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Airliner engines are sized to continue the takeoff if one engine fails after it has become too late to brake. This means that the oversized engine has to be lugged around the whole flight, increasing weight and drag. Creating traditional brakes that could withstand the heating of a rejected takeoff just before rotation would also add significant weight.

The brakes on the SKYLON spaceplane boil water during abort, and it appears that the steam is dumped. The water is fed by pyrotechnic blowdown. Following a successful takeoff, the water is dumped overboard. This saves weight for the remainder of the flight.

My question is, can this approach be used to save weight on airliners?

SKYLON info. https://web.archive.org/web/20151129034506/http://www.reactionengines.co.uk/tech_docs/SKYLON_Users_Manual_Rev_2.1.pdf https://web.archive.org/web/20110615104534/http://www.reactionengines.co.uk/tech_docs/JBIS_v57_22-32.pdf https://forum.nasaspaceflight.com/index.php?action=dlattach;topic=36826.0;attach=1073534

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This solves the problem of rejected takeoff, which is certainly a major factor in brake design. However, dumping the water after takeoff means that benefit is unavailable for landing. Events such as flap issues can require an aircraft to land at a higher speed than usual, requiring more braking capacity. The difference between this and rejected takeoff may not be enough to justify the weight, complexity, and expense of the water cooling system.

fooot
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I'm sure it could be used, the question is what problem it would solve that would make it worth doing. Dumping water for each take-off means more stuff that could break on the aircraft itself, and more stuff that requires maintenance every now and then.

Having to refill the airliner with water prior to each takeoff would require extra infrastructure on the ground; if water-cooled brakes are critical for operating the aircraft, you probably wouldn't be allowed to use just any water. Distilled water refilled using a documented process would probably be a must, adding time and making the whole thing more expensive to operate.

Airliners routinely operate in cold weather, so the ground supply and aircraft mechanisms have to account for that. No point having efficient brakes if they are frozen solid as a result of having to wait 10-15 minutes extra prior to takeoff. You can of course install heaters, but that adds additional costs and complexity.

All this stuff would mean nothing for anyone traveling with the airline. Compared to airlines using conventionally braked aircraft tickets are likely to be more expensive, driving people to use the cheaper non-water-cooled airlines.

bjelleklang
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  • From what I hear, airliner engines are sized to continue takeoff if one engine fails when the plane is moving too fast. This is especially bad for today's twinjets. And that is why I was thinking of a lightweight high-power braking solution to allow braking instead of needing overpowered engines. – Abdullah is not an Amalekite Apr 28 '20 at 16:15
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    More powerful brakes don't allow you to get rid of engine-out redundancy. If the engine fails just one foot off the ground, you can have the most powerful brakes in the world, they won't help you one bit. – Jörg W Mittag Apr 29 '20 at 09:06
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Of course, they could technically use water-cooled brakes, but there are downsides. For example, airports don't want water spilt all over the ground just because one airplane had some hot brakes. It's just more efficient to taxi around and wait for the brakes to cool down. Plus, it would be too expensive to install a whole water brake-cooling system, for something that just doesn't happen that often.

So to sum it up,

  1. It interrupts airport operations

  2. It's too expensive

BONUS: The airline manufacturer would have to get permission for the technology

Air Canada 001
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