Matronics Email Lists Forum Index Matronics Email Lists
Web Forum Interface to the Matronics Email Lists
 
 Get Email Distribution Too!Get Email Distribution Too!    FAQFAQ   SearchSearch   MemberlistMemberlist   UsergroupsUsergroups   RegisterRegister 
 ProfileProfile   Log in to check your private messagesLog in to check your private messages   Log inLog in 

Push-to-Test Lamp

 
Post new topic   Reply to topic    Matronics Email Lists Forum Index -> AeroElectric-List
View previous topic :: View next topic  
Author Message
hammer408(at)comcast.net
Guest





PostPosted: Wed Aug 27, 2008 3:56 pm    Post subject: Push-to-Test Lamp Reply with quote

Bob:

I've purchased 2 Push-to-Test Lamps: MS25041 (amber) for my Low Voltage
Warning Lamp and another one (blue) for Low Oil Pressure. The lamps have3
tabs, numbered 1-2-3 and I'm trying to determine how to wire this lamp:
which is ground, hot and common....

Any help or suggestions appreciated.

Henry


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
currydon(at)bellsouth.net
Guest





PostPosted: Wed Aug 27, 2008 4:55 pm    Post subject: Push-to-Test Lamp Reply with quote

I'm not Bob, but if I may, I'd like to provide at least a cursory answer. I
just installed a pair of these lights (made by Dialight) in my aircraft and
here's how we did it (the attached document is from Dialight and should bear
this out). There are two hot terminals and one ground terminal. One of the
hot terminals is for a switched input, so when the condition you are trying
to alert yourself to (e.g., low oil pressure) occurs, the switch is closed
on that wire, the circuit is completed, and the light lights. The other hot
terminal is unswitched and is for the push-to-test feature; it allows the
light to light when the lens is pressed even when the condition doesn't
exist. I believe it is the center terminal that is the ground. Hope this
helps. Don

[quote] --


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List



Dialight_Drawing_2.pdf
 Description:

Download
 Filename:  Dialight_Drawing_2.pdf
 Filesize:  243.93 KB
 Downloaded:  532 Time(s)

Back to top
nuckolls.bob(at)cox.net
Guest





PostPosted: Wed Aug 27, 2008 7:02 pm    Post subject: Push-to-Test Lamp Reply with quote

At 07:58 PM 8/27/2008 -0700, you wrote:
Quote:

<hammer408(at)comcast.net>

Bob:

I've purchased 2 Push-to-Test Lamps: MS25041 (amber) for my Low Voltage
Warning Lamp and another one (blue) for Low Oil Pressure. The lamps have3
tabs, numbered 1-2-3 and I'm trying to determine how to wire this lamp:
which is ground, hot and common....

Any help or suggestions appreciated.

A schematic for the fixture can be found at:

http://aeroelectric.com/Pictures/Lighting/PTT_Dim_Fixture.jpg

An exemplar application can be found in:

http://www.aeroelectric.com/articles/grndpwr.pdf
Bob . . .

----------------------------------------)
( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
----------------------------------------


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
etienne.phillips(at)gmail
Guest





PostPosted: Wed Aug 27, 2008 9:27 pm    Post subject: Push-to-Test Lamp Reply with quote

On 28 Aug 2008, at 5:01 AM, Robert L. Nuckolls, III wrote:
Quote:

An exemplar application can be found in:

http://www.aeroelectric.com/articles/grndpwr.pdf
Bob . . .


Hi Bob

Just a question. From my understanding, looking at this doc and the
attachment from Don Curry, it looks as though pin 1 is common, 2 is
normal and 3 is engaged on push. In your wiring, the bulb will only
light up when external power is applied, which is great. What happens
though when the bulb doesn't light up , and there's supposedly
external power applied? There are only 3 possibilities: there is a
problem with the external power, the bulb has popped, or the circuit
breaker is not closed. In the first 2 cases, pushing the lens will
not make the bulb light up.

Would it not be better to wire the bulb so that it allows better
fault-tracing? My suggestion would be pin 1 to ground, pin 2 to the
high voltage side of the contactor coil (where pin 1 is connected on
your diagram), and pin 3 to a fuse then onto the battery bus (or any
bus that would normally be powered when you'd want to use external
power).

The behaviour of the light would change though:
If there is external power, the lamp will light up with the switch in
either position, indicating external power is available for use
If there is no external power getting in (incorrect polarity or
broken power supply) the bulb will not light
To test the bulb at any time, with or without external power applied,
push the lens

What do you think? Am I smoking my socks?

Thanks
Etienne


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
mrspudandcompany(at)veriz
Guest





PostPosted: Thu Aug 28, 2008 4:03 am    Post subject: Push-to-Test Lamp Reply with quote

Quote:
Bob:

I've purchased 2 Push-to-Test Lamps: MS25041 (amber) for my Low Voltage
Warning Lamp and another one (blue) for Low Oil Pressure. The lamps have3
tabs, numbered 1-2-3 and I'm trying to determine how to wire this lamp:
which is ground, hot and common....

Any help or suggestions appreciated.

A schematic for the fixture can be found at:

http://aeroelectric.com/Pictures/Lighting/PTT_Dim_Fixture.jpg

An exemplar application can be found in:

http://www.aeroelectric.com/articles/grndpwr.pdf
Bob . . .

It looks like the test lamp function will not work on the gndpwr.pdf
drawing. When ground power is removed there is no power to test lamp.
To wire a low oil pressure switch: assuming the switch is normally open and
goes to ground, connect pin 1 to fused 12V, pin 2 (normally closed) to the
oil pressure switch, and pin 3 to ground.

Roger


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List



winmail.dat
 Description:

Download
 Filename:  winmail.dat
 Filesize:  3.77 KB
 Downloaded:  509 Time(s)

Back to top
nuckolls.bob(at)cox.net
Guest





PostPosted: Thu Aug 28, 2008 4:55 am    Post subject: Push-to-Test Lamp Reply with quote

At 07:59 AM 8/28/2008 -0400, you wrote:
Quote:
>Bob:
>
>I've purchased 2 Push-to-Test Lamps: MS25041 (amber) for my Low Voltage
>Warning Lamp and another one (blue) for Low Oil Pressure. The lamps have3
>tabs, numbered 1-2-3 and I'm trying to determine how to wire this lamp:
>which is ground, hot and common....
>
>Any help or suggestions appreciated.

A schematic for the fixture can be found at:

http://aeroelectric.com/Pictures/Lighting/PTT_Dim_Fixture.jpg

An exemplar application can be found in:

http://www.aeroelectric.com/articles/grndpwr.pdf
Bob . . .

It looks like the test lamp function will not work on the gndpwr.pdf
drawing. When ground power is removed there is no power to test lamp.

Correct . . . it also shows that no ground power is applied.
The idea here is that the pilot can know that ground power
is available before actually applying it to the airplane.

The PTT function can be used for more purposes that to
query condition of the lamp. I've used these fixtures as
push-button, lamp-holder combinations wherein the NO contact
of the fixture is used to signal a circuit to do a self-test
routine that ends with the lamp responding in some prescribed
manner. I've also used the contact to start an auto-terminating
operation . . . like trigger a timer on a bilge pump in a
sea-plane. It runs for a period of time (light is lit) and then
shuts off (light goes out).
Quote:
To wire a low oil pressure switch: assuming the switch is normally open and
goes to ground, connect pin 1 to fused 12V, pin 2 (normally closed) to the
oil pressure switch, and pin 3 to ground.

Yup, that works!

Bob . . .
----------------------------------------)
( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
----------------------------------------


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
nuckolls.bob(at)cox.net
Guest





PostPosted: Thu Aug 28, 2008 5:16 am    Post subject: Push-to-Test Lamp Reply with quote

At 07:24 AM 8/28/2008 +0200, you wrote:
Quote:

<etienne.phillips(at)gmail.com>
On 28 Aug 2008, at 5:01 AM, Robert L. Nuckolls, III wrote:
>
>An exemplar application can be found in:
>
>http://www.aeroelectric.com/articles/grndpwr.pdf
> Bob . . .

Hi Bob

Just a question. From my understanding, looking at this doc and the
attachment from Don Curry, it looks as though pin 1 is common, 2 is
normal and 3 is engaged on push. In your wiring, the bulb will only
light up when external power is applied, which is great. What happens
though when the bulb doesn't light up , and there's supposedly
external power applied? There are only 3 possibilities: there is a
problem with the external power, the bulb has popped, or the circuit
breaker is not closed. In the first 2 cases, pushing the lens will
not make the bulb light up.

Would it not be better to wire the bulb so that it allows better
fault-tracing? My suggestion would be pin 1 to ground, pin 2 to the
high voltage side of the contactor coil (where pin 1 is connected on
your diagram), and pin 3 to a fuse then onto the battery bus (or any
bus that would normally be powered when you'd want to use external
power).

The behaviour of the light would change though:
If there is external power, the lamp will light up with the switch in
either position, indicating external power is available for use
If there is no external power getting in (incorrect polarity or
broken power supply) the bulb will not light
To test the bulb at any time, with or without external power applied,
push the lens

What do you think? Am I smoking my socks?

Not at all, you've perceived the possibilities for meeting
different design goals. I explained the rationale for
wiring as-shown in another posting. The suggestions you've
made are equally valid. The differences are how the two
circuits convey understanding . . . which assumes that
the pilot KNOWS what to expect. This suggests that it's
up to the tech-writer who crafts the POH to covey that
understanding to the future users.

Bob . . .

----------------------------------------)
( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
----------------------------------------


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
Eric M. Jones



Joined: 10 Jan 2006
Posts: 565
Location: Massachusetts

PostPosted: Thu Aug 28, 2008 6:28 am    Post subject: Re: Push-to-Test Lamp Reply with quote

The US will join Australia and most other industrialized countries to discourage (or ban) the use of filament lamps in the next few years. Building an airplane with filament lamps seems to be a stretch...unless you are building one for a museum and you want it to be historically correct-along with the silk and gutta-percha insulation on the wires.

Another reason to ditch the filament lamps is seen when you look at the efficacy of filament lamps. Big lamps, especially halogens can be >20 lumens per watt, but the tiny indicator lamps are only 3-6 lumens per watt.

Although it seems to be a small thing, incandescent lamps are horribly
inefficient in small sizes. For example:GE# 67 (smallest bayonet instrument light) 13.5 Volts Lamp Power 8W 0.59A 4 Candelas (about 50 lumens) Average Life 5000 Hours. 50 lumens/8W = 6 lumens per watt.

The similar LED is 25-100 lumens per watt, but the comparison doesn't stop there. The GE #67 incandescent is typically color-filtered so that only 10% of the emitted light is used, and it is isotropic so only 25% of THAT light goes where you need it. Furthermore using 10 GE #67 lamps (typical on a panel) is about 6 AMPS.....Astonishing load for no good reason.

And the LED will last FOREVER or 100,000 hours....whichever comes first...20X longer at least. So the LED (depending on how you figure...) is 1000X better deal.

You want to put in a Push-to-Test switch? You don't need any for the LEDs. You don't need a socket either, since the LEDs outlast the socket, the connectors, and Push-to-Talk mechanism.

"Everything you've learned in school as 'obvious' becomes less and less obvious as you begin to study the universe. For example, there are no solids in the universe. There's not even a suggestion of a solid. There are no absolute continuums. There are no surfaces. There are no straight lines."

-R. Buckminster Fuller


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List

_________________
Eric M. Jones
www.PerihelionDesign.com
113 Brentwood Drive
Southbridge, MA 01550
(508) 764-2072
emjones(at)charter.net
Back to top
View user's profile Send private message Send e-mail Visit poster's website
echristley(at)nc.rr.com
Guest





PostPosted: Thu Aug 28, 2008 6:59 am    Post subject: Push-to-Test Lamp Reply with quote

Eric M. Jones wrote:
Quote:


The US will join Australia and most other industrialized countries to discourage (or ban) the use of filament lamps in the next few years. Building an airplane with filament lamps seems to be a stretch...unless you are building one for a museum and you want it to be historically correct-along with the silk and gutta-percha insulation on the wires.

Another reason to ditch the filament lamps is seen when you look at the efficacy of filament lamps. Big lamps, especially halogens can be >20 lumens per watt, but the tiny indicator lamps are only 3-6 lumens per watt.

Although it seems to be a small thing, incandescent lamps are horribly
inefficient in small sizes. For example:GE# 67 (smallest bayonet instrument light) 13.5 Volts Lamp Power 8W 0.59A 4 Candelas (about 50 lumens) Average Life 5000 Hours. 50 lumens/8W = 6 lumens per watt.

The similar LED is 25-100 lumens per watt, but the comparison doesn't stop there. The GE #67 incandescent is typically color-filtered so that only 10% of the emitted light is used, and it is isotropic so only 25% of THAT light goes where you need it. Furthermore using 10 GE #67 lamps (typical on a panel) is about 6 AMPS.....Astonishing load for no good reason.

And the LED will last FOREVER or 100,000 hours....whichever comes first...20X longer at least. So the LED (depending on how you figure...) is 1000X better deal.

You want to put in a Push-to-Test switch? You don't need any for the LEDs. You don't need a socket either, since the LEDs outlast the socket, the connectors, and Push-to-Talk mechanism.

One more advantage with the LED is that you can put one anywhere you can

drill a 3/16" hole, and even direct the light by angling the hole
properly. The standard 5mm LED is a push fit into a 3/16" hole. Then
you just need a small amount of room on the backside for hookup wires.
If the mounting surface is thick enough and you're careful, you can use
a #30 bit for the last 1/16" of the hole. Then you don't even need a
bevel. You wind up with a nearly hidden indicator or spot illuminator.
The push fit will keep it in place, but a dollup of shoo-goo is good for
peace-of-mind.

No way you could do that with the GE #67. It needs a special socket to
get rid of all that heat.


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
Display posts from previous:   
Post new topic   Reply to topic    Matronics Email Lists Forum Index -> AeroElectric-List All times are GMT - 8 Hours
Page 1 of 1

 
Jump to:  
You cannot post new topics in this forum
You cannot reply to topics in this forum
You cannot edit your posts in this forum
You cannot delete your posts in this forum
You cannot vote in polls in this forum
You cannot attach files in this forum
You can download files in this forum


Powered by phpBB © 2001, 2005 phpBB Group