat of a 200-seat plane, and you can put one more paying passenger in the cabin.
Heart Aerospace (YC W19) just flew the largest electric airplane ever flown — a 100-foot wingspan, a takeoff weight of 25,000 pounds, and $5 of electricity to get it off the ground.
In the video he explains that the goal of the hybrid system is mainly to be used when for some unexpected reason the airplane cannot land at its original destination.
I’ve been tinkering with the idea of a hybrid system where the ICE system is its own bolt on component to an electric aircraft that is used for takeoff and altitude before it detaches and returns to the airfield before the aircraft cruiser on electric power.
Could even have a rocket launch version for cargo
The interior of the plane is clearly designed by an engineer. They stripped everything down to save weight, passenger comfort be dammed. The seats don't even look comfortable.
They need to hire an actual designer, if the plane weighs 0.5% more but has actual human usability that's worth it.
But maybe they’re aiming at short haul cargo. And either way, wouldn’t that really be one of the last things to do? Just proving the plane can even get in the air and stay there for a useful distance on electricity is more important than how comfortable it is.
Interesting decision to build the whole aircraft instead of the propulsion system only. I wonder what the decision process was between retrofit of existing turboprop frame vs. build from the ground up? I would expect the level of effort and certification to be much higher building from scratch even though you get complete control.
It may be too hard to do a good retrofit. If you basically have to tear the entire plane apart and rebuild and recertify it to put batteries in the right places, maybe the costs aren’t worth it for potential customers.
I know many planes use their wings as fuel tanks but given the weight of batteries maybe that doesn’t work.
I agree it’s interesting. Not a small undertaking.
Generally all the weight of the fusaage has to go through the wings anyway so it is structurally more efficient to put weight on the wings in the first place.
And they do that with fuel?! Neat!
Judging by the seats, perhaps making it as light as possible. Existing airframes are relatively light but let's be honest, they aren't trying to save 500g here and there when they have massive jet engines to get everything airborne.
I discussed with people working on aircraft components, and my understanding is that weight is a constant obsession for them. Propose a new system to Airbus/Boeing, and the first question they'll ask is "how much does it weight?"
Every kg saved is a kg more of freight that can be transported (or a little less fuel used to keep the plane in the air); save 500g for each seat of a 200-seat plane, and you can put one more paying passenger in the cabin.
Heart Aerospace (YC W19) just flew the largest electric airplane ever flown — a 100-foot wingspan, a takeoff weight of 25,000 pounds, and $5 of electricity to get it off the ground.
These kind of startup excite me. More so than the "next killer app."
the concept of electric motors with ultimate "any" fuel flexibility for generators is definitely the future
then we are not tied to global fuel politics
and maybe airports will become far less toxic with leaded fuel finally being completely eliminated
(and there is a Ycombinator video channel? never knew)
Agreed, however only fuel for piston engine aircraft is leaded. Not many of them at a large commercial airport. More of a GA issue.
Thought this was a great watch, as a first time founder myself!
From the video:
Range: 125 miles all electric
In the video he explains that the goal of the hybrid system is mainly to be used when for some unexpected reason the airplane cannot land at its original destination.
There are maybe some advantages to a hybrid system.
The higher reliability of electric.
Losing an turbine engine doesn't mean asymmetrical thrust. Plane still flies normally.
Losing an engine on takeoff you still have full power.
Electric motors spin up faster than turbines. Which means faster throttle response. Which you need when hit with a wind shear on landing.
Take off and landing under electric power means much less noise.
Efficiency, you can increase the number of props or fans to get a much higher bypass ratio. Worth noting the plane in the video has four props.
I’ve been tinkering with the idea of a hybrid system where the ICE system is its own bolt on component to an electric aircraft that is used for takeoff and altitude before it detaches and returns to the airfield before the aircraft cruiser on electric power. Could even have a rocket launch version for cargo
Hope it's accurate. Sounds good to be true.
The interior of the plane is clearly designed by an engineer. They stripped everything down to save weight, passenger comfort be dammed. The seats don't even look comfortable.
They need to hire an actual designer, if the plane weighs 0.5% more but has actual human usability that's worth it.
Really, a prototype airplane, the first of this size ever built with this novel propulsion system, had engineers involved in the design?
But maybe they’re aiming at short haul cargo. And either way, wouldn’t that really be one of the last things to do? Just proving the plane can even get in the air and stay there for a useful distance on electricity is more important than how comfortable it is.