X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from m12.lax.untd.com ([64.136.30.75] verified) by logan.com (CommuniGate Pro SMTP 4.3.4) with SMTP id 984780 for flyrotary@lancaironline.net; Sat, 04 Jun 2005 18:16:33 -0400 Received-SPF: pass receiver=logan.com; client-ip=64.136.30.75; envelope-from=alwick@juno.com Received: from m12.lax.untd.com (localhost [127.0.0.1]) by m12.lax.untd.com with SMTP id AABBLELAHAALHTQJ for (sender ); Sat, 4 Jun 2005 15:15:35 -0700 (PDT) X-UNTD-OriginStamp: L941HVjjYzDhN3itp//mkLBBB3RdatArHzxC0v4Vf2qe109R/JcHUg== Received: (from alwick@juno.com) by m12.lax.untd.com (jqueuemail) id KUPDSX8V; Sat, 04 Jun 2005 15:14:58 PDT To: flyrotary@lancaironline.net Date: Sat, 4 Jun 2005 14:53:09 -0700 Subject: Re: [FlyRotary] Re: Rotary risks Message-ID: <20050604.151405.2820.1.alwick@juno.com> X-Mailer: Juno 5.0.33 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary=--__JNP_000_381f.56ba.5c27 X-Juno-Line-Breaks: 8-6,10-11,13-14,16-22,24,26-27,30-31,33,36-37,42-45,47-48,55-56,58-63,65-71,77-78,85,90-91,96-97,102,108-109,111-121,123-133,140-147,148-32767 From: al p wick X-ContentStamp: 50:25:197487270 X-MAIL-INFO:0df3c35747e72b7b0a4b8fc31f67bf4b2fdbbf2b9feb6ebffb5a2abb33be2ebeab57079b13cf3f9f97d3d3aaf71a2a0fdb5e8a9f6bb3b347e77b670a7f2fbf4702bf2b9aae0f27bf1ec3f34fe71e270f1e2e1eebce9ba39eb38e47ee476ee7d72b9f03d70a7b439b5fea1b83e32f0ebf8387bb17fb373f7efbbb7e73e3bb77df6f7b3b5abeda9f33af7ff79a1ada0f2a3ade X-UNTD-Peer-Info: 127.0.0.1|localhost|m12.lax.untd.com|alwick@juno.com This message is in MIME format. Since your mail reader does not understand this format, some or all of this message may not be legible. ----__JNP_000_381f.56ba.5c27 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit You ask me all these questions about my installation. I don't understand why. It has no bearing on the subject. Let's pretend I fly the highest risk aircraft ever made. Does that mean all my risk statements below have no substance? Does that mean there are no rotary risks? What in the world makes you think I'm comparing the two types of engines? I apologize for my "long winded" remark. I can see how it would appear condescending and inappropriate. -al wick On Sat, 4 Jun 2005 13:48:55 -0400 "Ian Dewhirst" writes: Hi Al, I was not going to bother replying to your posts but your last one pushed me over the top. I have a couple of questions: 1) Do you have two ECMs? Having redundant crank angle sensors is great, feeding them all into one computer is no better then having only one crank sensor. 2) Have you tested limp home mode on climb out? 3) How is your power output with a partially shorted temp sensor? I'm betting it is not going to be too good - like none. 4) How old is your ECM? Most people junk their cars after 10 years, where did you get data to support the reliability of the ECM as it ages? I do have some experience in automobile failure modes, I am a licensed auto technician with OBDII training. I have colleagues who work on Subaru's, one fellow works at a local dealership, and two others work at independent garages. FYI Subaru's, like every other vehicle ever made, do come in on a hook and they do coast to a stop from time to time. One last thing, you wrote: "Sorry for being so long winded, I have the impression that stuff like this haven't been discussed before." That's right, we are all morons that don't grasp concepts like risk and redundancy. While I plan to have fully redundant ignition and fuel, (using an EC-2 as primary and a megaSquirtNSpark as a backup) Tracy (and his many customers) concluded that some inputs like a crank angle sensor did not represent a failure risk, he seems like a pretty smart guy who considers the decisions he makes. 1600+ hours suggests to me that his decisions are pretty good. You may be a great analyst - your skills as a diplomat leave a lot to be desired. -- Ian -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net]On Behalf Of al p wick Sent: Saturday, June 04, 2005 10:43 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Rotary risks First, let's try to get a perspective. There is no job as creative as that of Design Engineer. This guy is making hundreds of decisions. How many inputs do I need, what size resistor, how wide should that track be, how do I isolate that from vibration, etc etc. It's a very very high risk activity. So easy to overlook something. Many of the decisions are arbitrary. You are just making your best guess. The Japanese produce superior products. When we analyzed their success 30 years ago, we found they used certain tools in the design and validation phase that U.S. designers didn't. One of these is the FMEA (see web site). They get a group of engineers together and say" Ok, this is our best guess on how it should be designed, what's going to fail?". They go thru each characteristic and rate them for risk. Then they find a way to prove how far from failure each of those items are. For example, they'll say"Ok, the alternator is going to fail. This will produce an ac voltage." So then they measure how large the ac voltage can get before the device dies. Then they take action if there is not a large safety margin, retest. They end up with numbers that measure their safety margin. So I would encourage reviewing all the various failure modes of the ECM. Deliberately subject it to experiences beyond what it will normally see. Unplug each sensor, see how it handles it. Apply heat way beyond normal, apply vibrations beyond normal. There are very simple ways to do this. It doesn't have to be some long drawn out thing. However, statistically, we know if you have true redundancy in this particular device, then you get to multiply the probability of failure. So if the probability of shut down is 1 time in 1000 hours, since we have two with independent probabilities, our odds plummet to 1 time in 1 million hours. So all you need are two independent circuits. When in doubt, just take a look at what the auto designers have done. They use more than one sensor to measure each characteristic. They compare the sensor results to historical data. They instantly recognize the sensor is providing false data, then warn you, and use tables or other sensor to keep you plugging along. That's why you don't see vehicles sitting on the side of the road. Sorry for being so long winded, I have the impression that stuff like this haven't been discussed before. -al wick Artificial intelligence in cockpit, Cozy IV powered by stock Subaru 2.5 N9032U 200+ hours on engine/airframe from Portland, Oregon Prop construct, Subaru install, Risk assessment, Glass panel design info: http://www.maddyhome.com/canardpages/pages/alwick/index.html On Sat, 4 Jun 2005 07:50:46 -0500 "William" writes: Al, What changes would be required? (reference your statement below) Bill Schertz KIS Cruiser # 4045 ----- Original Message ----- From: al p wick To: Rotary motors in aircraft Sent: Friday, June 03, 2005 9:50 PM Subject: [FlyRotary] Re: Rotary risks You bring up very important points. If you guys can develop robust solutions for each of the challenges, then you can end up with a powerplant that has some fabulous failure modes. Here is a great example, I suspect your ECM shutdown risk is now somewhere around 1 time in 1000 (maybe 500) hours. But with simple changes that make the system genuinely redundant, you would automatically raise that to 1 time in 1000000 hours. That is fantastic for a custom low volume ECM. -al wick Artificial intelligence in cockpit, Cozy IV powered by stock Subaru 2.5 N9032U 200+ hours on engine/airframe from Portland, Oregon Prop construct, Subaru install, Risk assessment, Glass panel design info: http://www.maddyhome.com/canardpages/pages/alwick/index.html ----__JNP_000_381f.56ba.5c27 Content-Type: text/html; charset=us-ascii Content-Transfer-Encoding: quoted-printable
You ask me all these questions about my installation. I don't = understand=20 why. It has no bearing on the subject. Let's pretend I fly the highest risk= =20 aircraft ever made. Does that mean all my risk statements below have = no=20 substance? Does that mean there are no rotary risks?
 
What in the world makes you think I'm comparing the two types of = engines?=20
 
I apologize for my "long winded" remark. I can see how it would appear= =20 condescending and inappropriate.
 
-al wick
 
 
 
 
On Sat, 4 Jun 2005 13:48:55 -0400 "Ian Dewhirst" <ianddsl@magma.ca> writes:
Hi=20 Al, I was not going to bother replying to your posts but your last one = pushed=20 me over the top.  I have a couple of questions:
 
1)=20 Do you have two ECMs?  Having redundant crank angle sensors is=20 great,  feeding them all into one computer is no better then = having=20 only one crank sensor.  
2)=20 Have you tested limp home mode on climb out?
3)=20 How is your power output with a partially shorted temp sensor?  I'm= =20 betting it is not going to be too good - like none.
4)=20 How old is your ECM?  Most people junk their cars after 10 years, = where=20 did you get data to support the reliability of the ECM as it ages?&= nbsp;=20
 
I = do have some=20 experience in automobile failure modes, I am a licensed auto = technician=20 with OBDII training. I have colleagues who work on Subaru's, one fellow = works=20 at a local dealership, and two others work at independent garages.  = FYI=20 Subaru's, like every other vehicle ever made, do come in on a hook = and=20 they do coast to a stop from time to time. 
 
One=20 last thing, you wrote:
 
"Sorry = for being so=20 long winded, I have the impression that stuff like this haven't been = discussed=20 before."
 
That's right, we are all morons that don't grasp concepts like = risk and=20 redundancy.  While I plan to have fully redundant ignition and fuel,= =20 (using an EC-2 as primary and a megaSquirtNSpark as a backup)=20 Tracy (and his many customers) concluded that some inputs like a = crank=20 angle sensor did not represent a failure risk, he seems like a pretty = smart=20 guy who considers the decisions he makes.  1600+ hours suggests to = me=20 that his decisions are pretty good. 
 
You=20 may be a great analyst - your skills as a diplomat leave a lot to be=20 desired.
 
--=20 Ian
 
 
-----Original Message-----
From: Rotary motors in = aircraft=20 [mailto:flyrotary@lancaironline.net]On Behalf Of al p=20 wick
Sent: Saturday, June 04, 2005 10:43 AM
To: = Rotary=20 motors in aircraft
Subject: [FlyRotary] Re: Rotary=20 risks

First, let's try to get a perspective.
There is no job as creative as that of Design Engineer. This guy = is=20 making hundreds of decisions. How many inputs do I need, what size = resistor,=20 how wide should that track be, how do I isolate that from vibration, = etc=20 etc. It's a very very high risk activity. So easy to overlook something= .=20 Many of the decisions are arbitrary. You are just making your best = guess.=20
 
The Japanese produce superior products. When we analyzed their = success=20 30 years ago, we found they used certain tools in the design and = validation=20 phase that U.S. designers didn't. One of these is the FMEA (see web = site).=20 They get a group of engineers together and say" Ok, this is our = best=20 guess on how it should be designed, what's going to fail?". They go = thru=20 each characteristic and rate them for risk. Then they find a way to = prove=20 how far from failure each of those items are.
For example, they'll say"Ok, the alternator is going to fail. This= will=20 produce an ac voltage." So then they measure how large the ac voltage = can=20 get before the device dies. Then they take action if there is not a = large=20 safety margin, retest. They end up with numbers that measure their = safety=20 margin.
 
So I would encourage reviewing all the various failure modes of = the=20 ECM. Deliberately subject it to experiences beyond what it will = normally=20 see. Unplug each sensor, see how it handles it. Apply heat way beyond=20 normal, apply vibrations beyond normal. There are very simple ways to = do=20 this. It doesn't have to be some long drawn out thing.
 
However, statistically, we know if you have true redundancy = in=20 this particular device, then you get to multiply the probability of = failure.=20 So if the probability of shut down is 1 time in 1000 hours, since we = have=20 two with independent probabilities, our odds plummet to 1 time in = 1=20 million hours. So all you need are two independent=20 circuits.
When in doubt, just take a look at what the auto designers have = done.=20 They use more than one sensor to measure each characteristic. They = compare=20 the sensor results to historical data. They instantly recognize the = sensor=20 is providing false data, then warn you, and use tables or other sensor = to=20 keep you plugging along. That's why you don't see vehicles sitting on = the=20 side of the road.
 
Sorry for being so long winded, I have the impression that stuff = like=20 this haven't been discussed before.
 

-al wick
Artificial intelligence in cockpit, Cozy IV = powered by=20 stock Subaru 2.5
N9032U 200+ hours on engine/airframe from Portland,= =20 Oregon
Prop construct, Subaru install, Risk assessment, Glass panel= =20 design=20 info:
http://www.maddyhome.com/canardpages/pages/alwick/index.html<= BR>
 
 
On Sat, 4 Jun 2005 07:50:46 -0500 "William" <wschertz@ispwest.com>=20 writes:
Al,
What changes would be required? (= reference=20 your statement below)
Bill Schertz
KIS Cruiser # 4045
----- Original Message -----
= From:=20 al p = wick=20
To: Rotary motors in = aircraft=20
Sent: Friday, June 03, 2005 = 9:50=20 PM
Subject: [FlyRotary] Re: = Rotary=20 risks
 
You bring up very important points. If you guys can develop = robust=20 solutions for each of the challenges, then you can end up with a=20 powerplant that has some fabulous failure modes. Here is a = great=20 example, I suspect your ECM shutdown risk is now somewhere around 1= time=20 in 1000 (maybe 500) hours. But with simple changes that make = the=20 system genuinely redundant, you would automatically raise that= to 1=20 time in 1000000 hours. That is fantastic for a custom low volume=20 ECM.
 
 

-al wick
Artificial intelligence in= =20 cockpit, Cozy IV powered by stock Subaru 2.5
N9032U 200+ hours on=20 engine/airframe from Portland, Oregon
Prop construct, Subaru install, = Risk=20 assessment, Glass panel design=20 info:
http://www.maddyhome.com/canardpages/pages/alwick/index.html
----__JNP_000_381f.56ba.5c27--