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![]() "Andrew Sarangan" wrote: Fiberglass epoxy will turn into a gel at a far lower temperature, around 100C. It won't withstand boiling water? |
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On Sep 19, 3:01 pm, Richard Riley wrote:
On Wed, 19 Sep 2007 11:18:58 -0500, "Dan Luke" wrote: "Andrew Sarangan" wrote: Fiberglass epoxy will turn into a gel at a far lower temperature, around 100C. It won't withstand boiling water? The epoxies used in homebuilts - cured at room temperature - generally start to soften around 200 degrees F. It varies with the epoxy and with what temperature any one part has been exposed to before - you can post cure many epoxies by subjecting them to higher temperatures, and get their transition temps up, by as much as 70 degrees F. The epoxies used in the 787 are cured at much higher temperatures to begin with. But this can't be too difficult for Boeing to explain. All they have to say is "our fiberglass is treated to handle as much heat as aluminum" or something similar, if that is indeed true. |
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On Sep 19, 11:22 pm, Richard Riley wrote:
On Wed, 19 Sep 2007 17:22:59 -0700, Andrew Sarangan The people that really matter - the FAA - already know. That assumes that FAA and Boeing are being faithful to their practices. I am not suggesting that they are not, but there are reasons to be cautious. We have seen examples in recent times where that assumption turned out to be false due to company financial pressures. If I were the head of Boeing's PR department, I'd hold off on trying to convince the public until it's clear whether the story has legs or not. Even the epoxies used for thing like this aren't as heat resistant as aluminum - but at some point it doesn't really matter. If the fuselage is seeing 400 degrees, there's something very seriously wrong, like the airplane is sitting in a giant pool of burning jet fuel. I can agree with that. But there are scenarios where the fuselage does not have to be soaking in burning jet fuel to see 400C. For example a service truck could be parked with its exhaust directly aimed at the fuselage. That may sound too simple and silly, but it was a silly thing like a foam block that caused catastrophic results for the space shuttle. In a situation like that I'm not sure whether aluminum or carbon will last longer. Aluminum WILL burn, once it gets hot enough, and is very energetic (think thermite). The carbon fibers themselves can withstand very high temperatures (think the leading edge of the space shuttle wing - carbon fibers in a carbon matrix). Epoxy will burn, but not all that energetically. As for crashworthyness - I know of three Berkuts that were absolutely totalled, where the occupants survived. One tumbled down the runway, one struck a high tension powerline, one deadsticked onto a freeway, got it's wing torn off by a tree and went head on into an SUV. I saw the wreck of Bill Davenport's Long EZ - engine out, wires tore off a wing, went inverted into a garage. He lived. Race cars are all composite now - and race driver deaths are very rare. Composite structures CAN be absolutely crashworthy. For the same weight as an aluminum structure, it can provide much more crash protection. I don't know how the 787 is being engineered, but I'd be very surprised if they were deliberately making it LESS crashworthy. After all - Boeing executives fly on these airplanes too. - Hide quoted text - I agree that composites have many advantages, and that's why I decided to build a composite aircraft. However, thermal stability is not one of their high points. |
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Andrew Sarangan wrote:
On Sep 19, 11:22 pm, Richard Riley wrote: On Wed, 19 Sep 2007 17:22:59 -0700, Andrew Sarangan The people that really matter - the FAA - already know. The FAA? That's a warm fuzzy. They can't find their ass with both hands most of the time. |
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FredGarvinMaleProstitute wrote in
: Andrew Sarangan wrote: On Sep 19, 11:22 pm, Richard Riley wrote: On Wed, 19 Sep 2007 17:22:59 -0700, Andrew Sarangan The people that really matter - the FAA - already know. The FAA? That's a warm fuzzy. They can't find their ass with both hands most of the time. Wheras you're probably expert at that. Bertie |
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On Sep 20, 11:56 am, Andrew Sarangan wrote:
On Sep 19, 11:22 pm, Richard Riley wrote: On Wed, 19 Sep 2007 17:22:59 -0700, Andrew Sarangan The people that really matter - the FAA - already know. That assumes that FAA and Boeing are being faithful to their practices. I am not suggesting that they are not, but there are reasons to be cautious. We have seen examples in recent times where that assumption turned out to be false due to company financial pressures. If I were the head of Boeing's PR department, I'd hold off on trying to convince the public until it's clear whether the story has legs or not. Even the epoxies used for thing like this aren't as heat resistant as aluminum - but at some point it doesn't really matter. If the fuselage is seeing 400 degrees, there's something very seriously wrong, like the airplane is sitting in a giant pool of burning jet fuel. I can agree with that. But there are scenarios where the fuselage does not have to be soaking in burning jet fuel to see 400C. For example a service truck could be parked with its exhaust directly aimed at the fuselage. That may sound too simple and silly, but it was a silly thing like a foam block that caused catastrophic results for the space shuttle. In a situation like that I'm not sure whether aluminum or carbon will last longer. Aluminum WILL burn, once it gets hot enough, and is very energetic (think thermite). The carbon fibers themselves can withstand very high temperatures (think the leading edge of the space shuttle wing - carbon fibers in a carbon matrix). Epoxy will burn, but not all that energetically. As for crashworthyness - I know of three Berkuts that were absolutely totalled, where the occupants survived. One tumbled down the runway, one struck a high tension powerline, one deadsticked onto a freeway, got it's wing torn off by a tree and went head on into an SUV. I saw the wreck of Bill Davenport's Long EZ - engine out, wires tore off a wing, went inverted into a garage. He lived. Race cars are all composite now - and race driver deaths are very rare. Composite structures CAN be absolutely crashworthy. For the same weight as an aluminum structure, it can provide much more crash protection. I don't know how the 787 is being engineered, but I'd be very surprised if they were deliberately making it LESS crashworthy. After all - Boeing executives fly on these airplanes too. - Hide quoted text - I agree that composites have many advantages, and that's why I decided to build a composite aircraft. However, thermal stability is not one of their high points. All commercial airports have a fleet of foam cannon fire trucks, don't worry be happy ! |
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