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george.mueller(at)aurora. Guest
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Posted: Tue Feb 21, 2006 10:04 am Post subject: Aux fuel pump in 701 |
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I am thinking about the fuel system in my 701 and am considering putting in
a facet fuel pump as a booster pump The pump I am considering is an
FP40105 which doesn't have a check valve and puts out 25 to 45 PSI (my
understanding is the Rotax 912 can handle a max pressure of 58psi) This
pump would be used to avoid vapor lock on take off and as an aux pump if
the mechanical pump on the Rotax fails I would install the pump after the
gascolator and after an in line fuel filter, basically next to the
gascolator Are there any problems that anyone can see with such an
installation? I am concerned with the greater likelihood of vapor lock
with auto gas
George
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frank.hinde(at)hp.com Guest
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frank.hinde(at)hp.com Guest
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bryanmmartin
Joined: 10 Jan 2006 Posts: 1018
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Posted: Tue Feb 21, 2006 11:03 am Post subject: Aux fuel pump in 701 |
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I think your numbers are off by a factor of ten. 2.5 to 4.5 psi sounds about
right for the fp40105.
If your fuel is in wing tanks, you probably won't need a booster pump
because the high wing 701 will gravity feed the fuel to the engine. But, if
you are going to put a pump in your system, it should go before the filter.
The fuel filter should be the last thing in the fuel line before the
carburetors. A clean filter might not cause a problem but if it starts to
clog up it will cause a flow restriction and the pressure will drop as fuel
flows through it. A pump can push fuel through a partially clogged filter
much better than it can suck fuel through it. Drawing suction on a fuel line
is a real good way to cause vapor lock. The lower the pressure, the lower
the boiling point. Even cars don't have filters installed ahead of the fuel
pump, just a screen in the tank to keep out larger particles that might
interfere with the pump.
This subject has been covered many times in the past on this list. You can
check the archives for previous posts on this subject.
--
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
on 2/21/06 12:56 PM, george.mueller(at)aurora.org at george.mueller(at)aurora.org
wrote:
Quote: |
I am thinking about the fuel system in my 701 and am considering putting in
a facet fuel pump as a booster pump The pump I am considering is an
FP40105 which doesn't have a check valve and puts out 25 to 45 PSI (my
understanding is the Rotax 912 can handle a max pressure of 58psi) This
pump would be used to avoid vapor lock on take off and as an aux pump if
the mechanical pump on the Rotax fails I would install the pump after the
gascolator and after an in line fuel filter, basically next to the
gascolator Are there any problems that anyone can see with such an
installation? I am concerned with the greater likelihood of vapor lock
with auto gas
George
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_________________ --
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
do not archive. |
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larry(at)macsmachine.com Guest
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Posted: Tue Feb 21, 2006 12:31 pm Post subject: Aux fuel pump in 701 |
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George,
I've been using a pair of 105s on my HDS and they are both after the
gascolator and before the
replaceable paper filter. From the filter to a T, the line branches to
the Bings. Works well, but I'd question
putting an annually replaceable filter before the pumps.
Larry McFarland - 601HDS at www.macsmachine.com
do not archive
george.mueller(at)aurora.org wrote:
Quote: |
I am thinking about the fuel system in my 701 and am considering putting in
a facet fuel pump as a booster pump The pump I am considering is an
FP40105 which doesn't have a check valve and puts out 25 to 45 PSI (my
understanding is the Rotax 912 can handle a max pressure of 58psi) This
pump would be used to avoid vapor lock on take off and as an aux pump if
the mechanical pump on the Rotax fails I would install the pump after the
gascolator and after an in line fuel filter, basically next to the
gascolator Are there any problems that anyone can see with such an
installation? I am concerned with the greater likelihood of vapor lock
with auto gas
George
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planejim(at)bellsouth.net Guest
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Posted: Thu Feb 23, 2006 7:00 am Post subject: Aux fuel pump in 701 |
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George,
I have 601Hd fuel system plumbed as you described. I use auto gas
exclusively. It has worked fine for 9 years (500.3 hours). I use the
electric pump for T/O and landing (in case of a go around) in case the
mechanical pump dies at the wrong time. The only question I have is the
pressure you mentioned. My engine driven (Rotax 912UL) pump and the
electric pump both put out around 5 Psi NOT 25 to 45 psi as you mentioned.
My elec. pump is a Facet and I don't use a "check valve" in the system. I
just checked my purchase records but the receipt doesn't mention the part
number and the airplane is miles from home. I plumbed the electric pump in
"parrallel" with the engine pump and it works fine.
Good luck.
Jim Hoak 601HD 500.3 hrs.
---
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Larry Martin
Joined: 10 Jan 2006 Posts: 31 Location: Cabot, Arkansas
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Posted: Thu Feb 23, 2006 7:24 am Post subject: Aux fuel pump in 701 |
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If you have a gravity feed system, a carbed engine, and no mechanical pump
then you should have an aux electric pump, no more than 6 psi to use for T/O
and other climbs. It is entirely possible that your carb bowl which is
normally pretty small can get higher that your tank. Thus no more gas
unless you pump it. I'm talking high wing. I intend to run a primary pump
all the time with a second backup aux pump. It's just something else not to
have to remember to turn on and off. And in the remote event the primary
pump fails, the pressure gauge will fall off but it will still gravity feed
thru the pump. I can switch on the aux pump if needed.
Larry, N1345L, www.skyhawg.com
---
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_________________ 701 with a Harley, www.skyhawg.com |
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frank.hinde(at)hp.com Guest
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Posted: Thu Feb 23, 2006 7:26 am Post subject: Aux fuel pump in 701 |
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I'm sure it does but what are the failure modes of this set up?
Is there something that could happen to the mechanical pump that
prevents the Facet from being a reliable backup?.... If the pump
diaphram were to rupture would it allow the fuel to backflow (either
back into the tank or inside the cowl)? I don't know the answer to these
questions but you can't simply write off the issue as "works fine" until
you understand how each component might fail and affect the system
performance.
Taking my scenario above for instance, a failed mechanical pump would
not only allow the engine to quit, it could also be a very big fire
hazard!
For us to recommend this setup we need to know a little more I think
Frank
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frank.hinde(at)hp.com Guest
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Posted: Thu Feb 23, 2006 7:47 am Post subject: Aux fuel pump in 701 |
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That's a wild looking cowling on that 701...Looks cool!
Not so sure I like the idea of your single pump...Do you know for sure
that you will get full fuel flow through a dead Facet fuel pump?
Why not simply run two of them in parallel. You can leave them running
all the time or turn both of them on just for TO and landing. A pair of
40105 Facets in parallel will not jack the fuel pressure any higher than
a single pump and I think there will be enough flow from each pump to
overcome the backflow thru the dead pump...If not you could always put
two check valves in or buy the pump with check valves...(model number
escapes me at present)
Nice plane!
Frank
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bryanmmartin
Joined: 10 Jan 2006 Posts: 1018
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Posted: Thu Feb 23, 2006 12:33 pm Post subject: Aux fuel pump in 701 |
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I have two Facet FP40105 pumps in parallel in my Zodiac. I only run one at a
time and have no check valves. I have never had a problem with back flow
through the inoperative pump. These pumps are designed to allow some back
flow in order to allow the line downstream of the pump to depressurize after
shut down. This back flow is just a trickle which makes check valves
unnecessary.
--
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
on 2/23/06 10:43 AM, Hinde, Frank George (Corvallis) at frank.hinde(at)hp.com
wrote:
Quote: |
<frank.hinde(at)hp.com>
That's a wild looking cowling on that 701...Looks cool!
Not so sure I like the idea of your single pump...Do you know for sure
that you will get full fuel flow through a dead Facet fuel pump?
Why not simply run two of them in parallel. You can leave them running
all the time or turn both of them on just for TO and landing. A pair of
40105 Facets in parallel will not jack the fuel pressure any higher than
a single pump and I think there will be enough flow from each pump to
overcome the backflow thru the dead pump...If not you could always put
two check valves in or buy the pump with check valves...(model number
escapes me at present)
Nice plane!
Frank
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_________________ --
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
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tshank(at)megsinet.net Guest
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Posted: Thu Feb 23, 2006 4:37 pm Post subject: Aux fuel pump in 701 |
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I don't think anyone has adequately explained the difference between the
mechanical engine pumps and the electric. The electric pumps typically
have an oscillating plunger that pumps the fuel though a pair of check
valves giving a rated pressure. If it is for example 5 psi then two
electric pumps in series is 10 psi. The engine pump operates
differently when the lever that is driven by an engine cam is moved it
pulls the diaphragm such as to enlarge the pumping chamber. This action
is against a spring. This is the intake stroke for the pump that pulls
fuel into the pump chamber. The fuel is forced out of the chamber by the
spring pressure and not the return of the pump lever which is connected
by a mechanism that does not allow it to pump on the return stroke. In
that way the spring determines the pressure of the pump not the engine
speed. In like manner if the fuel is being fed to the pump under
pressure the mechanical pump is not additive. The is the output pressure
will be which ever is higher the electric pump or the mechanical pump.
This is why for years certified low wing aircraft have had a mechanical
engine pump and a boost pump with no over pressure problem. For my
installation since I only have electric pumps I connected them in serial
with a pressure regulator to keep the pressure at 5 psi.
Tim Shankland
Jim Hoak wrote:
[quote]
George,
I have 601Hd fuel system plumbed as you described. I use auto gas
exclusively. It has worked fine for 9 years (500.3 hours). I use the
electric pump for T/O and landing (in case of a go around) in case the
mechanical pump dies at the wrong time. The only question I have is the
pressure you mentioned. My engine driven (Rotax 912UL) pump and the
electric pump both put out around 5 Psi NOT 25 to 45 psi as you mentioned.
My elec. pump is a Facet and I don't use a "check valve" in the system. I
just checked my purchase records but the receipt doesn't mention the part
number and the airplane is miles from home. I plumbed the electric pump in
"parrallel" with the engine pump and it works fine.
Good luck.
Jim Hoak 601HD 500.3 hrs.
---
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craig(at)craigandjean.com Guest
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Posted: Thu Feb 23, 2006 5:23 pm Post subject: Aux fuel pump in 701 |
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Another oft-forgotten point is that there are many models of the Facet
pumps. Some have check-valves, some have anti-siphon valves, some have
neither, some have both. There is a fairly wide variation in the range of
lift, GPH and min/max PSI. In all there are 36 different configurations in
the 12 volt models. The link below is to a PDF (Adobe Acrobat) document on
Facet's web site.
http://www.facet-purolator.com/mcl/media/technology/hd_pdfs/Cubed_Solid.pdf
Or as a tiny URL: http://tinyurl.com/nakhq
-- Craig
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vair601(at)yahoo.com Guest
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Posted: Thu Feb 23, 2006 6:12 pm Post subject: Aux fuel pump in 701 |
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Frank,
If the diaphram were to develop a hole it may exit out the weep hole however it would probably drain into the crankcase as it might still be pumping. Having a check valve seperating the two pumps, yet a good idea, but not required to have the system function. After all there is a check valve built into the mechanical pump to begin with or it couldn't pump. Just my two cents worth.
Bill Jeffries
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