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Master Switch/Contactor and Starter Questions

 
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nuckolls.bob(at)aeroelect
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PostPosted: Sun Jun 30, 2013 12:23 pm    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

At 11:07 AM 6/30/2013, you wrote:
Quote:

<dgaldrich(at)embarqmail.com>

Hi Robert et al.

Two issues to discuss

Under what circumstances could you recommend/condone the use of a
simple mechanical master switch (as in Z-17) rather than a
traditional battery contactor?

It needs to serve the same purpose as any other form
of battery master . . . offer the pilot direct control
of the battery by means located as close as possible to\
the battery . . . generally less than 1 foot. EVERY OBAM
aircraft could use a manual master switch as long as it
was in convenient reach of the pilot.

Quote:
I am building an aircraft with very similar loads to Z-17 but will
have an 18 amp dynamo/PMG and an Odyssey 680 battery so I guess the
real question is, do those two items change the ability to use a
switch versus the additional complexity and "hold" current usage of
a contactor?

You CAN purchase a low-hold current contactor . . . but
have you done a load analysis? What are your full up
running loads?

Quote:
Second issue is wiring the starter. Mine has two separate
terminals. One for the serious current and one for the
solenoid. I'm planning to wire the battery directly to the starter
with #2AWG cable and use #16AWG from the solenoid to the start
switch and back through a 5 or 10 amp CB. All of the Z- diagrams
show a start contactor so I'm wondering if my planning passes the "idiot" test.

It's not generally done that way . . . opening the
battery master is supposed to take the system max-cold.
This would include fat wires to the starter.
What kind of airplane/engine combination are we discussing?
Do you have night lighting? What drove your decision for the
680 as opposed to a smaller battery?


Bob . . .


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nuckolls.bob(at)aeroelect
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PostPosted: Sun Jun 30, 2013 8:38 pm    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

Quote:


The entire experimental aircraft can be built without contactors,
and I think it's a good approach.

I took dual instruction in a TriPacer back in '61 that
mounted the battery under the pax seat. The battery master
was a switch that you could reach under the seats between
pilot and co-pilot. The starter was a manual push button
in a similar position between the pilot's knees.

A contactor is not required . . . just a battery master
disconnect. If you can acquire manual switches suited to
the task and they can be mounted for convenient access
the choice is yours.

Bob . . .


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dgaldrich



Joined: 24 Apr 2009
Posts: 267
Location: Naples, Fl and Belfast, ME

PostPosted: Mon Jul 01, 2013 1:30 pm    Post subject: Re: Master Switch/Contactor and Starter Questions Reply with quote

Based on everyone's inputs and logic, I will use a normal aircraft style contactor for the battery. The aircraft is a Pietenpol with a Corvair engine and my arms are not long enough to reach the battery in the engine compartment from the rear cockpit. I would be interested in a low current one if it could handle the starter current when closed.

The aircraft will have LED lights/strobes, Microair radio and transponder, individual electric instruments, and conventional ignition. No landing light or heated pitot. I'm figuring a maximum of 10 amps so the dynamo has enough output to "hold" a contactor in addition to the normal load. The 680 battery was chosen for no better reason than it works in motorcycles and ATVs. Would love to use something lighter if it will turn over the engine reliably. I am not primarily concerned with a long endurance capability. Any kind of electrical issue, or mechanical for that matter, is a land at the nearest suitable field signal and I fly on the east coast where 30 minutes of battery power will generally get you on the ground, even at Pietenpol airspeeds.

The Corvair uses a Subaru starter which has an almost zero weld closed failure rate so I'm still thinking of running a large wire from the battery contactor to the big lug on the starter and using the starter solenoid as an independent way to turn the engine over. Two less junctions in the high current path.

Thanks Bob and others for the information and advice.

Dave


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nuckolls.bob(at)aeroelect
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PostPosted: Tue Jul 02, 2013 9:45 am    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

At 04:30 PM 7/1/2013, you wrote:
Quote:

<dgaldrich(at)embarqmail.com>

Based on everyone's inputs and logic, I will use a normal aircraft
style contactor for the battery. The aircraft is a Pietenpol with a
Corvair engine and my arms are not long enough to reach the battery
in the engine compartment from the rear cockpit. I would be
interested in a low current one if it could handle the starter
current when closed.

It's easy to craft a contactor-coil-current-manager.
See:

http://tinyurl.com/bolkoyc

Contactors like the EV series from Tyco will
do something similar . . . although probably
in a micro-cotroller.

Quote:
The aircraft will have LED lights/strobes, Microair radio and
transponder, individual electric instruments, and conventional
ignition. No landing light or heated pitot. I'm figuring a maximum
of 10 amps so the dynamo has enough output to "hold" a contactor in
addition to the normal load.

Okay, you're not 'hurting' for energy under
normal conditions. A e-bus alternate feed path
that bypasses the contactor could be crafted for
your panel bus.

Quote:
The 680 battery was chosen for no better reason than it works in
motorcycles and ATVs. Would love to use something lighter if it
will turn over the engine reliably.

The 680 will crank an IO720 . . . there are many
batteries will crank the Corvair engine.
Quote:
I am not primarily concerned with a long endurance
capability. Any kind of electrical issue, or mechanical for that
matter, is a land at the nearest suitable field signal and I fly on
the east coast where 30 minutes of battery power will generally get
you on the ground, even at Pietenpol airspeeds.

Do you plan to carry a hand-held?

Quote:
The Corvair uses a Subaru starter which has an almost zero weld
closed failure rate so I'm still thinking of running a large wire
from the battery contactor to the big lug on the starter and using
the starter solenoid as an independent way to turn the engine
over. Two less junctions in the high current path.

Your cranking path stresses are no worse and probably
much less than those for tens of thousands of single
engine airplanes. Modifications to the legacy
battery/battery-contactor/starter-contactor/starter
configuration has no calculable return on investement.
Bob . . .


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nuckolls.bob(at)aeroelect
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PostPosted: Thu Jul 04, 2013 5:20 am    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

At 07:13 PM 7/3/2013, you wrote:
Quote:
--> AeroElectric-List message posted by: "dgaldrich" <dgaldrich(at)embarqmail.com>

I agree. It seems pointless to have 2 solenoids operating at the same time. The other issue is that I believe the Subaru solenoid moves the gear before the contactor part puts juice to the motor brushes. An aircraft type contactor would do both at the same time rather than sequentially. Have not dismantled one so I may be in error.

None of applications of an external contactor
proposed for modern starters "bypasses" functionality
of the built in solenoid/contactor. The
starter's built in solenoids do engage the pinion
gear before closing electrical connection for
the starter motor.

Variants to select from when using these modern
starters causes the builder to decide whether
the built in contactor is energized by the panel
mounted, START switch -OR- energized through a more
robust device.

There is a problem to be solved when the panel
mounted starter control is used to energize the
starter's built in contactor. Unlike legacy
'starter solenoids' controlling starters with
Bendix drives, the modern pinion engagement
solenoids have a very high coil current demand
during the first few milliseconds of being
energized. See: http://tinyurl.com/op5cs2g

Failure to recognize this difference in
solenoid/contator performance caused a
kerfuffle over burned start switch contacts
on the ACS-510 key swicch (clone of legacy
Bendix/Gerdes). ACS now sells a diode with two
terminals applied.

[img]cid:.0[/img]




A critical need to install this diode across the
starter contactor engagement coil arose from the
alarming rate at which start contacts in the key
switch were destroyed by overstress when the legacy
starter/external contactor combo was replaced with
a light weight version with combination solenoid/
contactors. Many cars suffered similar failure modes
in their key-start switches.

SB92-01 from ACS originally place thier diode across
the switch contacts . . . wrong place. It was corrected
in a subsequent revision. See http://tinyurl.com/nva2xdy

B&C adopted the philosophy of jumpering the starter
solenoid coil right to the fat-wire terminal on
the starter . . . and controlling power to the
starter though a modern, starter contactor WITH
built in coil suppression diode. The external contactor's
inrush demands on the start switch are a small fraction
of that for direct control.

This philosophy posed a new problem when PM motor
starters began to show up on the airplane. PM motors
have a pronounced counter-emf during spin-down after
the power is removed. This would delay disengagement
of the pinion gear and was commonly called "starter
run on" . . . in fact it was better called "delayed
disengagement".

Starters with wound fields (B&C and some others)
do not suffer this indignity and function well with
the engagement solenoid jumpered directly to the
starter's fat-wire terminal.

In ANY case, the builder's design goals should
include providing a source of solenoid engagement
power that (1) is supplied through a low impedance
source (short and fatter than usual wires) and
(2) avoid running this power through the panel
mounted start switch.

If the starter is a PM version, the builder can
take advantage of the "I" terminal on many modern
starter cotactors and use it to SUPPLY current
to the engagement solenoid. This provides for
instant removal of coil power when the starter
switch is opened and prevents 'delayed disengagement'.

In this case, the builder would do well to have
diode coil suppression on BOTH the external contactor
coil AND the solenoid/contactor coil on the
starter.

Bob . . .


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nuckolls.bob(at)aeroelect
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PostPosted: Fri Jul 05, 2013 11:25 am    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

At 01:28 PM 7/5/2013, you wrote:
Quote:
--> AeroElectric-List message posted by: Ed <decaclops(at)gmail.com>

So....on the SkyTec permanent magnet starter, the diode goes from the little terminal to where - ground on the starter case?

Same for ALL starters with the built in solenoid/contactor.

[img]cid:.0[/img]


.... or like this

[img]cid:.1[/img]



Quote:
By the way, I only measure approximately .3 ohms from the small terminal to the starter case. I thought the coil would have more resistance than that. The starter comes from SkyTec with a jumper from small terminal to the fat wire terminal.

Yup, that resistance to ground is LOW . . . it gets higher
after the pinion gear extends but the initial current
draw is significant. That's why you use external contactors
or a buffer relay as shown above . . .

I've added diodes to Z22 . . . something I should
have done years ago. Thanks for reminding me.


Bob . . .


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nuckolls.bob(at)aeroelect
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PostPosted: Fri Jul 05, 2013 11:29 am    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

At 01:58 PM 7/5/2013, you wrote:
Quote:


Ed,

Do you get the same resistance reading in both directions? What if
you swap your meter leads? If there's an internal snubbing diode
there, you'll get a really low resistance reading in the direction
the diode conducts in and you'll read the coil resistance with the
meter leads swapped the other way around.

.3 ohms at 14V would pull about 47 amps. Probably more than your
starter switch can handle. I'm thinking it should be like 30 ohms or more.

Bill

40 amps . . . yeah that's about right.
See:

http://tinyurl.com/op5cs2g

Bob . . .


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PostPosted: Sat Jul 06, 2013 5:13 am    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

At 11:54 PM 7/5/2013, you wrote:
Quote:
--> AeroElectric-List message posted by: Ed <decaclops(at)gmail.com>

I knew on some level that low ohms means high current. That's why I questioned it, but I didn't do the math. 35 amps is a bunch! I'm not planning to throw away my starter contactor anytime soon. I did measure the coil both directions and it is the same.

Which starter contactor are we talking about?
One built onto a starter or an external contactor?

When you mentioned 0.3 ohms, the first image in
my head was for a contactor built onto a starter.
These DO present a very low terminal resistance in the
de-energized mode. There's mechanism inside that
demands a ~30A closure current and a more moderate,
~10A holding current. . .

Run of the mill external contactors

http://tinyurl.com/kqphmh

. . . have no such shift in demand and will require
~5A to close and hold the contacts. Further, the models
sold previously by us and now by B&C have built
in coil suppression diodes.

Be wary of low resistance measurements with the
garden variety multimeter. They're not designed
to 'wash out' the effects of lead length and their
excitation current to a device under test is
too low to offer useful resolution of low resistance
measurements.

This limitation is what prompted the design of a
4-wire low resistance measurements adapter. This
was published in a Beech shop notes bulletin some
years back. We had a rash of unnecessary replacement
of landing gear down-lock indicator switches on
fielded aircraft. This was traced to the quality
of contact resistance measurements using the
garden variety multi-meter. The task demanded
instrumentation better suited to the task.

http://tinyurl.com/4l3tuj6

A few years later I crafted this product based
on the earlier article . . .

http://tinyurl.com/6g9e7vm

The value of this technique for low resistance
measurement is described in the Grounding
chapter of the 'Connection. The same technique
is useful for getting meaningful data on coil
and contact resistance of the more robust components
in the ship's electrical system.



Bob . . . [quote][b]


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PostPosted: Sat Jul 06, 2013 8:38 pm    Post subject: Master Switch/Contactor and Starter Questions Reply with quote

Quote:


Speaking of diodes, is this overkill?
http://www.amazon.com/Amico-Molded-Plastic-Rectifier-Diodes/dp/B009IN1KB8/ref=sr_1_6?ie=UTF8&qid=1373088088&sr=8-6&keywords=diodes

I can get these, but the shipping is more than the diodes:
http://www.digikey.com/scripts/DKSearch/dksus.dll?Detail&itemSeq=133108363&uq=635086673453750862

I like the 1N5400 series devices which are stocked
by Radio Shack

http://tinyurl.com/pfwlz2v

and Jameco

http://tinyurl.com/qjefqzq

if you don't mind paying for 0.08 each in
packs of 30. They use first class parcel
for small orders . . . these would come to
your door for under $2.

The 1N5400 has reasonably robust leads and
package. Smaller diodes work too but these
are mechanically user friendly, easy to get
and the price is right.

Any P/N in the 1N540x series is okay from 0 to 9


Bob . . . [quote][b]


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