In a message dated 1/1/2006 9:54:03 P.M. Central Standard Time,
RWolf99@aol.com writes:
Actually, it is much, much worse. Not on orbit, of course, but on
the rocket ride up there. I have witnessed vibration testing to the
spectrum which these things are qualified -- it makes our prehistoric
4-bangers seem as smooth as turbines.
and
In a message dated 1/1/2006 9:53:52 P.M. Central Standard Time,
elippse@sbcglobal.net writes:
You should have seen the vibration spectrum we had to put our GE
guidance transponders through to qual them for the Atlas. If my little 235
shook that way, I would have shut it down so fast it would have made your
head spin! I've seen that shake table demolish vibration isolators like they
were made from Jello!
Rob and Paul,
OK, let's not cause undue concern amongst the builders. It is
unnecessary to overbuild things.
When considering any system in our powered lawn darts, the first of
many tests is "can it withstand constant vibration?" These
aircraft are not rocket ships that spend most of their time collecting
cosmic rays and meteorite dust in a vacuum (no, not in a Dyson).
Constant vibration that begins after engine start and doesn't cease until
shutdown. Every flight hour until TBO is spent vibrating. I've
had an incompletely closed BNC connector vibrate apart (7 flight
hours), a poorly supported unimportant solder joint shake and break (500
flight hours) and the alternator B-lead crimp connection work harden
the wire and break at the crimp because of a poor support choice (8 flight
hours).
I have many Fastons (switches, power buses, ground buses) - none have
failed so far in over 700 flight hours. I have a large number of Molex
connectors - none have failed so far. I have all kinds of terminals, plugs
and pins that are crimped without solder - none have failed so far. I
have large numbers of d-subs connecting autopilot parts, Garmin 430,
radios, etc. - no failures so far. I have utilized more tie-wraps than I
can count to make sure wires are supported so that vibration effects are held to
a minimum.
I have two d-sub connectors that almost failed because of thoughtless
design and cheap components - Magneto accessory case LSE timing
hall sensor connectors worked loose in less than 20 flight hours. Why,
because LSE decided to hard mount the d-sub receptacles to the sensor box,
unlike LASAR that has its' connectors located at the end of a pigtail so
that the connection can be located to minimize vibration. The problem
has been handled by using better connectors and safetying the locking
screws.
You don't need rocket ship connectors that handle the big rumble when all
that is needed is to be aware of the constant buzz and deal with it.
Scott Krueger
AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL
(KARR)