RE: Acousic Noise from ITE

2002-09-16 Thread Gary McInturff

Rich, 
There us to be a series of specifications for noise equipment in office 
environments - not so much what type of equipment but more on the order of a 
quiet office environment equipment had to be 50 or 55 dBA, I forget which. Lots 
of nasty things to go along with all of that. Printers had impulse noise to 
contend with, etc. I don't know if they have, but the trend was to go from 
sound pressure measurements to sound power measurements. On the one had it made 
it easier for the manufacturer to make repeatable and accurate measurements, 
and you didn't need to have a sound anechoic chamber and make parallel piped 
measurements at various spots around the equipment.
Been a while since I made those measurements, but Bruel and Kjaer had 
lost of papers on the issue.
Gary

-Original Message-
From: Warren Birmingham [mailto:war...@comfortjets.com]
Sent: Monday, September 16, 2002 1:26 PM
To: richwo...@tycoint.com
Cc: emc-p...@majordomo.ieee.org
Subject: Re: Acousic Noise from ITE



I went to the Global Engineering Website and http://www.global.ihs.com 
and found over 300 standards related to the keyword acoustic  You can 
narrow the search.

Warren Birmingham
Epsilon-Mu Consultants

On Monday, Sep 16, 2002, at 08:43 US/Pacific, richwo...@tycoint.com 
wrote:


 Are there any EU or national (e.g. GS) normative requirements to 
 comply with
 any of the following standards or any other acoustic standards for ITE?

 EN27779 Acoustic measurement of airborn noise emitted by computer and
 business equipment.
 EN29295 Acoustic measurement of high frequency noise emitted by 
 computer
 and business equipment.
 ISO 9296 Acoustics declared noise emission values of emitted by 
 computer
 and business equipment.


 Richard Woods
 Sensormatic Electronics
 Tyco International


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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

I was not arguing that PEDS should be allowed to operate throughout ascent
and descent.  I was responding to Woodgate's comment that if PEDS are
causing a problem, there must be serious immunity issues with aircraft
avionics.  I know in detail what the immunity requirements are, and I know
that PEDS do not emit anywhere near the immunity levels.  PEDS interfere
with radio reception.  Woodgate quite correctly pointed out that unless the
rfi occurred at the radio tuned frequency, it can be considered an antenna
port immunity concern, because immunity requirements can and are levied to
protect radio receiver out-of-band sensitivity.

--
From: Warren Birmingham war...@comfortjets.com
To: Ken Javor ken.ja...@emccompliance.com
Cc: emc-p...@ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 4:01 PM


 Ken, you may be right but it is like trying to convince the FAA that
 there is no harm in using car gas in airplanes.  There are just too
 many ways for uncontrolled fuel to become contaminated from unknown
 sources.

 With respect to the EMC and immunity issues, it is not the technical
 issues that are of concern, but rather the liability and publicity of
 even being accused of causing interference, regardless of how it got
 there.  The potential for it exists, and lives are potentially at
 stake.  Who would argue with this?

 I am also an aviation consultant as well as an engineering one.  Most
 devices are allowed to be used in flight.  Cell Phones and 2-way pagers
 cause too much GROUND interference when used from the air and THAT is
 the primary reason they are not permitted.  They use more resources
 than intended when used from the air.

 By the way, I was consulting to a company that did not even test ANY of
 their equipment to FCC Part 15, and I discovered that they were out of
 specification for Class A by several db.  We had our attorney negotiate
 with the FCC, who wanted to know if ANY of the over-limit frequencies
 fell into the aviation bands.  They did not, so we had to fix the
 problems with no other action required other than submission of new
 compliant verification reports.  There is concern for this even
 originating outside of the aircraft.

 Warren Birmingham
 Epsilon-Mu Consultants
 (510) 793-4806
 email: war...@epsilon-mu.com
 website: http://www.epsilon-mu.com


 On Monday, Sep 16, 2002, at 09:56 US/Pacific, Ken Javor wrote:


 Most of what you say below meshes with my experience and does not
 contradict
 my basic premise, that PEDs can only interfere through aircraft
 antennas.  I
 am curious what the resolution of the Boeing installation was.
 Equipment
 undergoing EMI qualification must be tested with a representative
 flight
 harness.  Did your company test with screened cables and then try to
 force
 Boeing to use the same?  Bad form.  Did Boeing try to buy an
 off-the-shelf
 system qualified with screened cables and then install the system using
 unscreened cables?  Equally bad form.  This must be worked out before
 design
 and testing for procured equipment, and if the equipment is
 off-the-shelf,
 then the qualification configuration harness must be installed, or the
 equipment must be requalified using the planned/existing configuration
 wiring.  Another question of interest: Was the system you provided
 Boeing
 flight critical?

 There is one place that what you say could be interpreted to imply
 that PED
 emissions get into aircraft wiring:

 It has been found through surveys carried out on aircraft by ERA and
 QinetiQ that the interference appears to get into these systems from
 certain
 locations within the aircraft where cable run reside under certain
 seats.

 Consider the physical parameters.  The PED is small and low power and
 while
 it may not meet RTCA/DO-160, it does not blanket the entire aircraft
 with
 emissions.  The intensity falls off rapidly with separation from the
 source.
 This is clearly a case where the emitting device is electrically small
 over
 almost the entire communications band.

 Assume the emitted radiation intensity were 100 mV/m, 5-6 orders of
 magnitude above CISPR limits.  The transfer function of coupled
 current to a
 cable above ground is 1.5 mA per Volt/meter.  I can supply that
 derivation
 if you like, but it is inherent in both RTCA/DO-160D and
 MIL-STD-461D/E.  It
 is different in IEC 61000-4-6, but that is because the ground plane is
 far
 away or nonexistent in buildings and the cable-under-test is a more
 efficient pick-up device in that environment.  Anyway, the coupled
 current
 would be 150 uA, and that assumes at least one half wavelength of the
 cable
 was immersed in a plane wave with precisely the right orientation
 relative
 to the wire in order to get that.  If the victim circuit contains
 information represented by low potentials, such as below 0.1 Volt,
 then I
 would expect the cable carrying that signal to be shielded, as in a
 twisted
 shielded pair.  150 uA riding on a shield 

Dwell times for ETS 300 019-2-3 May 1994 table B.6.3 class 3.1E

2002-09-16 Thread Gary McInturff

Have the chart in front of me and still making no sense out of it.
Table 3 Test specification T 3.1E calls out some test points and a 
dwell time along with the reference to IEC 68-2-1, -2, -14 and -56. Under the 
method column it then says that the method in Annex b can be used. 
In Annex B there is a Table B.1 that has numerous set points that don't 
match up well, in my reading, with the first table. Heavy Sigh!  Still I can 
build the profile if I just knew the dwell times at each spot. Can anybody help 
me out - I don't really want to have to by multiple IEC standards, I'd rather 
be able to buy food for the week.
Final question. They give rate changes when temperature is held 
constant and when humidity is held constant, but in some instances they change 
both simultaneously. Usually the change in temperature takes longer than the 
change in humidity - but what's a poor kid from Spokane suppose to do? First 
ramp the humidity holding temp the same, and then change the temp while holding 
the new humidity level constant?
Thanks
Gary

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Re: New EU regulations - civil aviation

2002-09-16 Thread Warren Birmingham


Ken, you may be right but it is like trying to convince the FAA that  
there is no harm in using car gas in airplanes.  There are just too  
many ways for uncontrolled fuel to become contaminated from unknown  
sources.


With respect to the EMC and immunity issues, it is not the technical  
issues that are of concern, but rather the liability and publicity of  
even being accused of causing interference, regardless of how it got  
there.  The potential for it exists, and lives are potentially at  
stake.  Who would argue with this?


I am also an aviation consultant as well as an engineering one.  Most  
devices are allowed to be used in flight.  Cell Phones and 2-way pagers  
cause too much GROUND interference when used from the air and THAT is  
the primary reason they are not permitted.  They use more resources  
than intended when used from the air.


By the way, I was consulting to a company that did not even test ANY of  
their equipment to FCC Part 15, and I discovered that they were out of  
specification for Class A by several db.  We had our attorney negotiate  
with the FCC, who wanted to know if ANY of the over-limit frequencies  
fell into the aviation bands.  They did not, so we had to fix the  
problems with no other action required other than submission of new  
compliant verification reports.  There is concern for this even  
originating outside of the aircraft.


Warren Birmingham
Epsilon-Mu Consultants
(510) 793-4806
email: war...@epsilon-mu.com
website: http://www.epsilon-mu.com


On Monday, Sep 16, 2002, at 09:56 US/Pacific, Ken Javor wrote:



Most of what you say below meshes with my experience and does not  
contradict
my basic premise, that PEDs can only interfere through aircraft  
antennas.  I
am curious what the resolution of the Boeing installation was.   
Equipment
undergoing EMI qualification must be tested with a representative  
flight
harness.  Did your company test with screened cables and then try to  
force
Boeing to use the same?  Bad form.  Did Boeing try to buy an  
off-the-shelf

system qualified with screened cables and then install the system using
unscreened cables?  Equally bad form.  This must be worked out before  
design
and testing for procured equipment, and if the equipment is  
off-the-shelf,

then the qualification configuration harness must be installed, or the
equipment must be requalified using the planned/existing configuration
wiring.  Another question of interest: Was the system you provided  
Boeing

flight critical?

There is one place that what you say could be interpreted to imply  
that PED

emissions get into aircraft wiring:

It has been found through surveys carried out on aircraft by ERA and
QinetiQ that the interference appears to get into these systems from  
certain
locations within the aircraft where cable run reside under certain  
seats.


Consider the physical parameters.  The PED is small and low power and  
while
it may not meet RTCA/DO-160, it does not blanket the entire aircraft  
with
emissions.  The intensity falls off rapidly with separation from the  
source.
This is clearly a case where the emitting device is electrically small  
over

almost the entire communications band.

Assume the emitted radiation intensity were 100 mV/m, 5-6 orders of
magnitude above CISPR limits.  The transfer function of coupled  
current to a
cable above ground is 1.5 mA per Volt/meter.  I can supply that  
derivation
if you like, but it is inherent in both RTCA/DO-160D and  
MIL-STD-461D/E.  It
is different in IEC 61000-4-6, but that is because the ground plane is  
far

away or nonexistent in buildings and the cable-under-test is a more
efficient pick-up device in that environment.  Anyway, the coupled  
current
would be 150 uA, and that assumes at least one half wavelength of the  
cable
was immersed in a plane wave with precisely the right orientation  
relative

to the wire in order to get that.  If the victim circuit contains
information represented by low potentials, such as below 0.1 Volt,  
then I
would expect the cable carrying that signal to be shielded, as in a  
twisted
shielded pair.  150 uA riding on a shield should not cause any  
problems to
any flight critical signal, even with a pigtailed shield termination.   
For
instance, if the pigtail termination yielded a transfer impedance as  
high as

50 Ohms at some frequency, the resultant common mode coupling to the
interior pair would still only be 7.5 mV.  Again I contend that Boeing  
and

Airbus would not route a flight critical signal with a threshold of
susceptibility that low.  And if the circuit is totally unshielded,  
that

implies it is a discrete or other relatively high level signal, where
information is carried in such a away that it takes Volts of induced
potential to cause an upset.  Coupling to an unshielded wire above  
ground
occurs at a transfer function of 75 mV per Volt/meter. [ Cf. IEC  
61000-4-6,
coupling efficiency of 1 Volt per Volt/meter, open circuit 

Re: Flexible cable reliability and testing

2002-09-16 Thread Warren Birmingham


UL has 2 standards which pertain to power cables.  UL 817 and UL 1072

Warren Birmingham
Epsilon-Mu Consultants

On Monday, Sep 16, 2002, at 09:32 US/Pacific, rbus...@es.com wrote:



I have been tasked with finding a standard and test procedure to 
validate the reliability of flexible cables over time. I have found a 
standard, EIA TP-41C (EIS-364-41C), but it focuses primarily on the 
electrical connectors rather than the cable. Another standard 
Mil-C-13777G is used by some of the wire and cable manufacturers, but 
searching the web I found a US Government site that indicated that 
this standard was inactive for new design.  I can find no source for 
this standard. My application is for signal cables, but I assume other 
power cables would have some type of standard which they are tested  to.


Are there other standards applicable to cables in a flex environment? 
Any help would be appreciated.


Rick Busche
Evans  Sutherland
SLC, Utah
rbus...@es.com
(801) 588-7185

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Re: Acousic Noise from ITE

2002-09-16 Thread Warren Birmingham


I went to the Global Engineering Website and http://www.global.ihs.com 
and found over 300 standards related to the keyword acoustic  You can 
narrow the search.


Warren Birmingham
Epsilon-Mu Consultants

On Monday, Sep 16, 2002, at 08:43 US/Pacific, richwo...@tycoint.com 
wrote:




Are there any EU or national (e.g. GS) normative requirements to 
comply with

any of the following standards or any other acoustic standards for ITE?


EN27779 Acoustic measurement of airborn noise emitted by computer and
business equipment.
EN29295 Acoustic measurement of high frequency noise emitted by 
computer

and business equipment.
ISO 9296 Acoustics declared noise emission values of emitted by 
computer

and business equipment.



Richard Woods
Sensormatic Electronics
Tyco International


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RE: New EU regulations - civil aviation

2002-09-16 Thread Pettit, Ghery

Bob,

A good idea, but we are dealing with some older technology in many cases.
The VOR (VHF Omni-Range) receivers are based on a pair of pulses from the
navigation station.  The station puts out a rotating pulse with a sync pulse
when the rotating pulse is at 0 degrees (magnetic).  Your receiver sees the
sync pulse and then times the delay to the second one.  30 RPS for the
rotation rate.  If an impulsive emission occurs with enough strength your
receiver responds to it and you can lose track of what radial you are on,
giving a spurious indication on the CDI (course deviation indicator).  No
error checking in this analog system.  Updating it would not be practical
given the number of aircraft equipped to use it and the cost of replacing
the equipment.  The airlines might absorb the cost (by charging higher
fares), but your average GA bugsmasher pilot just isn't going to be too hot
on spending several thousand dollars on new equipment.  It's easier to
control PEDs on the plane.

BTW, I'm one of those GA bugsmasher pilots.  I'm not too hot on my club
having to spend the money, either.  We'd have to charge members more for the
use of the planes.  Yuck.  Welcome aboard and please keep your laptop
computer stowed and turned off for the duration of the flight.  Besides,
there are more interesting things to look at out the windows than on that
screen grin.

Ghery Pettit
Intel
Boring holes in the sky and loving every minute of it!


-Original Message-
From: Robert Johnson [mailto:john...@itesafety.com]
Sent: Monday, September 16, 2002 11:58 AM
To: emc-p...@majordomo.ieee.org
Subject: RE: New EU regulations - civil aviation


One thing that surprises me about avionics is the reports of spurious
and misleading readings from instruments due to interference. It seems
in these days of error checking and verification that we should be able
to make instruments which are either confident of the data received or
capable of reporting the reason they cannot display.

Bob Johnson
ITE Safety
 


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Re: Add-On Printed Circuit

2002-09-16 Thread Warren Birmingham


You don't say to which standard UL has investigated the Product A 
device or whether is is a listed product or a Recognized Component.


The listed product A must conform to the was it was built by the 
manufacturer.  Changes/options to it must be shown in the Followup 
Services Books, otherwise the product is not covered and UL may force 
the shipments to be held for conformance or the listing mark removed.


RCs are evaluated for use in the end product according to UL's 
conditions.


Warren Birmingham
Epsilon-Mu Consultants

On Monday, Sep 16, 2002, at 08:25 US/Pacific, John Juhasz wrote:



Colleagues,

I am seeking your input.

Manufacturer A sells a complete, fully approved  (CE, FCC Part 15, UL, 
etc)

product (product A)
Manufacturer B makes a device (product B) that will plug into a 
connector in

product A
(actually inside product A's enclosure - like a 'daughter' module) as a
value added feature.
There are no external interfaces on product B, and it is not accessible
unless product A is totally dismantled. Product B is intended/sold 
only for

use with product A,
and is otherwise useless.
The two products are sold independent of each other by the 
manufacturers to

'dealer/installers'.
When the dealer/installer sells/installs product A, he can offer 
product B

as an option.

What are the regulatory requirements/manufacturer's responsibilities 
for

product B?
(est. 2-3 inches square, UL 94V-0 printed circuit board, tens of mA 
12V DC,

no external interfaces.
On-board clock).

Thoughts?

John A. Juhasz

GE Interlogix
Fiber Options Div.
Bohemia, NY


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Re: Add-On Printed Circuit

2002-09-16 Thread John Woodgate

I read in !emc-pstc that John Juhasz john.juh...@ge-interlogix.com
wrote (in 2a1845f4cde8d511b4400090279c703bfb6...@bctexc10.ilx.indsys.ge
.com) about 'Add-On Printed Circuit' on Mon, 16 Sep 2002:
What are the regulatory requirements/manufacturer's responsibilities for
product B?
(est. 2-3 inches square, UL 94V-0 printed circuit board, tens of mA 12V DC,
no external interfaces.
On-board clock). 

For Europe, the complete product, A+B, must meet the applicable safety
and EMC requirements. Since B is not exposed for retail sale, it does
not have to be CE marked, but it is not illegal to do so. 

The Declaration of Conformity for B must (if you want a quite life!)
explain what you explained, about it being embodied in A and ONLY in A. 
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Re: Earthing through screws.

2002-09-16 Thread John Woodgate

I read in !emc-pstc that Doug McKean dmck...@corp.auspex.com wrote (in
003e01c25daa$8da4b380$cb3e3...@corp.auspex.com) about 'Earthing
through screws.' on Mon, 16 Sep 2002:
I wasn't aware that primary grounding securements 
could be used for another purpose. 

It depends on the applicable safety standard; some allow it, some don't.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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EMC Chamber Relocation

2002-09-16 Thread Collins, Jeffrey

Hello Group,


We are considering relocating our 3 meter EMC chamber. Can you:

*  Recommend a company that is proficient at this and will work in the Bay
Area ( San Jose / San Francisco CA)

*  Give estimated costs

*  Share things to watch out for

*  Things you would do different the next time.

*  Give your experiences/opinion on Relocating chambers vs. Building a new
one



Thanks,


Jeffrey Collins 
Sr. HW Engineering Manager 
EMC/ NEBS/ Reliability/ Safety
CIENA  Core Switching Division
10480 Ridgeview Court, Cupertino, CA. 95014
(408) 366-4806, Fax (408) 366-4867
jcoll...@ciena.com
http://www.ciena.com






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RE: New EU regulations - civil aviation

2002-09-16 Thread Robert Johnson
One thing that surprises me about avionics is the reports of spurious
and misleading readings from instruments due to interference. It seems
in these days of error checking and verification that we should be able
to make instruments which are either confident of the data received or
capable of reporting the reason they cannot display.

Bob Johnson
ITE Safety
 

attachment: Robert Johnson.vcf

RE: Acousic Noise from ITE

2002-09-16 Thread Tyra, John

Richard,

I would contact Steven Kraemer @ TUV Rheinland in the Toronto office. He is
very knowledgeable in the area of Noise requirements in the EU.

regards,

John

-Original Message-
From: richwo...@tycoint.com [mailto:richwo...@tycoint.com]
Sent: Monday, September 16, 2002 11:44 AM
To: emc-p...@majordomo.ieee.org
Subject: Acousic Noise from ITE



Are there any EU or national (e.g. GS) normative requirements to comply with
any of the following standards or any other acoustic standards for ITE?

 EN27779 Acoustic measurement of airborn noise emitted by computer and
 business equipment.
 EN29295 Acoustic measurement of high frequency noise emitted by computer
 and business equipment.
 ISO 9296 Acoustics declared noise emission values of emitted by computer
 and business equipment.
 
 
Richard Woods
Sensormatic Electronics
Tyco International


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RE: harmonic current on inverters for industrial uses in Japan

2002-09-16 Thread POWELL, DOUG

Tom,

Thank you, your information is very helpful.

-doug

---
Douglas E. Powell, Compliance Engineer
Advanced Energy Industries, Inc.
Mail stop: 203024
1626 Sharp Point Drive
Ft. Collins, CO 80525

970.407.6410 (phone)
970-407.5410 (fax)
mailto:doug.pow...@aei.com
---





-Original Message-
From: T.Sato [mailto:vef00...@nifty.ne.jp]
Sent: Saturday, September 14, 2002 5:54 PM
To: emc-p...@ieee.org
Subject: Re: harmonic current on inverters for industrial uses in Japan



On Thu, 12 Sep 2002 08:57:51 -0600,
  POWELL, DOUG doug.pow...@aei.com wrote:

 I am searching for an English language version of a report writtne in
 Japanese, I already have the title translated:
 
 Calculation methods of harmonic current on inverters for industrial
uses.
 JEM- TR 201
 
 Can enayone help with location of this report in English?

It seems there is no English version of JEM-TR 201 at least
at this time.
Catalogue of translated JEM/JEM-TR documents is available at
http://www.jema-net.or.jp/Japanese/jem/jem_eng.htm, but it seems
none of them are available online anyway.
You may want to concact JEMA for more information.

Only for information - Japanese JEM-TR 201 is available online at:
http://www.jema-net.or.jp/Japanese/jem/jem_handou.htm

Regards,
Tom

--
Tomonori Sato  vef00...@nifty.ne.jp
URL: http://member.nifty.ne.jp/tsato/


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that is confidential and proprietary information of Advanced 
Energy Industries, Inc.  The dissemination, distribution, use 
or copying of this message or any of its attachments is 
strictly prohibited without the express written consent of 
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Re: Earthing through screws.

2002-09-16 Thread Doug McKean

I wasn't aware that primary grounding securements 
could be used for another purpose. 

Regards, Doug McKean 


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Re: Heatsinks and EMI

2002-09-16 Thread Doug McKean

Heatsinks and EMIAny metallic structure capable of carrying circulating
currents will
radiate.  Ungrounded heatsinks can be particularly susceptible to
radiation, or carrying crosstalk from one part of a circuit to
another part. Regards, Doug McKean


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Re: New EU regulations - civil aviation

2002-09-16 Thread Cortland Richmond

I've been watching this discussion with interest. It appears you are
agreeing with each other - at some length. (grin)  The subject of
interference to airborne navigation and communications receivers seems
never to go away. Since it was the probability of just such interference
which lead the FAA to impose its PED regulations, this is perhaps
appropriate. I have seen emissions from non-ITE PED's (CD players) that
greatly exceeded the FCC class B limit, and it is not unreasonable to
expect interference to receivers from many kinds of device. 

I seem to recall mention in one of the EMC magazines (Conformity?) a couple
of years ago about a GSM telephone *in checked baggage* having been
identified as causing direct EMI to aircraft systems. This, apparently
because GSM amplitude modulation is more conducive to rectified  logic
upset than a steadily emitting frequency-modulation. And of course the hold
is NOT a typical location for customer-carried PED's.

There was also mention further back (this may be on the FAA Web site - a
useful compendium of reports) of a test in which a handy-talky of some type
was, as an experiment, used to transmit inside the cockpit of an airliner,
with noticeable upset to instruments at the flight engineer's station. 
This could be direct interference from a PED, though hardly _likely_ in
flight, especially with today's security restrictions on where passengers
may go. 

I personally recall an incident about 7 years ago in which a product of my
then-employer, a laptop computer, was reported to have caused an aircraft
on a long over-water flight to take a left bank of two degrees, which trim
upset went away when the computer was turned off. However we were unable to
identify emissions which could have caused this. I do not believe that
passenger AC power, MOST likely culprit, was provided at the time, so that
seems to be ruled out, and the energy in the LCD backlight inverter was far
enough away from wiring that it SHOULD not have done so.

Cortland

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EMI from heatsinks

2002-09-16 Thread Fleury, Bill

Richard,

I have three different articles about this subject. I think I found them on
CDs from recent IEEE EMC Symposiums but I don't remember which ones or even
if they were all on the same CD. I saved the files so I can e-mail them to
you if you wish; as I don't think the files are that big. 

Regards,
Bill Fleury

***Artesyn Communication Products, LLC**


Bill Fleury Email: bi...@artesyncp.com
Compliance Engineer Phone: 608-826-8375
8310 Excelsior DriveFax:   608-831-8844
Madison, WI 53717


Friends are those people who know the words to the song in your heart and
sing them back to you when you have forgotten the words.
(unattributed)

*** Visit us at www.artesyn.com/cp **


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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

Most of what you say below meshes with my experience and does not contradict
my basic premise, that PEDs can only interfere through aircraft antennas.  I
am curious what the resolution of the Boeing installation was.  Equipment
undergoing EMI qualification must be tested with a representative flight
harness.  Did your company test with screened cables and then try to force
Boeing to use the same?  Bad form.  Did Boeing try to buy an off-the-shelf
system qualified with screened cables and then install the system using
unscreened cables?  Equally bad form.  This must be worked out before design
and testing for procured equipment, and if the equipment is off-the-shelf,
then the qualification configuration harness must be installed, or the
equipment must be requalified using the planned/existing configuration
wiring.  Another question of interest: Was the system you provided Boeing
flight critical?

There is one place that what you say could be interpreted to imply that PED
emissions get into aircraft wiring:

It has been found through surveys carried out on aircraft by ERA and
QinetiQ that the interference appears to get into these systems from certain
locations within the aircraft where cable run reside under certain seats.

Consider the physical parameters.  The PED is small and low power and while
it may not meet RTCA/DO-160, it does not blanket the entire aircraft with
emissions.  The intensity falls off rapidly with separation from the source.
This is clearly a case where the emitting device is electrically small over
almost the entire communications band.

Assume the emitted radiation intensity were 100 mV/m, 5-6 orders of
magnitude above CISPR limits.  The transfer function of coupled current to a
cable above ground is 1.5 mA per Volt/meter.  I can supply that derivation
if you like, but it is inherent in both RTCA/DO-160D and MIL-STD-461D/E.  It
is different in IEC 61000-4-6, but that is because the ground plane is far
away or nonexistent in buildings and the cable-under-test is a more
efficient pick-up device in that environment.  Anyway, the coupled current
would be 150 uA, and that assumes at least one half wavelength of the cable
was immersed in a plane wave with precisely the right orientation relative
to the wire in order to get that.  If the victim circuit contains
information represented by low potentials, such as below 0.1 Volt, then I
would expect the cable carrying that signal to be shielded, as in a twisted
shielded pair.  150 uA riding on a shield should not cause any problems to
any flight critical signal, even with a pigtailed shield termination.  For
instance, if the pigtail termination yielded a transfer impedance as high as
50 Ohms at some frequency, the resultant common mode coupling to the
interior pair would still only be 7.5 mV.  Again I contend that Boeing and
Airbus would not route a flight critical signal with a threshold of
susceptibility that low.  And if the circuit is totally unshielded, that
implies it is a discrete or other relatively high level signal, where
information is carried in such a away that it takes Volts of induced
potential to cause an upset.  Coupling to an unshielded wire above ground
occurs at a transfer function of 75 mV per Volt/meter. [ Cf. IEC 61000-4-6,
coupling efficiency of 1 Volt per Volt/meter, open circuit from a 150 Ohm
source impedance.]  Given the original 100 mV/m assumption, that translates
into a coupled common mode potential of 7.5 mV and the conclusion still
stands: no possibility of interference.

--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 8:55 AM



 Ken

 During the mid 90s we manufactured equipment that was installed on 747s
 which was tested to RTCA/DO-160C and all the cables on that aircraft for
 that system were unscreened. Boeing informed us that they would not permit
 screened cables due to the increase in weight that would then affect the
 passenger cargo carrying capability of the aircraft.

 I know that  rf signals are coax and that certain control signals are
 screened for flight critical systems.

 It isn't so bad for newer aircraft but some of the older ones that use Omega
 and the earlier flight nav systems have reported interfernce with these
 systems and the autopilot. When the passengers have been requested to switch
 off their equipments the interference has dissappeared.

 It has been found through surveys carried out on aircraft by ERA and QinetiQ
 that the interfernce appears to get into these systems from certain
 locations within the aircraft where cable run reside under certain seats.

 Incidents of interfernce breakthough on coms have been more difficult to
 identify. Investigations are still being carried out.

 If you want more data suggest you get in touch wuth Dr Nigel Carter @
 QinetiQ or Eric Stevens @ ERA.

 Regards
 Andy

 Andrew Price
 Principal Development Engineer (EMC Specialist)
 BAE 

Flexible cable reliability and testing

2002-09-16 Thread rbusche

I have been tasked with finding a standard and test procedure to validate the 
reliability of flexible cables over time. I have found a standard, EIA TP-41C 
(EIS-364-41C), but it focuses primarily on the electrical connectors rather 
than the cable. Another standard Mil-C-13777G is used by some of the wire and 
cable manufacturers, but searching the web I found a US Government site that 
indicated that this standard was inactive for new design.  I can find no 
source for this standard. My application is for signal cables, but I assume 
other power cables would have some type of standard which they are tested to.

Are there other standards applicable to cables in a flex environment? Any help 
would be appreciated.

Rick Busche
Evans  Sutherland
SLC, Utah
rbus...@es.com
(801) 588-7185

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

Very good point.  Obviously the cables could be very long, at least as long
as half the aircraft, if the 12 Vdc supply were situated in the exact center
of the aircraft.  Since the laptops were qualified running of a 50/60 Hz
power mains, the measured CSIPR emissions don't apply to this mode.  Would
it be too much to expect that the adapters for sale for this purpose do meet
stringent RE limits?  Or do they fall in a a regulation crack - CISPR
wouldn't apply and somehow I don't see these devices being qualified to
RTCA/DO-160.

But while all of this is interesting and food for thought, it STILL doesn't
affect my basic premise, that PEDs interfere with aircraft operation via
aircraft antennas, not aircraft wires.

--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:15 AM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2i001lcfw...@mtaout04.icomcast.net) about 'New EU regulations -
 civil aviation' on Sun, 15 Sep 2002:
My response is that conducted path is so lossy as to be negligible.

 But how long are the cables? I think we have more or less agreed that it
 is *radiation* from consumer devices interfering with aircraft radio
 reception where the potential problem arises. Hence the threat with the
 12 V supplies is *radiation from the cables*, due to conducted emissions
 form the consumer device.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

Actually the mil-std appendix does exactly what you suggest; the following
is excerpted from the discussion for RE102, which controls radiated electric
field emissions:

The basic intent of the requirement is to protect sensitive receivers from
interference coupled through the antennas associated with the receiver.
Many tuned receivers have sensitivities on the order of one microvolt and
are connected to an intentional aperture (the antenna) which are constructed
for efficient reception of energy in the operating range of the receiver.
The potential for degradation requires relatively stringent requirements to
prevent platform problems.

There is no implied relationship between this requirement and RS103 that
addresses radiated susceptibility to electric fields.  Attempts have been
made quite frequently in the past to compare electric field radiated
emission and susceptibility type requirements as a justification for
deviations and waivers.  While RE102 is concerned with potential effects
with antenna-connected receivers, RS103 simulates fields resulting from
antenna-connected transmitters.


--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:17 AM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2i002t0im...@mtaout03.icomcast.net) about 'New EU regulations -
 civil aviation' on Sun, 15 Sep 2002:

Another way to say this is to paraphrase the appendix of MIL-STD-461D/E,
which states categorically that there is no relationship between radiated
emissions and radiates susceptibility requirements, they are for different
purposes and the magnitudes between the respective limits are not to be
considered a design margin.

 That is true, but it would be more helpful if it went on to explain what
 the 'different purposes' are.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

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Acousic Noise from ITE

2002-09-16 Thread richwoods

Are there any EU or national (e.g. GS) normative requirements to comply with
any of the following standards or any other acoustic standards for ITE?

 EN27779 Acoustic measurement of airborn noise emitted by computer and
 business equipment.
 EN29295 Acoustic measurement of high frequency noise emitted by computer
 and business equipment.
 ISO 9296 Acoustics declared noise emission values of emitted by computer
 and business equipment.
 
 
Richard Woods
Sensormatic Electronics
Tyco International


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Add-On Printed Circuit

2002-09-16 Thread John Juhasz

Colleagues,

I am seeking your input.

Manufacturer A sells a complete, fully approved  (CE, FCC Part 15, UL, etc)
product (product A)
Manufacturer B makes a device (product B) that will plug into a connector in
product A
(actually inside product A's enclosure - like a 'daughter' module) as a
value added feature. 
There are no external interfaces on product B, and it is not accessible
unless product A is totally dismantled. Product B is intended/sold only for
use with product A,
and is otherwise useless.
The two products are sold independent of each other by the manufacturers to
'dealer/installers'. 
When the dealer/installer sells/installs product A, he can offer product B
as an option.

What are the regulatory requirements/manufacturer's responsibilities for
product B?
(est. 2-3 inches square, UL 94V-0 printed circuit board, tens of mA 12V DC,
no external interfaces.
On-board clock). 

Thoughts?

John A. Juhasz

GE Interlogix
Fiber Options Div.
Bohemia, NY 


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RE: New EU regulations - civil aviation

2002-09-16 Thread Price, Ed

This discussion is touching on several aspects of Personal Electronic
Devices (PED's) aboard aircraft. Bruce Donham, of Boeing, has a two-year-old
paper with some hard data at:

http://www.boeing.com/commercial/aeromagazine/aero_10/interfere_story.html

Also, here's a cross reference to PED Electronic regulations:

http://aviation-safety.net/events/ped/ped-regl.htm

And, 106 pages of Aviation Safety Reporting System PED related history,
current to May 2002, at:

http://asrs.arc.nasa.gov/report_sets/ped.pdf


This whole subject is about as confusing as EMF's and cancer.


Regards,

Ed


Ed Price
ed.pr...@cubic.com
Electromagnetic Compatibility Lab
Cubic Defense Systems
San Diego, CA  USA
858-505-2780  (Voice)
858-505-1583  (Fax)
Military  Avionics EMC Is Our Specialty
Shake-Bake-Shock - Metrology - Reliability Analysis


-Original Message-
From: Ken Javor [mailto:ken.ja...@emccompliance.com]
Sent: Monday, September 16, 2002 6:33 AM
To: andrew.p.pr...@baesystems.com; emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation



I do realize there is a big difference in the use of cable 
shielding/screening between general and commercial aviation practices.
However the same general aviation aircraft that get by with 
little or no
cable shielding/screening also have no electronic critical 
flight controls,
so it is a wash.  Any aircraft with flight controls qualified to
RTCA/DO-160A will also have its maximum degree of automation limited to
using the autopilot, possibly in conjunction with navigation 
inputs from
aircraft NAV receivers.  Both the rf (coax) and the base-band 
signal inputs
into the autopilot would be shielded in my experience.  I 
would definitely
NOT expect personal electronics to interfere with such control systems
(except for that all-important radio link).

I would also expect that as an older aircraft gets avionics 
upgrades, with
avionics qualified to RTA/DO-160D, that the cables connecting 
to the new
avionics must be upgraded if the certification is to maintain validity.
Specifically, if a new avionics upgrade were form, fit and function
compatible with the old part, but required a shielded harness to meet
RTCA/DO-160D, then that cable would have to be retrofitted 
along with the
equipment.  Am I being overly idealistic and out of touch here?

In any case I reiterate: basic systems engineering practices 
mandate that a
(non-rf)  signal that carries flight critical information 
should be piped
through the aircraft such that neither cross-talk nor stray 
emissions from
other electronics cause interference.

Along these lines, there are those who mourn the passing of 
the old term,
rfi, because the term evoked the concept of RADIO 
interference, rather than
the general term electromagnetic interference, which is global in its
meaning.  We need to consciously retain the idea that stray 
(unintentional)
rf emissions from non-antenna connected electronics have the 
potential to
create only rfi.
--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:57 AM



 Firstly all avionic equipment is qualified to RTCA/DO-160 (European
 equivalent EUROCAE ED-14).
 All new equipment is test to DO-160D however there is still equipment
 installed on aircraft that was originally tested to DO-160A.
 Overtime the DO-160 has become more stringent with tighter 
emission levels
 and high immunity test levels which includes HIRF testing.

 There is one problem that arises from this as most of the 
cabling installed
 on the aircraft is unscreened. This is for weight saving reasons.

 Therefore with alot of older aircraft having a mixture of new and old
 equipments installed using cabling that is unscreened it is 
reasonable to
 assume that some Passenger Portable devices such as Gameboys, Laptop
 Computors, Mobile Phones, etc. will if that passenger 
happens to be sitting
 above a cable run cause interference with one or more 
aircraft systems. The
 UKCAA keeps a log of all reported incidents.

 Regards
 Andy


 Andrew Price
 Principal Development Engineer (EMC Specialist)
 BAE SYSTEMS Avionics
 A125
 Christopher Martin Road
 Basildon, Essex
 SS14 3EL

 tel:   +44 (0) 1268 883308
 email: andrew.p.pr...@baesystems.com


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Heatsinks and EMI

2002-09-16 Thread Georgerian, Richard
Greetings All,

I sort of remember reading an article on heatsinks and radiated emissions
within the past 12 months. In short, the article indicated that the fins of
the heatsink should be considered an antenna regarding radiated emissions.
Has anyone else remember seeing such an article? If so, can you send me
where I might again find it. I have tried the archives of RF Design,
Conformity, Evaluation Engineering and Power Electronics. Search on the web
on 'heatsinks + emi did not prove fruitful.

Thanks in-advance.

Richard Georgerian
Compliance Engineer 
Carrier Access Corporation
5395 Pearl Parkway
Boulder, CO 80301
USA

Tele: 303-218-5748  Fax: 303-218-5503
mailto:rgeorger...@carrieraccess.com


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Re: New EU regulations - civil aviation

2002-09-16 Thread andrew . p . price

Ken

During the mid 90s we manufactured equipment that was installed on 747s
which was tested to RTCA/DO-160C and all the cables on that aircraft for
that system were unscreened. Boeing informed us that they would not permit
screened cables due to the increase in weight that would then affect the
passenger cargo carrying capability of the aircraft.

I know that  rf signals are coax and that certain control signals are
screened for flight critical systems.

It isn't so bad for newer aircraft but some of the older ones that use Omega
and the earlier flight nav systems have reported interfernce with these
systems and the autopilot. When the passengers have been requested to switch
off their equipments the interference has dissappeared.

It has been found through surveys carried out on aircraft by ERA and QinetiQ
that the interfernce appears to get into these systems from certain
locations within the aircraft where cable run reside under certain seats.

Incidents of interfernce breakthough on coms have been more difficult to
identify. Investigations are still being carried out.

If you want more data suggest you get in touch wuth Dr Nigel Carter @
QinetiQ or Eric Stevens @ ERA.

Regards
Andy

Andrew Price
Principal Development Engineer (EMC Specialist)
BAE SYSTEMS Avionics
A125
Christopher Martin Road
Basildon, Essex
SS14 3EL

tel:   +44 (0) 1268 883308
email: andrew.p.pr...@baesystems.com
 


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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

I do realize there is a big difference in the use of cable 
shielding/screening between general and commercial aviation practices.
However the same general aviation aircraft that get by with little or no
cable shielding/screening also have no electronic critical flight controls,
so it is a wash.  Any aircraft with flight controls qualified to
RTCA/DO-160A will also have its maximum degree of automation limited to
using the autopilot, possibly in conjunction with navigation inputs from
aircraft NAV receivers.  Both the rf (coax) and the base-band signal inputs
into the autopilot would be shielded in my experience.  I would definitely
NOT expect personal electronics to interfere with such control systems
(except for that all-important radio link).

I would also expect that as an older aircraft gets avionics upgrades, with
avionics qualified to RTA/DO-160D, that the cables connecting to the new
avionics must be upgraded if the certification is to maintain validity.
Specifically, if a new avionics upgrade were form, fit and function
compatible with the old part, but required a shielded harness to meet
RTCA/DO-160D, then that cable would have to be retrofitted along with the
equipment.  Am I being overly idealistic and out of touch here?

In any case I reiterate: basic systems engineering practices mandate that a
(non-rf)  signal that carries flight critical information should be piped
through the aircraft such that neither cross-talk nor stray emissions from
other electronics cause interference.

Along these lines, there are those who mourn the passing of the old term,
rfi, because the term evoked the concept of RADIO interference, rather than
the general term electromagnetic interference, which is global in its
meaning.  We need to consciously retain the idea that stray (unintentional)
rf emissions from non-antenna connected electronics have the potential to
create only rfi.
--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:57 AM



 Firstly all avionic equipment is qualified to RTCA/DO-160 (European
 equivalent EUROCAE ED-14).
 All new equipment is test to DO-160D however there is still equipment
 installed on aircraft that was originally tested to DO-160A.
 Overtime the DO-160 has become more stringent with tighter emission levels
 and high immunity test levels which includes HIRF testing.

 There is one problem that arises from this as most of the cabling installed
 on the aircraft is unscreened. This is for weight saving reasons.

 Therefore with alot of older aircraft having a mixture of new and old
 equipments installed using cabling that is unscreened it is reasonable to
 assume that some Passenger Portable devices such as Gameboys, Laptop
 Computors, Mobile Phones, etc. will if that passenger happens to be sitting
 above a cable run cause interference with one or more aircraft systems. The
 UKCAA keeps a log of all reported incidents.

 Regards
 Andy


 Andrew Price
 Principal Development Engineer (EMC Specialist)
 BAE SYSTEMS Avionics
 A125
 Christopher Martin Road
 Basildon, Essex
 SS14 3EL

 tel:   +44 (0) 1268 883308
 email: andrew.p.pr...@baesystems.com



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Re: New EU regulations - civil aviation

2002-09-16 Thread andrew . p . price

Firstly all avionic equipment is qualified to RTCA/DO-160 (European
equivalent EUROCAE ED-14).
All new equipment is test to DO-160D however there is still equipment
installed on aircraft that was originally tested to DO-160A.
Overtime the DO-160 has become more stringent with tighter emission levels
and high immunity test levels which includes HIRF testing.

There is one problem that arises from this as most of the cabling installed
on the aircraft is unscreened. This is for weight saving reasons.

Therefore with alot of older aircraft having a mixture of new and old
equipments installed using cabling that is unscreened it is reasonable to
assume that some Passenger Portable devices such as Gameboys, Laptop
Computors, Mobile Phones, etc. will if that passenger happens to be sitting
above a cable run cause interference with one or more aircraft systems. The
UKCAA keeps a log of all reported incidents.

Regards
Andy


Andrew Price
Principal Development Engineer (EMC Specialist)
BAE SYSTEMS Avionics
A125
Christopher Martin Road
Basildon, Essex
SS14 3EL

tel:   +44 (0) 1268 883308
email: andrew.p.pr...@baesystems.com
 


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Re: New EU regulations - civil aviation

2002-09-16 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2i002t0im...@mtaout03.icomcast.net) about 'New EU regulations -
civil aviation' on Sun, 15 Sep 2002:

Another way to say this is to paraphrase the appendix of MIL-STD-461D/E,
which states categorically that there is no relationship between radiated
emissions and radiates susceptibility requirements, they are for different
purposes and the magnitudes between the respective limits are not to be
considered a design margin.

That is true, but it would be more helpful if it went on to explain what
the 'different purposes' are. 
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-16 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2i001lcfw...@mtaout04.icomcast.net) about 'New EU regulations -
civil aviation' on Sun, 15 Sep 2002:
My response is that conducted path is so lossy as to be negligible.  

But how long are the cables? I think we have more or less agreed that it
is *radiation* from consumer devices interfering with aircraft radio
reception where the potential problem arises. Hence the threat with the
12 V supplies is *radiation from the cables*, due to conducted emissions
form the consumer device.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Reminder: Sep Meeting of RMCEMC

2002-09-16 Thread Charles Grasso

To all interested parties:

The September meeting of the RMCEMC IEEE Society is:

The Mysteries of Grounding on Tuesday, September 17, at
the Courtyard by Mariott in Louisville, CO from
7:00pm to 8:00pm. The speaker will be Daryl Gerke of 
Kimmel Gerke Associates.

For more details please go to our website at
www.ieee.org/rmcemc

Thank you
Charles Grasso
RMCEMC Vice-Chair

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

I agree that we agree.  The reason I responded in so much depth on this 
thread is that I consider the underlying issue behind the terminology very
important, and I was dismayed during an earlier similar thread at some of
the responses posted on this forum.  The issue I am referring to is that RE
are controlled to protect radio receivers, and not electronics in general.
Another way to say this is to paraphrase the appendix of MIL-STD-461D/E,
which states categorically that there is no relationship between radiated
emissions and radiates susceptibility requirements, they are for different
purposes and the magnitudes between the respective limits are not to be
considered a design margin.

--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sun, Sep 15, 2002, 2:29 PM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2h0068wpv...@mtaout06.icomcast.net) about 'New EU regulations -
 civil aviation' on Sun, 15 Sep 2002:

We are getting off subject, in that the CISPR requirements listed below
don't apply to avionics, only to the personal electronics people carry on
board.

 I thought we were discussing your very restricted 'definition' of
 immunity.

 However, I don't think we really disagree very much on the actual
 issues, just a bit on the terminology.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

My response is that conducted path is so lossy as to be negligible.  
Consider that the 12 Vdc is developed by conversion from either aircraft 28
Vdc, or 400 cycles.  In either case, that converter or power supply must
meet the conducted emissions requirements of RTCA/DO-160, or its European
equivalent.  The 12 Vdc loads do not interface directly with aircraft power.
Further, aircraft avionics, including radios, must meet stringent conducted
susceptibility/immunity requirements on input power ports.  Although I am
not familiar with the European equivalent, I am sure it is the same way,
because it was a British influence that placed similar requirements in
RTCA/DO-160 and MIL-STD-461.  I refer here mainly to Dr. Nigel Carter of the
UK.  These conducted susceptibility/immunity requirements simulate the
effect of powerful radio transmissions coupling to the aircraft power bus,
and are at levels orders of magnitude above the CE limits placed on aircraft
avionics.  I would say that it is a highly unlikely path for influencing
aircraft avionics, although I would also say that if I, as an EMC engineer
working for a major air-framer, were procuring a 12 Vdc supply for this use,
I would push to characterize its input/output isolation from 0.15 - 400 MHz,
for the sake of completeness.  By input/output in this case I mean injecting
a signal on the 12 Vdc output, and measuring the resultant signal on the
aircraft power side.  And I would measure this both differential and common
mode, as I would expect different performance for different modes.  But that
would be strictly a CYA file, not a hard requirement.

--
From: Warren Birmingham war...@comfortjets.com
To: Ken Javor ken.ja...@emccompliance.com, emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sun, Sep 15, 2002, 3:41 PM


 This is not so.  Many aircraft now have personal 12v ports under each
 seat for personal electronic devices.

 Warren Birmingham
 Epsilon-Mu Consultants
 (510) 793-4806
 email: war...@epsilon-mu.com
 website: http://www.epsilon-mu.com


 On Sunday, Sep 15, 2002, at 10:28 US/Pacific, Ken Javor wrote:

 The point is that personal electronics carried on board an aircraft
 interact
 with the aircraft ONLY via the radiated emissions route.
 

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