I currently fly at that altitud frequently.

----- Original Message ----- 
From: "gleone" <[email protected]>
To: <[email protected]>
Sent: Monday, March 08, 2004 4:23 PM
Subject: Re: KR>Turbocharging a KR


> I believe there's an OXYGEN requirement above a certain altitude.
>
> -------Original Message-------
>
> From: KRnet
> Date: 03/08/04 17:05:06
> To: Ron Eason; KRnet
> Subject: Re: KR>Turbocharging a KR
>
> I understand the theory and mechanics of turbocharging.
> What I don't know is if a Turbo KR can or is certified to
> fly at 17500 or higher(there is always the problem of
> aircraft limitations).
> Joe
>
> ----- Original Message -----
> From: "Ron Eason" <[email protected]>
> To: "KRnet" <[email protected]>
> Sent: Monday, March 08, 2004 3:51 PM
> Subject: KR>Turbocharging a KR
>
>
> > Here is some thoughts.
> > The Advantages of Turbo-Normalizing
> >
> >
> >
> > Normally aspirated engines suffer from reduction of manifold pressure as
> > they climb, which pilots compensate for by pushing in the throttle. At
> > about 7,500 feet the engine runs "out of throttle". As the altitude
> > increases, the manifold pressure decreases and the plane slows. Flying
> > higher becomes more and more inefficient.
> >
> > With a turbo-normaling system providing sea level air pressure for
> > combustion all the way to high altitude, the loss of power and speed is
> > delayed until reaching "the critical altitude". With the my Turbo
system,
> > critical altitude is 20,000 feet, or so. Advantageously, the air speed
> > increases as the skin friction of thinner air density decreases. High
> > altitude capability allows the pilot the choice of:
> >
> > a.. Topping the weather
> > b.. Avoiding turbulence
> > c.. Maintaining terrain clearance over mountains
> > d.. Seeking more favorable headwinds
> > e.. Catching tail winds
> > f.. More enjoyable clear air and sunshine
> > g.. Navigation and communications is better --- longer line of sight
> > h.. Obstacle clearance and mountain turbulence, generally 10,000 ft in
> the
> > East and 16,000 feet in the West.
> > i.. Safety advantage of altitude: 12,500 to 17,500 have least traffic
> > j.. Added safety in an emergency from greater glide time. Area for
> > landing increases as the square of the range
> > At 6,000' glide is about 7 minutes, 12.5 miles
> >
> > At 12,000' glide is about 14 minutes, 25 miles
> >
> > At 18,000' glide is about 21 minutes, 37.5 miles
> >
> >
> > Faster speeds mean less engine time, less avionics time and the
> probability
> > of less maintenance
> >
> > Faster speeds mean greater range with the same amount of fuel
> >
> > High flight makes available smoother ride, colder air -- less icing risk
> >
> > [ I am also using fuel injection and ECU to manage the timing and
> > pre-detonation problem.]
> >
> > That's my thoughts.
> >
> > KRron
> >
> >
> >
> >
> >
> >
> >
> > ----- Original Message -----
> > From: "joe" <[email protected]>
> > To: <[email protected]>; "KRnet" <[email protected]>
> > Sent: Monday, March 08, 2004 5:16 PM
> > Subject: Re: KR>Turbocharging a KR
> >
> >
> > > What gains, useful load; cruise spd etc does turbo give you(also
> > operating
> > > altitude)
> > > Joe
> > > ----- Original Message -----
> > > From: "Brian Kraut" <[email protected]>
> > > To: "Orma Robbins" <[email protected]>; "KRnet"
> > <[email protected]>
> > > Sent: Monday, March 08, 2004 3:20 PM
> > > Subject: Re: KR>Turbocharging a KR
> > >
> > >
> > > > Dan Diehl did some good articles on turbocharging the VW. I can't
> > > remember exactly where I saw them. I think it was in some of the old
KR
> > > newsletters that are available online. Anyone remember exactly where
> the
> > > articles were?
> >
> >
> >
> > _______________________________________
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>
>
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>
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