hi jeff did you upgrade from a 1835 by any chance just wondered how much
extra power you gained
p
----- Original Message -----
From: <jeffyor...@qx.net>
To: "KRnet" <kr...@mylist.net>
Sent: Tuesday, November 22, 2005 10:35 PM
Subject: Re: KR> Geared vs direct drive Turbo & my 2 cents


> I love this subject and have contemplated turbo charging my 2180 for quite
> some time. I feel I have extensive knowledge of turbo charging systems as
I
> have done extensive amounts of turbo and turbo engine work on automobile
> applications.
>
> However, and not to slight anyone here, I don't think I would ever
consider
> taking a turbo from one application and believe I could bolt it to my VW
> 2180 or a Corvair engine and expect success.
>
> I cut my teeth in turbo experimenting with automobiles. I will also credit
> much of the knowledge I gained came from many individuals involved in the
> Shelby Dodge Auto Clubs. Here is what I learned. Or, I could just cut to
the
> finish and suggest that if you  want to turbo your airplane, start with a
> proven turbo and engine application and then make minor modifications as
you
> need. But back to what I learned.
>
> With a turbo several things are critical to it's success.
> I would say that the most important is proper air fuel ratio delivery and
> the ability to monitor that. In an aircraft , this would be highly
critical.
> I think more engines blow up ( turbo or normally aspirated) because they
get
> to a lean mixture condition. Adding a turbo makes this even more of an
> issue. For that matter, anything that increases horsepower makes fuel
> delivery very important. So, fuel injection would be my choice over a carb
> on this subject. I would also install an air fuel meter.
>
> You would also need to deal with the great deal of increased heat that a
> turbo creates. Both to your oil and probably even your air fuel mixture.
> Cooling the air fuel mixture can be done with and intercooler. The
increase
> in oil temps would be a challenge to your oil cooler and oil delivery
> system. You may also need to deal with the fact that when you shut off the
> engine, all that hot oil from your turbo will drain down to your engine ,
> thus increasing oil temps after shut down. The most reliable automotive
> turbo's use both oil and engine coolant to keep the turbo cool.
>
> You also need a reliable way to regulate the waste gate. Or in other words
> you have to be able to keep the turbo from overboosting. Again, I believe
> you need to monitor this with a guage. If not you will never be able to
keep
> head gaskets on your engine. You would also burn holes in the tops of your
> pistons, burn valves and so on and so on. Speaking of valves, my
experience
> leads me to believe that you would need to change the exhaust valves on
your
> engine as well , in order to deal with the increased temps of combustion.
> This goes back to the idea of starting with a reliable engine turbo
> combination.
>
> I could go on and on with the subject of turbo charging. I would also say
> that I think it is the cheapest and best way to get more ponies and torque
> out of an engine. I also would guess that there are people on this list
that
> know 10 times more then me on turbo charging. But I qualify my information
> with the years I spent experimenting with turbo in automobiles and that I
> was able to take a 2.2 four cylinder engine of 140 horsepower and develop
a
> reliable dyno tested 360 HP with incredible amounts of torque. But, I did
> this using a tried and tested engine and turbo combination. I was able to
> take advantage of computerized controls for fuel delivery and waste gate
> controls. I was able to write my own computerized fuel tables and timing
> curves to assure air fuel mixture at various RPM ranges. This was all done
> via Engine ECU and interfacing a laptop computer. And the whole system
seems
> a little complex for a KR2. I also need to mention that I struggled with
all
> the items mentioned above. No big deal when on the ground ( ok maybe a few
> towing bills and head gaskets and parts and such) but I sure wouldn't want
> to have those issues in the air.
>
> I would still like to turbo an engine for my KR2. I am still unsure of the
> best, lightest and most reliable way to do it. Maybe I will start with
some
> Rev Master turbo parts and go from there.
>
> Jeff York
> KR-2 Flying
> N839BG
> Home page  http://web.qx.net/jeffyork40/
> My KR-2       http://web.qx.net/jeffyork40/Airplane/   to see my KR-2
> Email             jeffyor...@qx.net
>
> ----- Original Message -----
> From: "hussein nagy" <nagy_ta...@yahoo.com>
> To: <brokerpilot9...@earthlink.net>; "KRnet" <kr...@mylist.net>
> Sent: Monday, November 21, 2005 7:40 PM
> Subject: Re: KR> Geared vs direct drive
>
>
> > Hello, Colin,
> >   I always enjoy you comments on subjects, I am an observer to the KRnet
> , I bought a KR2 Boat with retractable gear and tail dragger,  I  have no
> experience of  building A/C but opinion of experienced  folks count, Now
let
> ask you , I have the wing center Old aerfoil  RAF48, Do you think the new
> aerofoil is woth it at this stage of the  built, and changing to fixed
gear
> better than the retract fo KR2, when  the new aerfoil instaaled do you
think
> that the elevator and the rudder  will be resized.  would like to know
your
> opinion,
> >   Best regards
> >   Nagy
> >   Jacksinville, Florida
> >   904-543-8183
> >
> > Colin Rainey <brokerpilot9...@earthlink.net> wrote:  Netters
> > This  debate about best engines for experimentals, and whether to turbo,
> whether to Gear drive/PSRU or direct drive has been going on for a  while
> now, and I suspect will probably continue, kind like the  Ford/Chevy
debate
> (Chevy is best, LOL ). I am NOT going to take sides  of whether a builder
> should choose auto or aircraft engine, normally  aspirated or turbo, or
> direct drive or PSRU. All these things are in  the archives, and found in
> literal volumes in other writings, both  Internet and books like, "Auto
> Engines for Experimental Airplanes" by  Robert Finch, just to sight one
> example. There are many others.
> >
> > What  all Netters, especially you new members need to take to heart is
> that  engine selection is VERY important. Looking at certified aircraft,
you
> will see that it it the single most important factor when considering  an
> aircraft's present value, how many hours on the engine. Of all the
expense
> of owning an aircraft, once it is completed, the most money you  will
spend
> will be for the engine, and its up keep/maintenance. Turbo  charging is
the
> cats meow for cheap horsepower, but just ask Orma  Robbins about how this
> "enhancement" comes with its own unique set of  problems to deal with and
> overcome. Also, the article sighted states  that turbo charging generally
> adds at least 50% more power. This is out  right fiction! The best that I
> have seen proven by dyno runs is  approximately 40%, and this is with
> associated engine modifications,  AND the use of an inter cooler, which is
> not mentioned in the article  at all. B&M, Vortech, Banks Turbo-charging,
> and Paxton all report  similar
> >  values for their "bolt-on" systems. I am not saying that a  turbo or
> supercharger cannot add 50% or more power, but that rather  that bolt on
> systems do not give that kind of increase, and do not want  builders
running
> out and buying a turbo for their engine expecting to  get a 50% increase
in
> power and torque by just hacking the exhaust in  order to add the turbo.
> >
> > The same rules hold true for direct  drive vs PSRU. There are definite
> benefits to a PSRU, but to set one up  on a 2.2 to 1 reduction, just to
> achieve maximum horsepower from an  engine from a dyno run, and say that
is
> best does not take into account  all phases of flight for the engine, only
> take off. That is the only  time you will use max power. This amount of
> reduction although it makes  the max power available according to the
dyno,
> it does not allow for a  reasonable rpm for cruise. This is because the
prop
> will be slowed to  2000 to 2100 rpm, which begins putting it below its
> cruise efficiency  speed. Just compare certified props that are made to
run
> in this range  of rpms. They produce max thrust at near redline, and
produce
> best  cruise thrust at 75 to 80% engine power. This puts the prop at
around
> 2300 to 2400 rpms on a 2750 redline. This puts the engine in the re  drive
> at 5060 rpms for the 2300, and 5280 rpms for the 2400 rpms at the  prop.
Now
> your engine is running
> >  just like the Rotax family of engines  and can expect the same life, or
> simply 50 to 100 hour maintenance  intervals with a major a max of 500
hours
> out. It also makes the  combination "peaky", where basically you spend
> literally all your time  at or near peak rpm.
> >
> > Robert Finch's book details a lot of  engines that have been
successfully
> used in direct drive configuration;  the Buick V8, the VW family, the
> Corvairs, and several others mentioned  in his book. In larger aircraft
that
> have more generous weight  allowances for the engine, the more complicated
> and heavier engines  have a good appeal. BUT for our applications, in
order
> to stay in the  RECOMMENDED weight range of engines AND their output,
direct
> drive  offers the best answers, and air cooled the simplest installation.
> Above all, it takes research and study to decide and engine install,  and
> talking to other actual pilots of those engines. Don't get sucked  into
the
> trap of some fancy numbers calculations and good advertising  on one web
> page where one engine is presented as the experimental  airplanes dream
> engine. There are a lot of "assumptions" and over  generalizations made at
> the expense of the builder. No quick answers  here. It takes years to
build
> a KR, take enough time to
> >  study your  engine completely BEFORE spending any money.
> >
> >
> > Colin Rainey
> > brokerpilot9...@earthlink.net
> > EarthLink Revolves Around You.
> > _______________________________________
> > Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> > to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> > please see other KRnet info at http://www.krnet.org/info.html
> >
> >
> >
> >
> > nagy hussein
> >
> > ---------------------------------
> >  Yahoo! FareChase - Search multiple travel sites in one click.
> > _______________________________________
> > Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> > to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> > please see other KRnet info at http://www.krnet.org/info.html
> >
>
>
>
> _______________________________________
> Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
>
>
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