Swiss' Entire Boeing 777 Fleet Now Has Shark Skin Technology
simpleflying.com
simpleflying.com
Anyone knows how long a airplane has to fly to be written of?
It's far less comparatively strong under compression, which seems to have been the principle failure mode of the now-permanently-submerged Titan.
The failure modes of explosive vs. implosive failure are also relevant. High-pressure implosions tend to collapse the entire hull, whilst so far as I understand, explosive failure, particularly at the relatively low pressure differentials of air and space flight, tend to be localised, and the fibre-reinforced nature of composite materials should reduce damage to the neighbourhood of the initial failure point in many cases. Implosive failure needn't actually penetrate the hull so much as crease it, a mode which CF handles poorly respective to the application.
Hence sci-fi horrors is like getting sucked out into space through a pinhole.
Most of you would still be at the right pressure, and skin is pretty tough stuff.
yes
> so metal oxidation isn’t an issue
no. It's not rust, but that higher pressure air can hold more water at the same relative humidity. The higher pressure air is achievable because carbon fiber has higher tensile strength per weight.
The 787 and A350 cabins have higher relative humidity.
> no. It's not rust,
Citation needed. Corrosion resistance is one of the most advertised benefits of the composite materials in those aircraft[1][2].
1: http://www.lb.boeing.com/commercial/aeromagazine/articles/qt...
2: https://skybrary.aero/sites/default/files/bookshelf/3851.pdf
Thanks!
Edit: it's between 6000 and 8000: https://aviation.stackexchange.com/questions/66563/why-arent...
So around 8000 for the likes of the bog standard 737 and A320 and around 6000 for the cool new carbon fibre ones I guess.
Also, if you want to go for a walk, the distance you are allowed to walk is a lot further.
That is quite nice as a passenger, but also a big part of why they're no longer made, and why most airlines are phasing them out...
Airliners are required to do different checks at different stages, and the big one costs millions of dollars and requires them to basically disassemble and rebuild the plane. They even may have to remove the paint to check the hull for issues. Industrialized nations generally will only do this a couple times before the cost is more than the jet is worth (I think this is generally around 20,000 cycles, depending on the plane) then they sell them to a third world airline who doesn't have as strict a regulatory scheme. Even then, they generally live on for quite awhile, our regulatory scheme is designed to get as close to zero risk as possible, not to be economical, and it's hard to argue with the results. This is one of many reasons why there are an order of magnitude more crashes in the developing world, though even still safety is high relative to almost anything other than first world commercial airlines.
... mechanics could count on tell-tale build-up of nicotine around cracks as air escaped from the passenger cabin when the plane pressurized after lift-off."
https://www.upi.com/Archives/1988/05/27/The-recently-imposed...
I wonder if it could be made significantly worse. Leg room has been reduced overtime as far as I can tell. I’m 198cm, and it’s actually hell. I probably need to just pay more and go nearer the front, however this would only solve the legroom problem. The seats are too low and aren’t even close to supporting someone tall. I’m in NZ so everything is far away, and 18+ hour flights are actually awful.
I’m flying on an A380 in a few days, that will be interesting experience after only flying long haul on 777s in the past few years
Sure, we'd expect certain engineering things to get cheaper over time, but you can also see why some luxury touches got phased--or rather priced--out. :p
I suspect that pressure hull and wing spars experience the greatest loading and fatigue, and may be differentially influenced by overall flight time and takeoff/landing cycles.
The criteria might have changed since that incident.
Maintenance schedules are based on hours. Pilot experience is also logged as hours.
For those unfamiliar, a 1988 airline incident in which a Hawaiian airliner experience explosive decompression, though 94 of 95 occupants survived. The lone fatality was a flight attendant who was sucked out through the hole, and if my memory of the post-incident report stands, actually contributed to much of the fuselage damage by enlarging the initial failure region.
<https://en.wikipedia.org/wiki/Aloha_Airlines_Flight_243>
Another of my references are the US B-52 Stratofortress fleet, the youngest of which were built 61 years ago in 1963, for which active status is anticipated to extend into the 2050s. My understanding is that wing loadings/unloadings are the limiting factor, with virtually all other parts of the plane being capable of replacement.
<https://en.wikipedia.org/wiki/Boeing_B-52_Stratofortress>
The overall airframe is rated for 32,500 to 37,500 hours, with aircraft experiencing about 380 flight hours/year. The wing upper service being the lowest limit of body parts indicated here:
Hearing him tell the story first hand was pretty incredible. He saw sky, so knew he had a hole… but had no idea it was so extensive until they landed and he walked back there.
Can you imagine the phone footage we would have had from that it if it happened today?!
Pretty much every aircraft pressurizes to below 8k feet because of regulations.
Supposed these panels were $100k/plane.
Jet fuel costs $0.36/lbs and a 777 burns about 30 lbs/nm in cruise. Suppose a 777 averages 14,000 nm/day. That's 420,000 lbs/day or $151,200/day. 1% savings would be $1,512/day, so the break even point would be roughly 2 months and would be profitable from then on. Suppose a 2 year lifecycle. That a savings $500k per year per plane.
Put a little more thought and data into your comments if you would be so kind.
P(success)*reward - P(failure)*penalty - opportunity cost (TCO)
Worth doing for the environment even if it's cost neutral probably.
I’m not saying this is a negative , just that plastic pollution is a huge issue , I can’t see this stuff making the situation much better.
The ROI appears to be 2 years. Considering the application is relatively easy, this looks like a good deal for airlines.
I've spent a few minutes looking for imagery of the film itself, sufficient to show details. There's surprisingly little, and I suspect the manufacturer doesn't want visual details of the skin itself available.
There's a schematic in the link below, which also shows the contrast of the AEROShark film to actual shark skin. The film is more grooves than scales, for those curious.
<https://swiss.newsmarket.com/english/press-releases/swiss-ad...>
While it's at this point obviously tested and proven to work, I wonder about the size of that texture in relation to the texture on actual shark-skin, and whether they are working at similar Reynolds numbers.
That makes it a tiny airline in comparison to others. For example Lufthansa group (which Swiss is a part of) has 98 wide-body aircraft. Competing Air France group has 165. The US is similar, Delta has 164. The Middle East is on another scale, Emirates has 249...
Still a nice innovation, but as a headline "Lufthansa group tests shark skin on 12 Boeing 777s" would be more realistic.
Each 777 can carry about 150 ton of fuel.
So they got about 15 fill ups free
No, It says a week in the article.
“Each aircraft takes about a week to have its AeroSHARK film applied, which requires high-precision workmanship from our personnel.”
I guess Swiss is Lufthansa's test before rolling it out to the rest of the group's brands.
I'm not going