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Reversible electric motors and CBs

 
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raymondj(at)frontiernet.n
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PostPosted: Thu Jan 07, 2010 7:37 am    Post subject: Reversible electric motors and CBs Reply with quote

Just thinking, would there be any value in having CBs on reversible
motors. I'm considering: flap motors; trim motors; gear motors;
variable pitch electric propellers. Perhaps being able to move the
motor in the other direction might have some value or trying again after
a mistake like deploying at too high a speed or in a condition where ice
might have caused an overload. I recognize the low probability of these
things occurring but thought they deserved mentioning in the current
discussion.

Raymond Julian
Kettle River, MN


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nuckolls.bob(at)aeroelect
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PostPosted: Thu Jan 07, 2010 8:03 am    Post subject: Reversible electric motors and CBs Reply with quote

At 09:21 AM 1/7/2010, you wrote:
Quote:


Just thinking, would there be any value in having CBs on reversible
motors. I'm considering: flap motors; trim motors; gear motors;
variable pitch electric propellers. Perhaps being able to move the
motor in the other direction might have some value or trying again
after a mistake like deploying at too high a speed or in a condition
where ice might have caused an overload. I recognize the low
probability of these things occurring but thought they deserved
mentioning in the current discussion.

Careful my friend, you'll be accused of doing
FMEA . . . it's addictive.

What you've hypothesized is a potential for
nuisance tripping the circuit protection in
non-normal or extra-ordinary operations.

My sense is that there are very few motors
at risk for jamming due to environmental
conditions. Flaps and trim surfaces are away
from ice-accretion spots. Ice might gather
close to the hub of a prop blade but those
motors tend to be highly geared and capable
of producing much more torque than is necessary
to move the blades. I think virtually all
OBAM aircraft with retractable gear use hydraulics
where the motor is not subject to "overload" . . .
pressure relief valves generally address that
issue. Further, large demand devices like
motor driven hydraulics are protected with very
robust protection devices like current limiters.

Extending flaps against cruise speed air-loads
MIGHT be a case where you could pop a fuse . . .
but loads on most flap systems start out low
and ramp up as the flap extends into the
wind. Behavior of the airplane during the first
few degrees of extension would no doubt get
the pilot's attention long before current
demands by the motor put a fuse at risk.

But one can always UP-size a fuse and feeder
to the flap system. PM motors draw so much
current in a stalled state that if you doubled
the size of the fuse (very fast) to accommodate
some perceived transient overload condition
you would not put the motor at risk for other
fault conditions.

That brings up another thought. We know that
unlike breakers, fuses are subject to "wearing"
caused by short term operations at or just above
the fuse's ratings. So if your flap system normally
calls for a 5 or 7A breaker, you would be on
solid ground for upsizing to 10A.

The goal is to provide a solid, trip free
source of power. PM motor inrush currents
are spectacular. Breakers are much slower
than fuses and are pure I(squared)*R sensors.
Fuses can slowly degrade over time when
hit repeatedly with transient "overloads".

Good thoughts . . .

Bob . . .


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mrspudandcompany(at)veriz
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PostPosted: Thu Jan 07, 2010 9:17 am    Post subject: Reversible electric motors and CBs Reply with quote

I think virtually all
OBAM aircraft with retractable gear use hydraulics
where the motor is not subject to "overload" . . .
pressure relief valves generally address that
issue. Further, large demand devices like
motor driven hydraulics are protected with very
robust protection devices like current limiters.
The Falco, which I am building, is one OBAM aircraft which uses a motor and
jack screws to deploy the LG. There have been many complaints of the
breaker popping when raising the gear. Some owners have set the limit
switches so the gear does not retract fully, and finish the last little bit
of retraction with the hand crank. I believe there is a fundamental design
flaw in the retract mechanism, but have not seen a good fix.

Roger


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raymondj(at)frontiernet.n
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PostPosted: Thu Jan 07, 2010 9:50 am    Post subject: Reversible electric motors and CBs Reply with quote

I always apply a probability to an adverse event, even if it is a WAG
just to help keep my perspective. You're right, it can be addictive.

Raymond Julian
Kettle River, MN.
Robert L. Nuckolls, III wrote:
Quote:

<nuckolls.bob(at)aeroelectric.com>

At 09:21 AM 1/7/2010, you wrote:
>
>
> Just thinking, would there be any value in having CBs on reversible
> motors. I'm considering: flap motors; trim motors; gear motors;
> variable pitch electric propellers. Perhaps being able to move the
> motor in the other direction might have some value or trying again
> after a mistake like deploying at too high a speed or in a condition
> where ice might have caused an overload. I recognize the low
> probability of these things occurring but thought they deserved
> mentioning in the current discussion.

Careful my friend, you'll be accused of doing
FMEA . . . it's addictive.

What you've hypothesized is a potential for
nuisance tripping the circuit protection in
non-normal or extra-ordinary operations.

My sense is that there are very few motors
at risk for jamming due to environmental
conditions. Flaps and trim surfaces are away
from ice-accretion spots. Ice might gather
close to the hub of a prop blade but those
motors tend to be highly geared and capable
of producing much more torque than is necessary
to move the blades. I think virtually all
OBAM aircraft with retractable gear use hydraulics
where the motor is not subject to "overload" . . .
pressure relief valves generally address that
issue. Further, large demand devices like
motor driven hydraulics are protected with very
robust protection devices like current limiters.

Extending flaps against cruise speed air-loads
MIGHT be a case where you could pop a fuse . . .
but loads on most flap systems start out low
and ramp up as the flap extends into the
wind. Behavior of the airplane during the first
few degrees of extension would no doubt get
the pilot's attention long before current
demands by the motor put a fuse at risk.

But one can always UP-size a fuse and feeder
to the flap system. PM motors draw so much
current in a stalled state that if you doubled
the size of the fuse (very fast) to accommodate
some perceived transient overload condition
you would not put the motor at risk for other
fault conditions.

That brings up another thought. We know that
unlike breakers, fuses are subject to "wearing"
caused by short term operations at or just above
the fuse's ratings. So if your flap system normally
calls for a 5 or 7A breaker, you would be on
solid ground for upsizing to 10A.

The goal is to provide a solid, trip free
source of power. PM motor inrush currents
are spectacular. Breakers are much slower
than fuses and are pure I(squared)*R sensors.
Fuses can slowly degrade over time when
hit repeatedly with transient "overloads".

Good thoughts . . .

Bob . . .







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jay(at)horriblehyde.com
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PostPosted: Thu Jan 07, 2010 10:15 am    Post subject: Reversible electric motors and CBs Reply with quote

This is an area that I have used to 'placate' one of my clients whose
aircraft I am building. He really wants to see breakers but I talked him
around to fuses and non-inflight changeable ones at that... But, to get him
to accept that I agreed that the hydraulic pump might 'overload' and hence
you might want to reset that breaker, so we put in a breaker for that
circuit and fuses for everything else. It's a perception thing, but here
there was a good compromise.

Jay

--


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jimw_btg(at)earthlink.net
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PostPosted: Thu Jan 07, 2010 11:08 am    Post subject: Reversible electric motors and CBs Reply with quote

If you have visual access to your Fuse Block or Blocks, mine I have a light
smoke plex cover indicator led show quite well, with the ATC/ATO fuses and
the Led that lights when fuse is blown you can quite quickly determine,
first something is of malfunction, two its XXXXXX and three where the fuse
is to replace. Quite Quick and cost effective. On pre flight you can
glance at the block or blocks in seconds determine there all functioning.
All for $0.448 cents. You can get them from Wayteck, Digikey, Auto Zone
.....etc. Something that gives visual and replace able with no extra
wiring or circuit. This listing is from Wayteck. Just another thought.
Take care.

LED BLADE TYPE FUSE ATO/ATC
Category: Circuit Protection
Sub Category: Blade Fuses And Accessories
Sub-Sub Category: ATO/ATC Fuses-Light When Blown

Description: LED BLADE TYPE FUSE ATO/ATC
10 AMP RED (12 VOLTS)

Selling U/M: EA
Weight: 0.0032
Price: $0.4480
Min Order Qty: 10

Quantity Discounts:
Quantity Price
100.00 0.3808
500.00 0.3360




For larger quantities then shown,
contact Sales at quotes(at)waytekwire.com.

Qty:




Click here to view catalog.

Comments:


Jim Wickert
Tel 920-467-0219
Cell 920-912-1014

--


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nuckolls.bob(at)aeroelect
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PostPosted: Thu Jan 07, 2010 11:29 am    Post subject: Reversible electric motors and CBs Reply with quote

At 12:10 PM 1/7/2010, you wrote:
Quote:

This is an area that I have used to 'placate' one of my clients whose
aircraft I am building. He really wants to see breakers but I talked him
around to fuses and non-inflight changeable ones at that... But, to get him
to accept that I agreed that the hydraulic pump might 'overload' and hence
you might want to reset that breaker, so we put in a breaker for that
circuit and fuses for everything else. It's a perception thing, but here
there was a good compromise.

We wouldn't do that on a King Air . . . the motor
supply circuit would be protected with a ROBUST fuse,
i.e. a current limiter.

Besides, how does he get the gear down if the motor
craps?

Bob . . .


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nuckolls.bob(at)aeroelect
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PostPosted: Thu Jan 07, 2010 11:43 am    Post subject: Reversible electric motors and CBs Reply with quote

At 11:11 AM 1/7/2010, you wrote:

<mrspudandcompany(at)verizon.net>

I think virtually all
OBAM aircraft with retractable gear use hydraulics
where the motor is not subject to "overload" . . .
pressure relief valves generally address that
issue. Further, large demand devices like
motor driven hydraulics are protected with very
robust protection devices like current limiters.

The Falco, which I am building, is one OBAM aircraft which uses a motor and
jack screws to deploy the LG. There have been many complaints of the
breaker popping when raising the gear. Some owners have set the limit
switches so the gear does not retract fully, and finish the last little bit
of retraction with the hand crank. I believe there is a fundamental design
flaw in the retract mechanism, but have not seen a good fix.

There IS a fix . . . but it's not common to the
OBAM aircraft industry. Some years ago I participated
in the development of a line of electro-mechanical
landing gear actuators. They were controlled over
a serial data line and needed only +28 and a
communications line to hook up. These had micro-
controllers driving brushless dc motors. As "smart"
actuators, they knew when they were approaching
limits and would slow down to a crawl . . . the
stroke drove to hard mechanical limits in the gear
mechanism. The microprocessor sensed the up-tick
in current and shut the motor off. No limit switches
needed.

One of my clients has a line of 'smart actuators'
based on a universal controller with only the motor,
drive transistors, and actuator mechanical details
tailored to the task.

A few years ago, I built some fast electronic
current limiters for a builder who wanted to use
independent actuators at each wheel of a Lancair.
They were not fast and the mechanisms could tolerate
driving to hard stops without tearing up the gear
train. The electronic current limiters prevented
motor inrush and "limit" spikes.

Don't know how that project worked out. Don't even
recall now who was building it.

Bob . . .


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jay(at)horriblehyde.com
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PostPosted: Thu Jan 07, 2010 12:29 pm    Post subject: Reversible electric motors and CBs Reply with quote

He used to fly King Airs.. Smile
The gear comes down without power using a hydraulic release valve- which is
why I say its perception thing- he knows that he has a manual backup but he
wants a breaker or two on the panel; it's a compromise of sorts..
--


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mprather(at)spro.net
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PostPosted: Thu Jan 07, 2010 1:47 pm    Post subject: Reversible electric motors and CBs Reply with quote

I say give him a breaker which powers a switch driving a noise maker of
some sort. Flip the switch up for the light and noise, down for none.
Maybe a "ding alarm." Pull the breaker to disable. Label it "Retro
Encabulator" with apologies to Rockwell Automation...
Matt-

do not archive

[quote]
He used to fly King Airs.. Smile
The gear comes down without power using a hydraulic release valve- which
is
why I say its perception thing- he knows that he has a manual backup but
he
wants a breaker or two on the panel; it's a compromise of sorts..
--


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jay(at)horriblehyde.com
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PostPosted: Thu Jan 07, 2010 11:13 pm    Post subject: Reversible electric motors and CBs Reply with quote

Actually, what you need is one of these....

http://www.youtube.com/watch?v=Z86V_ICUCD4

--


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nuckolls.bob(at)aeroelect
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PostPosted: Fri Jan 08, 2010 3:06 pm    Post subject: Reversible electric motors and CBs Reply with quote

At 01:10 AM 1/8/2010, you wrote:
Quote:


Actually, what you need is one of these....

http://www.youtube.com/watch?v=Z86V_ICUCD4

Pretty cute. I'll have to get the details on
it. Be a good project for my oldest grandson
this summer. I've got a bucket-load of model
servos left over from a project.

Bob . . .


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