Scott, I don't want  to offence you, please understand me right,  just as a 
joke :-)
Your problem is too much knowledge, you probably know that story about 
scientists, all the people 
spend their time to demonstrate that the mission is impossible, but one who 
didn't know about
just did it successfully :-) 
We know the difference between REAL aero engine and auto conversion, of course 
you are right, it is not
correct to compare mileage in the car with flying hours. There are many 
different thin points, but the main conclusion,
they works and works nice, in our small experimental planes of course. 

BR,
Alex

-----Original Message-----
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf Of 
Scott Cable
Sent: Wednesday, January 14, 2004 6:06 AM
To: KRnet
Subject: Re: KR>Auto engines-vs Aero Engine Manifesto


Dave,
Not trying to come across with anything likened to
hostility...  Please read the whole thread on these
issues, It goes back for almost a week now....

  I've decided, because this issue seems dear to so
many out there, to write a Aero Engine vs. Auto Engine Manifesto of sorts, I 
plan on formatting this document on a part by part comparison of the 
differences between the 2 types of engines, and how those differences 
dramatically impact us, the KR builder community.

  In short, to reply directly to your comments Dave:
When you are comparing the automobile engine
application to an Aero engine application, you must
consider the differences in environments that these
engines are: designed for, fabricated in and operate
in.
  Comparing mileage that's allegedly "trouble-free" is
of no importance, because:
1. It doesn't have to operate in the same operating
conditions. and

2. The impact of the engine failing while in service
is without the life threatening, dire circumstances or predicament that an aero 
engine faces. i.e. If the auto engine fails, the operator coasts to the side of 
the road. Systems like redundant, independent ignition systems are a minimum 
safeguard for a powerplant used in this context.

  Now for the rest of the KRNetters who have been
following this over week-long thread on Engines, I
know many of you are just chomping at the bit to hit
the Reply key.  Please resist the temptation to do so,
and be patient, as I am woking on this document fairly dilligently.  The reason 
why I have decided to take on this task is in hopes that with my experience and 
background will benefit this community.
  I also feel that I am somewhat? qualified to do such
a task because:
1.) I served as an US Army Helicopter:
     a.) Turbine Engine Mechanic
     b.) Crew Chief
     c.) Flight Test Mechanic
     d.) Aircraft Systems Technician
2.) I served as an US Army Fixed Wing:
      a.) Crew Chief
      b.) Maintenance Platoon Sergeant
3.) After the Service I was:
      a.) Heavy Duty Line Mechanic
      b.) Cylinder Head Machinist
      c.) Race Engine Builder
4.) After I finished my Degree I worked in:
      a.) Hydraulics, Rotors and Controls at MDHC
      b.) Controls Design on the MD520 Notar, MDX - 
          MD900 Explorer at MDHC
      c.) Aircraft Structural Design on the Swearingen
          SJ-30, including the engine installation.
      d.) Aircraft Jet Engine Design, PW4000.  I
          designed a Hollow Titanium First Stage
          Compressor Blade for the 777 (48,000 thrust
          engine) 
       e.) Aircraft Structural Design on the F/A-18
           C,D, E & F models, Main Landing Gear Pod 
           Redesign Team on the C-17.  Horizontal 
           Redesign Team for the C-17. McDonnell
           Douglas Phantom Works Design Engineer.
        f.)Powertrain Design engineer for GM
           Powertrain's High Feature V-6 engine.
        g.)Senior Project Engineer for 2nd & 3rd Row
           Seating for the Trailblazer, Envoy and 
           Bravada Program.
        h.)Lead Structural Design Engineer for Boeing
           Integrated Defense Systems back in Phantom 
            Works.
Considering that I have worked pretty much every
conceivable perspective of this topic.  I'm probably,
maybe just a little qualified to author such a
document? If not, is there another individual who
would be willing to take on a task of this magnitude?


--- David Lininger <kb0...@positech.net> wrote: 
We drive our cars up and down mountains with single
ignition systems and don't think anything about it,
but put that same engine in an airplane at the same
altitude and we think we need dual ignition. 

=====
Scott Cable
KR-2S # 735
Wright City, MO
s2cab...@yahoo.com

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