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On Sep 18, 10:46 pm, "Dan Luke" wrote:
"Andrew Sarangan" wrote: I have personally witnessed the post-crash fire of an experimental Velocity. When the fire was out, there was nothing left on the ground except some metal parts from the wheels, avionics and control links. IOW, about the same as what's left of a burned out aluminum airplane. I have only seen photos of metal airplane crashes, and in most cases you can tell that it was an airplane crash. Many tell tale parts of the airplane will remain intact. In this case you would not have known that this was an airplane crash. There were no discernible parts. Aluminum melts around 650C. Fiberglass epoxy will turn into a gel at a far lower temperature, around 100C. Most fiberglass airplanes can't even withstand normal heat from the sun unless they are painted white. So the fact that the glass airplane simply vaporized in the fire makes sense to me. In any case, my observations are only anectodal, and are based on homebuilt aircraft. Boeing may be using advanced epoxies with superior thermal and mechanical properties. If that is the case, it would be trivial for them to put these concerns to rest. I hope that is indeed the case, and that the 787 is not built with the same epoxy I am using on my homebuilt. |
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![]() In any case, my observations are only anectodal, and are based on homebuilt aircraft. Boeing may be using advanced epoxies with superior thermal and mechanical properties. If that is the case, it would be trivial for them to put these concerns to rest. I hope that is indeed the case, and that the 787 is not built with the same epoxy I am using on my homebuilt. Did you lay your composites up on a frame and bake them at high temperature and pressure in a giant autoclave to cure them? If not, then I bet you aren't using the same materials or processes... |
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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 18, 11:35 am, C J Campbell
wrote: On 2007-09-18 07:06:06 -0700, WhoGivesAFig? said: This could be huge http://seattletimes.nwsource.com/ABP...2003889769.pdf Hmmm. A retired employee who worked for Boeing for 46 years claims to know more than the FAA and Boeing about how planes should be crash tested. He concludes that composites are not as crashworthy as metal, but does not back his assertions up with any hard data. His complaint is that composite materials are stronger in some directions than they are in others, that cracking is less visible, and that composites are more subject to fire and more vulnerable to lightning. He points out that g levels in a crash are unlikely to be uniform all along a composite structure. All of this is true, but he seems to be alleging some sort of Boeing coverup of these facts. He discounts actual experience with other composite aircraft, saying that either they are not airliners subjected to the stress and number of flights that airliners get, or that the numbers of such composite aircraft are too few to be statistically significant. Of course, his report will make great fodder for trial lawyers when the first 787 crashes, no matter what the actual cause of death of the passengers is. Weldon seems to be down at the site trying to tell people how to crash test an airplane even though he no longer works there. No doubt his experience is valuable, but he cannot possibly be aware of everything that Boeing is doing to mitigate these problems and Boeing is certainly not going to give corporate secrets to former employees. -- Waddling Eagle World Famous Flight Instructor Plus his degrees are obsolete, BS 1960, MS 1970 ![]() |
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Richard Riley wrote:
On Tue, 18 Sep 2007 10:06:06 -0400, WhoGivesAFig? wrote: This could be huge http://seattletimes.nwsource.com/ABP...2003889769.pdf Or it could be nothing. Real world experinece with smaller composite airplanes have showed them to be MUCH more crashworthy than aluminum airplanes. Composite small planes have been certified for lightning strike before. You are correct. I should have said "May" be flawed |
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