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RV-List Digest Archive
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Total Messages Posted Tue 02/06/07: 50
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Today's Message Index:
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1. 05:41 AM - Re: Re: I've sworn off purge valve installations (Stewart, Michael (ISS Atlanta))
2. 06:26 AM - Re: Aircraft Spruce update (n801bh@netzero.com)
3. 06:44 AM - How do you like your engine monitor? (Bob Collins)
4. 06:57 AM - Re: Re: pilot's family awarded $10.5M (n801bh@netzero.com)
5. 07:15 AM - Re: Re: RVAtor Article Needed (Brian Meyette)
6. 07:18 AM - Re: Off Topic: GPS for Cars (Dan Checkoway)
7. 07:19 AM - Re: Re: pilot's family awarded $10.5M (Bob Collins)
8. 07:25 AM - Re: Off Topic: GPS for Cars (Lockamy, Jack L)
9. 07:28 AM - Re: Re: pilot's family awarded $10.5M (Ron Lee)
10. 07:37 AM - Re: Re: I've sworn off purge valve installations (Gerry Filby)
11. 07:42 AM - Re: RVAtor Article Needed (Bob Collins)
12. 07:44 AM - Re: Re: pilot's family awarded $10.5M (Bob Collins)
13. 07:44 AM - Re: Re: RVAtor Article Needed (Bob Collins)
14. 08:17 AM - Re: Re: pilot's family awarded $10.5M (Dale Ensing)
15. 08:20 AM - Re: Off Topic: GPS for Cars (Dale Ensing)
16. 08:23 AM - Re: Re: I've sworn off purge valve installations (Dan Checkoway)
17. 08:30 AM - 3.7 lb, 600 cranking amp, 11.5 A-hr battery (Bill Dube)
18. 08:31 AM - Exactly why we publish 24 Years of the RVator (Andy Gold)
19. 09:11 AM - Re: RVAtor Article Needed (Brian Meyette)
20. 09:15 AM - Re: Off Topic: GPS for Cars (Terry Watson)
21. 10:02 AM - Re: Re: I've sworn off purge valve installations (Gerry Filby)
22. 10:45 AM - Re: RV-List Digest: 21 Msgs - 02/05/07 (Nick Gaglia)
23. 10:45 AM - Re: RV-List Digest: 21 Msgs - 02/05/07 (Nick Gaglia)
24. 10:54 AM - Re: Off Topic: GPS for Cars (Ron Lee)
25. 11:14 AM - Re: 3.7 lb, 600 cranking amp, 11.5 A-hr battery (Jim Sears)
26. 11:18 AM - Re: Aircraft Spruce update (Aircraft Spruce Info)
27. 11:46 AM - Re: I've sworn off purge valve installations (Don)
28. 11:59 AM - Re: Re: RVAtor Article Needed (Brian Meyette)
29. 12:11 PM - Re: Off Topic: GPS for Cars (Tedd McHenry)
30. 12:11 PM - ground GPS (JOHN STARN)
31. 12:26 PM - Re: 3.7 lb, 600 cranking amp, 11.5 A-hr battery (Bill Dube)
32. 12:32 PM - Re: Re: I've sworn off purge valve installations (Konrad L. Werner)
33. 12:33 PM - Re: 3.7 lb, 600 cranking amp, 11.5 A-hr battery (Bill Dube)
34. 12:38 PM - Re: Re: Aircraft Spruce update (Tim Bryan)
35. 01:17 PM - RvAtor Article Needed (John Fasching)
36. 01:32 PM - Re: Re: I've sworn off purge valve installations (RV Builder (Michael Sausen))
37. 01:33 PM - Re: Re: Aircraft Spruce update (Joseph Larson)
38. 01:42 PM - Re: Re: Aircraft Spruce update (Brian Meyette)
39. 02:10 PM - Re: Re: Aircraft Spruce update (RV Builder (Michael Sausen))
40. 02:28 PM - Re: Re: Aircraft Spruce update (Bruce Gray)
41. 02:59 PM - Re: Re: Aircraft Spruce update (Tim Bryan)
42. 03:02 PM - Fuel Injection (Wheeler North)
43. 03:20 PM - Re: Re: Aircraft Spruce update (Kyle Boatright)
44. 03:38 PM - Re: Re: Aircraft Spruce update (Kevin Horton)
45. 03:54 PM - Re: Re: JPI was Aircraft Spruce update (Tim Bryan)
46. 04:58 PM - Re: pilot's family awarded $10.5M (Bob Collins)
47. 06:37 PM - Re: Off Topic: GPS for Cars (Dave B)
48. 09:15 PM - Re: Re: Aircraft Spruce update (Steven DiNieri)
49. 09:35 PM - Re: Re: Aircraft Spruce update (Konrad L. Werner)
50. 10:27 PM - Aircraft Spruce Experience (Paul Trotter)
________________________________ Message 1 _____________________________________
Time: 05:41:12 AM PST US
Subject: RE: RV-List: Re: I've sworn off purge valve installations
From: "Stewart, Michael (ISS Atlanta)"
Hmm. Spout off? Sensationalize? That's interesting. I have been bringing
my experience to the table in an effort to educate the users. Yes, I did
not safety wire the screws, neither did the off field failure. I have
received 2 listers off messages that they read these posts and also
found their screws now safety wired. Im not here to spout off. Im here
to learn, engage in useful dialogue, and educate where I can based on my
experience.
Im not an AFP basher. Dons a bright guy with an excellent product, one
that I use on my plane.
I would respectfully recommend that he find a way to ship the valve with
the screws safety'd already, like the rest of his system. The flow
divider and fuel servo both come all wired up and ready to bolt on, but
not the purge valve. Leaving this up to the installer can lead to a
failure to do so. With many things on an airplane, this cant be avoided.
But with this purge valve, I think it can be done simply. How many
accidents do we need before it changes from dumb user error, to design
change? Giving the user a chance to fail, where it can be avoided, does
not sound like good practice.
Just my 2 cents.
Best,
Mie
-----Original Message-----
From: owner-rv-list-server@matronics.com
[mailto:owner-rv-list-server@matronics.com] On Behalf Of Dan Checkoway
Sent: Monday, February 05, 2007 7:25 PM
Subject: Re: RV-List: Re: I've sworn off purge valve installations
RV listers,
Don Rivera from Airflow Performance (AFP) responded off-list to my
previous
inquiry, asking about the rationale for having a designed-in ICO leak.
I
don't know too many manufacturers who take the time to address concerns
&
questions in such detail. What follows is his response. I have his
permission to post it where required, and I felt this forum would
benefit
from this in-depth explanation of the design's history.
======= BEGIN Don's Response ======
Dan,
It saddens me to hear of incidents let alone ones that are strictly the
cause of poor judgment, practice, attention; you know what I mean. It
seems
that Michael Stewart has his opinion and that's fine, but to spout off
like
he does, is kind of up setting, as he seems to sensationalize events
that
are strictly in his control.
You had made comment that you wanted to know more about the mixture
control
valve design. To completely understand the reasoning behind this design
you
have to know a little history of how this all got started. When we
started
our company in 1984 I had already 10 years experience with aircraft fuel
injection systems at the Bendix Corporation. Being the under study of
the
inventor of the RS and RSA fuel injection system and later being the
project
engineer on that product line gave me insight into the manufacturing
problems and cost associated the RSA design. In Airflow's infancy, we
knew
that we would have to design a system to satisfy a large range of
horsepower
requirements with a minimum of part and tooling changes. Knowing that
we
wanted to be able to run engines from around 80 HP to 1000 HP we
designed
the present fuel regulator concept.
Studying the needs in the aviation field we constantly heard of the big
draw
back to fuel injection was 1) initial cost, 2) hot starts, 3) high cost
of
overhaul. In this design we determined that eliminating part count
without
sacrificing performance would help with manufacturing costs, and
overhaul
cost.
Studying various manufacturing techniques, we knew that plate valves
were
expensive to make (high part count) were susceptible to scoring unless
you
used some expensive materials and there's always the issue of making the
parts flat (specialized equipment). Rotary valves on the other hand
were
easy to control in manufacture (OD grinding) and round bores were easy
to
control with honing. This would allow parts that would not have to be
hand
lapped or fitted. The round parts could be made with tight enough
tolerances that matched parts were not necessary. Having a through bore
that both idle and mixture valves ran in gave the bonus of getting cost
out
of manufacturing as through bore honing would hold the bore straight and
we
could easily hold + .0005" on the entire bore. Brass was chosen as the
material to run in an anodized honed bore. Designing the L/D of the
valve
gave excellent bearing surface and I have to admit, we really haven't
had
any problems with wear or scoring of these parts in 20+ years of
service.
The only down side is continued actuation of the parts when dry can
cause
galling of the valve. This is solved by oil flushing the parts after
test,
and in service the parts are always in fuel. Of course with a rotary
valve
there has to be clearance for the valve to rotate, therefore ICO cannot
be 0
leak. We also only shut off the metered side of the circuit in the
regulator. This removed the additional parts required to mechanize an
additional valve to shut off this side of the circuit and since the
decision
was made to use the purge valve as standard equipment, a zero leak
mixture
valve was not required.
Hot starts were a common problem with low-pressure non-returning fuel
injection systems, and even some early mechanical automotive fuel
injection
like the Bosch K Jetronic suffered from this problem. We determined
that
the hot start problem was due to heat soak on the fuel system components
on
the engine. Since fuel boiled at around 130 degrees F at sea level
pressure, after the engine shut down the fuel on the engine side of the
fire
wall in the hoses, engine driven fuel pump, fuel control, flow divider,
and
nozzle lines would be partially boiled away. Since the fuel metering
system
was non-returning, there was no way to get rid of the hot fuel and
vapor.
You had to start the engine flooded or when the engine started you had
to
run it up excessively to pass the vapor through the metering system to
keep
the engine running. Some people didn't have problems with this
technique,
many did. The components that held the most volume of fuel were the
culprits. The #6 fuel hoses, the engine driven fuel pump and the fuel
control. Since our metering system metered fuel to the engine based on
engine airflow consumption there was a limit on how fast fuel would
transfer
through the system when the engine was not running. On a typical 4
cylinder
Lycoming the normal calibration set up allowed about 1 cup of fuel to
transfer through the system in 45 seconds of purging with the throttle
wide
open. This would pretty much exchange the fuel in the engine driven
fuel
pump and the fuel control and hoses. At idle the fuel transfer would be
.038 cup of fuel in one minute. This is why idling the engine will
never
get the air out of the system, well at least not for 26 minutes. This
is
another reason we want to minimize the volume of fuel on the engine side
of
the firewall.
The purge valve was designed on the premise that cleaning out the hot
fuel
and vapor from the engine driven pump, fuel control and hoses would cure
the
hot start problem. The first system was installed on an IGSO 480 in an
aerobatic airplane, which was pretty much unstartable when hot. The
system
worked quite well with pretty much the same start routine hot or cold.
Also
the benefit with the purge valve was that it would dump the fuel
pressure
when the engine was shut off to keep fuel from bleeding into the engine
after shut down. This was a problem with engines using diaphragm fuel
pumps. We always had complaints of fuel dripping into the air box after
shut down on Bendix servos which basically dead head the fuel pump
pressure
against a plate valve. When the plate valve scored a little leakage
started
and the engine would not shut down clean. People whine and moan about
this
now, but 30 years ago when I was working at Bendix we heard the same
thing.
Thus, another reason for the design of the purge valve.
The purge valve design was not something we designed from scratch with a
fresh sheet of paper. The basic valve design was studied as to what
design
in the field gave the most trouble free service. Looking at helicopter
service, we found that that seemed to get the most abuse. From both a
vibration and wear stand point this installation typically had fuel
tanks
above the engine so the valve had to be near zero leak as possible, yet
be
robust enough to withstand the harsh environment it was in. So the
valve
bushing was used from a RSA-7 fuel regulator. This same design had been
used on all Hughes 300 and Beechcraft Baron 58P installations. With a
few
million flight hours accumulated, there had been not one incident of
malfunction of the valve, let alone the screw backing out because it was
not
lockwired. The idle valve bushing on these fuel servos had the same
design,
that is, being held in by one screw. Thus the Airflow purge valve was
designed to mimic the Bendix design, with some minor changes in the
venting
of the ports in the bushing, and of course a housing was designed to
hold
the valve.
So there you have it. A history and reasoning behind the mixture
control
and purge valve design. This design was done to satisfy requirements
that
we determined customers wanted in the field. After all, if the status
quo
was accepted, why build anything? It would not address any of the
issues
that existed, and you would end up with a clone of the same 40-year-old
design. Kind of like a Silver Hawk. All of these parts were designed
for a
reason and with lot of forethought. Are there other ways to do it? You
bet. Is there a better cost effective way to address the problems
associated with low-pressure non-returning fuel injection systems?
Probably
not, with the market as it is today.
======= END Don's Response ======
________________________________ Message 2 _____________________________________
Time: 06:26:46 AM PST US
From: "n801bh@netzero.com"
Subject: Re: RV-List: Aircraft Spruce update
Well, I was wrong when I said that Jim Irwin would not follow through an
d investigate my problem with ACS. He did and contacted me with this "
Ben: Thanks for your quick reply and your understanding. I am sure that
the lack of the return tag was simply an oversight by whoever handled t
his matter 3 years ago. All of our staff is very busy on a day to day ba
sis and they probably just forgot to do the last step in the process, wh
ich was to be sure to get the "short" tubing picked up. If you were char
ged for the replacement tubing but never credited for the first shipment
(because it was not returned), please let me know the approximate amount
of the replacement invoice so we can reimburse you. I appreciate your
kind words and am sorry that we could not get this resolved years ago. T
hanks in advance for letting the RV readers know that we have discussed
the problem. I hope that we can be of service to you sometime soon. Let
me know what the cost was on that tubing! Best Regards, Jim IrwinAircraf
t Spruce
///////////////////////////////////////////
This the good ol ACS I rememeber when I first started my project. I hope
it stays this way because I need ALOT of 4130 tubing and other stuff fo
r the firewall forward packages I am about to selling. The Murphy Moose
and the Bearcat kits are first. I don't even want to start on the RV-10
customers yet, those will outsell the others by 5-1.
Thanks Jim for your leg work in correcting my bad experience with ACS.
Ben Haas
N801BH
www.haaspowerair.com
Any questions? Get answers on any topic at www.Answers.yahoo.com. Try i
t now.
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Well, I was wrong when I said that Jim Irwin would not follow t
hrough and investigate my problem with ACS. He did and contacted me with
this "
|
|
Ben:
Thanks for your quick reply and your un
derstanding. I am sure that the lack of the return tag was simply an ove
rsight by whoever handled this matter 3 years ago. All of our staff is v
ery busy on a day to day basis and they probably just forgot to do the l
ast step in the process, which was to be sure to get the "short" tubing
picked up. If you were charged for the replacement tubing but never cred
ited for the first shipment(because it was not returned), please let me
know the approximate amount of the replacement invoice so we can reimbur
se you.
I appreciate your kind words and am sor
ry that we could not get this resolved years ago. Thanks in advance for
letting the RV readers know that we have discussed the problem. I hope t
hat we can be of service to you sometime soon.
Let me know what the cost was on that t
ubing!
Best Regards,
Jim Irwin
Aircraft Spruce | <
/TBODY> |
///////////////////////////////////////////
This the good ol ACS I rememeber when I first started my project. I h
ope it stays this way because I need ALOT of 4130 tubing and other stuff
for the firewall forward packages I am about to selling. The Murphy Moo
se and the Bearcat kits are first. I don't even want to start on the RV-
10 customers yet, those will outsell the others by 5-1.
Thanks Jim for your leg work in correcting my bad experience wi
th ACS.
Ben Haas
N801BH
www.haaspowerair.com&nbs
p;
Any questions? Get answers on any to
pic at www.Answers.yahoo.com. Try it now.
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