A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

787 flawed



 
 
Thread Tools Display Modes
  #1  
Old September 19th 07, 05:18 PM posted to rec.aviation.piloting
Dan Luke[_2_]
external usenet poster
 
Posts: 713
Default 787 flawed


"Andrew Sarangan" wrote:
Fiberglass epoxy will turn into a gel at
a far lower temperature, around 100C.


It won't withstand boiling water?


  #2  
Old September 20th 07, 01:22 AM posted to rec.aviation.piloting
Andrew Sarangan
external usenet poster
 
Posts: 382
Default 787 flawed

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.


  #3  
Old September 20th 07, 05:56 PM posted to rec.aviation.piloting
Andrew Sarangan
external usenet poster
 
Posts: 382
Default 787 flawed

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.



  #4  
Old September 20th 07, 07:44 PM posted to rec.aviation.piloting
FredGarvinMaleProstitute
external usenet poster
 
Posts: 21
Default 787 flawed

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.
  #5  
Old September 20th 07, 07:54 PM posted to rec.aviation.piloting
Bertie the Bunyip[_19_]
external usenet poster
 
Posts: 3,851
Default 787 flawed

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

  #6  
Old October 28th 07, 04:24 PM posted to rec.aviation.piloting
[email protected]
external usenet poster
 
Posts: 183
Default 787 flawed

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 !

 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
Military parts were flawed, indictment says Otis Willie Military Aviation 0 September 3rd 04 08:58 PM
Florida List for Purge of Voters Proves Flawed WalterM140 Military Aviation 2 July 10th 04 05:57 PM


All times are GMT +1. The time now is 05:52 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.