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At 12:33 11 February 2020, Martin Gregorie wrote:
On Mon, 10 Feb 2020 19:12:42 -0800, Eric Greenwell wrote: Your chart doesn't account for the efficiencies in converting energy to propulsion. An electric motor will deliver about 95% of the electrical energy to the propeller, but only about 40% of the gasoline energy will be delivered to the propeller. Since it is propulsion we desire, not just stored energy, you should reduce the lead acid and lithium battery sizes by 55% to account for their greater energy to propulsion efficiency. Fair point, but SLA still shows as a non-starter while SAFT cells are still six times the weight of hydrocarbon and occupy at least 25 times the volume. The one thing we both missed, though is that a good brushless motor plus its controller will be a lighter and smaller than the equivalent ICE piston engine driving a propeller. Has anybody got numbers for this? IOW, is motor+controller+prop+Li-ion battery still heavier than petrol+piston engine+prop? It will almost certainly be heavier than a Jet-A+turboprop engine+propeller. And, or course, empty fuel tanks are a lot lighter than full ones but a flat battery weighs the same as a fully charged one. Not Quite True. Since a charged battery contains a greater total amount of energy than a dead battery, the earth's gravity will pull more strongly on it. But you will have trouble measuring the difference ;¬)) |
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On Tuesday, February 11, 2020 at 5:15:04 AM UTC-8, Tim Newport-Peace wrote:
Not Quite True. Since a charged battery contains a greater total amount of energy than a dead battery, the earth's gravity will pull more strongly on it. But you will have trouble measuring the difference ;¬)) But seriously, no. Energy in and of itself has no mass. A an old-time watch or windup toy has the same mass regardless of whether it is wound or unwound. |
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Martin Gregorie wrote on 2/11/2020 4:33 AM:
On Mon, 10 Feb 2020 19:12:42 -0800, Eric Greenwell wrote: Your chart doesn't account for the efficiencies in converting energy to propulsion. An electric motor will deliver about 95% of the electrical energy to the propeller, but only about 40% of the gasoline energy will be delivered to the propeller. Since it is propulsion we desire, not just stored energy, you should reduce the lead acid and lithium battery sizes by 55% to account for their greater energy to propulsion efficiency. Fair point, but SLA still shows as a non-starter while SAFT cells are still six times the weight of hydrocarbon and occupy at least 25 times the volume. The one thing we both missed, though is that a good brushless motor plus its controller will be a lighter and smaller than the equivalent ICE piston engine driving a propeller. Has anybody got numbers for this? IOW, is motor+controller+prop+Li-ion battery still heavier than petrol+piston engine+prop? It will almost certainly be heavier than a Jet-A+turboprop engine+propeller. And, or course, empty fuel tanks are a lot lighter than full ones but a flat battery weighs the same as a fully charged one. We are all agreed that short powered range favors electric power, while long range favors fossil fuel power. The details, such as overall weight, become very interesting in the design of a self-launching sailplane, because the desired power range is much smaller than for an airplane. Schleicher's ASH 26E and AS-34 are 18M span gliders with similar gliding and power performance. That would be a good start for comparing propulsion systems. My impression is the propulsion systems have similar weights. Note the fuel weight is not significant for powered ranges less than 250 miles: the 26E holds 4 gallons, only 25 pounds in a 1020 pound glider (including pilot). High density altitude favors the electric systems, because the motor power does not decrease with altitude, unlike the normally aspirated Wankel or two-stroke engines. The smaller, lighter, but powerful electric motors give electrics an advantage unmatched by IC engines: they make the FES system practical. For us, all this talk about electric powered seaplanes, passenger carrying airplanes, and alleged fraud is irrelevant: electric powered gliders are available from all the major manufacturers and some of the smaller ones. They will only get better and more numerous. -- Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me) - "A Guide to Self-Launching Sailplane Operation" https://sites.google.com/site/motorg...ad-the-guide-1 |
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On Tuesday, February 11, 2020 at 4:33:26 AM UTC-8, Martin Gregorie wrote:
..The one thing we both missed, though is that a good brushless motor plus its controller will be a lighter and smaller than the equivalent ICE piston engine driving a propeller... Not only that, but it delivers smoother power with less vibration, delivers it the moment it is started, requires less service infrastructure (starting, lubrication, cooling, exhaust, etc), and can easily be positioned for stowage. It runs cleaner and cooler and more predictably under a wider range of conditions, and is more easily monitored for performance and troubleshooting. --Bob K. |
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On Tue, 11 Feb 2020 10:16:45 -0800, Bob Kuykendall wrote:
On Tuesday, February 11, 2020 at 4:33:26 AM UTC-8, Martin Gregorie wrote: ..The one thing we both missed, though is that a good brushless motor plus its controller will be a lighter and smaller than the equivalent ICE piston engine driving a propeller... Not only that, but it delivers smoother power with less vibration, delivers it the moment it is started, requires less service infrastructure (starting, lubrication, cooling, exhaust, etc), and can easily be positioned for stowage. It runs cleaner and cooler and more predictably under a wider range of conditions, and is more easily monitored for performance and troubleshooting. Another thing, but this probably doesn't affect us much: a brushless motor, which all these units are, has its rpm set primarily by the rate at which the controller switches power round its (static) field coils and, when driving a propeller, isn't much affected by the load its working against. Its one reason electric brushless motors are popular with the RC and CL aerobatic crowd - the nearly constant RPM causes airspeed on uplines and downlines to be more constant than it ever was with IC engines. -- Martin | martin at Gregorie | gregorie dot org |
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