Mailing List flyrotary@lancaironline.net Message #23091
From: Echo Lake Fishing Resort (Georges Boucher) <echolakeresort@telus.net>
Subject: Re: [FlyRotary] Re: Rotary risks
Date: Sat, 4 Jun 2005 14:29:52 -0700 (Pacific Standard Time)
To: <flyrotary@lancaironline.net>
Ian 
I'm  in the process of adapting an outboard motor alternator attached to the drive plate, The EC-2 will have a CAS on each half. One will be retarded, it will be on with the NOS (which has a small computer that increases fuel).
Georges B.
 
-------Original Message-------
 
Date: 06/04/05 13:30:31
Subject: [FlyRotary] Re: Rotary risks
 
Hi Georges, I agree with you that there is not much chance that the shaft will break, more likely a problem with the harness going to the CAS.  Did you consider using a renesis crank trigger? or perhaps something on the flex plate?  I assume that you plan on two EC-2s if so get one with 13B code and the other with Renesis code.  Have both firing the plugs, turn the secondary injectors (second EC-2) on if you have a problem with # 1. -- Ian
-----Original Message-----
From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net]On Behalf Of Echo Lake Fishing Resort (Georges Boucher)
Sent: Saturday, June 04, 2005 3:10 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Rotary risks

Dale 
There are four problems with the "twin dizzy" cover. One there is no room for the water pump housing (you could go to EWP) Two the CAS are not a direct swap with the distributors (can be overcome). Three the cover mounting bolt position are not the same ( only one & can be fixed) & four if you wand to use oil injection you will need to adapt a 4 port pump, it comes with a 2 port with a different mounting pattern. That is the reason I'm using the double decker CAS conversion.
Georges B.
 
-------Original Message-------
 
Date: 06/04/05 08:38:42
Subject: [FlyRotary] Re: Rotary risks
 
Al Wick <alwick@juno.com> wrote:
 
> Sorry for being so long winded, I have the impression that stuff like
> this haven't been discussed before.
 
   Actually, most of the application related part has - at
various times.  A couple of weeks ago, Leon posted pictures
of a 12A front cover designed for two distributors - "Twin
Dizzies" (apparently also suitable for twin CAS units).
There's been discussion of ways to "stack" dual pickups on
a single shaft; and some other on adding a CPS/CAS on either
the flexplate or on the crank pulley.  We've long acknowledged
that an *ideal* system would have true redundancy.
 
   Then again, is this where our inventive efforts would
yield the most value, at this time?  So far, it seems that
the Mazda CAS is one of the _least_ vulnerable of the engine
management components.
 
   So far, the most fragile parts of the system have turned
out to be the intake and fuel systems.  So that is where a
lot of attention has been, of late.
 
My $.002 (.02, after 35 years of inflation)
 
Dale R.                              (___
COZY MkIV-R13B #1254          |----==(___)==----|
Ch's 4, 5, 16 & 23 in progress      o/ | \o
 
 
> From: al p wick <alwick@juno.com>
> Date: 2005/06/04 Sat AM 10:43:11 EDT
> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
> 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:
>
 
 
 
>>  Homepage:  http://www.flyrotary.com/
 
 
--
No virus found in this incoming message.
Checked by AVG Anti-Virus.
Version: 7.0.323 / Virus Database: 267.6.0 - Release Date: 6/3/2005
 
.
 
No virus found in this outgoing message.
Checked by AVG Anti-Virus.
Version: 7.0.323 / Virus Database: 267.6.0 - Release Date: 6/3/2005
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster