The difficulties of providing 110-volt power to your airline seat
theatlantic.com
theatlantic.com
http://www.tekkeon.com/products-mypowerall.html
I bought a male Adaptaplug and a Magsafe cord from eBay, and after 5 minutes with a soldering iron, it works for my 13" unibody MacBook as well. I plan on upgrading to a 13" MacBook Air soon. I should be able to get 14 hours working time from this setup.
As a companion to my WiFi iPad, it's great. The Cradlepoint will run for 18 hours off of it. (I have the MP3450.) Not small enough for a pocket, but it fits fine in most laptop bags.
EDIT: I bet there's a business renting these things out to people at airports!
About time the lower orders did some work.
Come to think of it. Maybe we should have excercise bikes in 1st powering economy. On board gym?
Given that the power output of the engines of a Boeing 747 is 140MW [1], enough to power 15 copies of the Empire State Building at peak business hours[2], I find this impossibility a bit depressing.
[1] http://en.wikipedia.org/wiki/Orders_of_magnitude_(power)#meg... [2] http://depletedcranium.com/what-is-a-megawatt/
The numbers get a bit more complicated when you figure in the weight for transformers, alternators, inverters, etc. But fuel is not a major component of this. The math really doesn't support the assertion that it's not cost-effective.
How do you figure?
Say some extra weight delta_w in additional equipment is required, and say that the fuel required to complete a given flight is a function f of the plane's weight, and that the cost of the fuel is C. Further, let the lifetime maintenance cost of the new equipment be E, and the lifetime maintenance of the plane's structural components be g, also a function of its weight. As a rough approximation, the additional cost should be
E + C df/dw|_W * delta_w + dg/dw|_W * delta_w
(Note that, really, f is a function of both passenger power consumption and of weight, both of which we're varying here, but I'll buy your argument that df/dp|_P * delta_p is neglible in comparison to f(P,W))
The article asserts that one or both of the derivates in this equation are large enough that its product with delta_w is non-negligible (in fact, prohibitive). I'm guessing that df/dp is not the problem, which is the only term you really addressed.
More to the point, 240W is irrealistic for a laptop. Most laptops consume under 40W. With this better estimation, this is 1/117th of a percent.
It's more than just fuel costs.
Someone please correct me if I'm wrong, but I believe this article is defeated by the actual fact of the matter that some planes do have AC to all the seats.
When designing an aircraft and its sub-systems, the engineer provides power availability specifications. The people who make the headlights, avionics, and coffee machines are all aware of the common power configurations and design their equipment to work with that specification directly. I used to work on light aircraft (private), which all used 24 VDC. Everything in the plane was designed to run on 24 VDC. Commercial airliners likely have more than one voltage specification available, but I'd imagine it's all DC.
Any time you have to convert voltage, you're going to lose some efficiency. Inverters (DC to AC) have some particularly nasty characteristics that make them undesirable on an aircraft. A DC voltage converter would work, but you still introduce some degree of inefficiency. A good switching DC voltage converter can exceed 90% efficiency, but so can an AC inverter. Neither operates at that efficiency all the time though. I know that AC inverters perform best when run at close to nominal load. At lower current levels, efficiency drops. I don't know enough about DC converters to say.
Add to this the fact that inverters and converters are heavy, and you can begin to understand why a power outlet at each seat is problematic.
(Also, some older private aircraft, such as mine, use a 12VDC standard.)
Yes there was no in-flight entertainment in mid-60s, but avionics back then were still to a great extent valve-based and consumed gobs of power.
Of course, doing the rolling blackouts might encourage less use of devices, reducing power use.
Most people would really only want a few hours of charging. Then you could have a capped number of active sockets per flight of say 50-100 seats.
I've had trouble connecting a laptop that wants to charge to inverters before, so this isn't without reason.
For those advocating for a low-voltage DC power source, look at Empower--it's installed on more than 40 airlines. 15V DC, 75W.
http://en.wikipedia.org/wiki/EmPower_%28aircraft_power_adapt...
(240 watt) * 12 hour * 500 people / 45 MJ (energy dencity per gallon) / .35 energy effecency = 330 gallons * 6.8 lb / gallion = ~2244 pounds. Granted this is probably +/- 30% depending on the fuel, engine effecency, transmission losses etc.
For comparison a 12 hour flight would burn ~ 43,000 gallons or 292,000 lb of fuel.
True, not laptops have the same AC plug, so an adapter would be necessary.
http://img.hisupplier.com/var/userImages/old/selong/selong$7...
So it's definitely doable, and I'd be prepared to bet money that it runs off the same APU that powers the entertainment system.
Also I don't really want to work on laptops in tight space anyway. A 5V USB port is sufficient. All Air Canada flights have this. (Due to RIM I guess?)
36vDC would have similar weight problems and, in addition, would require everybody to buy and haul around Yet Another Power Brick since it is oddball.
I would expect the VOD display system to be running around 10W. My guess is 1W lost in a 90% efficiency power supply, 5W for the display, 1W for an ARM processor, the rest for the video decoder chip and miscellaneous support chips.
Why not just use a switching power supply to change that to 60hz 110v? Why this whole business with inverters?
One way to change the frequency of a power source is through a double-conversion type AC/AC converter, i.e. 1st stage is a rectifier which outputs a DC voltage - this is an arbitrary DC voltage, but it needs to be within the voltage tolerances of the 2nd stage - an inverter, which reconstructs an AC voltage from the DC link to whatever frequency you like.
This setup is also the basis of most UPS systems btw, with a battery connected in the DC link.
It is in fact possible to use a switching circuit to convert an arbitrary ac voltage/frequency to another arbitrary ac voltage/frequency directly without a DC link intermediary. This is called a "matrix converter." http://en.wikipedia.org/wiki/AC/AC_converter
So it should theoretically be possible to take say 200VAC at 400 Hz and convert this to 120VAC 60Hz. In fact this would probably be more compact/less expensive than the usual inverters mentioned in this article, since these are usually meant to be powered by a low voltage DC source and thus have to deal with taking a low voltage and very high current and first stepping this up to several hundred volts, then modulate it into an AC sine wave. A matrix converter (or even AC-DC-AC converter) would have no such requirement if it were powered from the already high voltage aircraft power bus.
At this point I think it's a matter of the technology catching up, since this is a highly specialized application that has just recently become an opportunity for innovation.
EDIT: Also - 240W per person? This seems outrageously high as a baseline load. I would estimate more like 50-100W per person on average, with 300W peak (like when the power supply is first plugged in.) The peak loads would not all happen at once unless everyone decides to plug in and turn on their computers at once, in which case the power limiting would kick in...
To supply 10x the current, you need substantially larger wires. Wires are heavy. Airlines don't like heavy, it costs a lot of money over the lifetime of an aircraft to haul non-fare paying weight around.
Another point, 12vDC is not a typical aircraft voltage, so a DC-DC converter would be needed to generate the 12vDC. 12vDC is typically not a native laptop input voltage (19vDC is more typical), so another DC-DC converter would be needed. At that point, an inverter (DC-AC) and normal laptop power supply (AC-DC switcher) makes more sense (efficiencies are similar).
There are DC adapter plugins in aircraft - the idea is that they are only sold for laptops and are expensive enough that few people use the.
I don't use it very often because all the cords that it would require annoys me, and my laptop has 12 hours of battery life. But it is there, leading me to believe that this is not actually a problem.
(I think the fact that it's DC power limits the number of people that will use it, because you have to plan ahead, and nobody ever plans ahead for flights except seasoned travelers. If it was AC power, people would plug stuff in just for the hell of it, instead of reading a book as they do now.)
I am not familiar with any specific methods of causing a large explosion that access to a 120V AC socket would allow, which not having access to one would not, with what is currently allowed to passengers through airport security [0]; But considering that producing a cigarette lighter or some nail polish remover in the cabin are grounds to be tackled by an air marshal and prosecuted, an electrical outlet is a hell of a lot of accessible power.
[0] kindly disregard my past five minutes' search history, NSA sniffer