Re: KR> exhaust system - nothing left but the tailpipe!

2017-02-13 Thread Kayak Chris via KRnet
on the exhaust subject, my picture of Ken Rand original shows short
stub pipes. Obviously these take up the least real estate, and get
more heat out of the cowl.  assuming backpressure needs can be
addressed with baffles (?) whats the downside?

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Re: KR> Mole tail?

2017-02-27 Thread Kayak Chris via KRnet
How light is it?

>
> At the moment, Richard is finishing up construction of one of the
> world's lightest internal combustion powered airplanes for human pilots.
>  He meticulously designed every aspect of it.  Now he's building a
> trailer to haul it to the airport...
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KR> test - no need to reply

2017-02-27 Thread Kayak Chris via KRnet
this is test of gmail krnet subscription

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Re: KR> Mole tail?

2017-02-27 Thread Kayak Chris via KRnet
I think this lightest aircraft is not a KR. It looks to me like a
clean sheet project and I'd like to know more about it.

As to reinventing the KR, even ken rand "reinvented" the plane in a
number of way including creating the KR2, and other major and minor
developments.  many see experimental aircraft as an opportunity to
learn, as they are described in the regs, and so we try things.  You
make tradeoffs. you want less cost, you may add weight, or vice versa.

I am trying to make my project as faithful to the first KR1 as
possible but it will need to be a trigear because thats what i know
how to land best and its safer.  a good example of worthwhile
reinventing the wheel.  also, the original had a short nose due to the
c-channel engine mounting system right against the firewall. however
that necessitated the belt driven magneto which is why there is a
shelf at the top of f/w. do you really want a belt driven mag?  that
was resolved by moving the engine forward onto a traditional tubular
mount.

I may have other options including electronic ignition.  more
reinventing.  maybe I will never even build this thing to completion.
but as long as I am trying, reinventing the 46 year old(!) design will
be a part of it to some extent.

On Mon, Feb 27, 2017 at 1:33 PM, larry howell via KRnet
 wrote:
>
>  I am surprised how many late comers to the party try to reinvent the wheel, 
> use $5.00 cheaper lumber for the whole project but adds 20 lbs etc. I
>>
>> How light is it?
>>
>>>
>>> At the moment, Richard is finishing up construction of one of the
>>> world's lightest internal combustion powered airplanes

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Re: KR> books

2017-03-03 Thread Kayak Chris via KRnet
Actually, someone here mentioned Tony Bingelis blue book, and I had
never heard of him or his books. So I ordered the blue book, without
knowing about the other three. So I did benefit from a KRNet post
about these.

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Re: KR> fiber glassed fuselage

2017-03-09 Thread Kayak Chris via KRnet
why do you think the original fuselage design is not strong? I dont
recall any of these breaking except in a "hi-g landing" (crash)

> I am wondering if there have been any fuselages built that have the plywood 
> as well as fiber glass over the top of it?
> I k. now that would add weight but am curious about strength added as well.
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Re: KR> Liquid cooled VW

2017-03-10 Thread Kayak Chris via KRnet
actually, the opposite may be true. I just went through this with an
antique engine I am working with. my machinist had installed customer
provided custom aluminum pistons in a big very old liquid cooled car
engine. the clearances were too tight and they seized. I was
considering replacing my cast iron piston with aluminum and was
advised by another machinist who works with them to allow extra
clearance at the top for piston expansion. he mentioned 2 thousanths
extra above the rings. he made a piston once for a similar engine that
started getting tight when hot and that fixed it.

this is from a guy who makes his own crankshafts from steel plate!
(including twisting them)

On Fri, Mar 10, 2017 at 8:12 PM, brian.kraut--- via KRnet
 wrote:

> I know that one of the major advantages to liquid cooled engines is that
> the pistons and cylinders are made with much smaller clearances because
> the temperature of the engine stays relatively constant so less
> expansion and contraction with the different metals.
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Re: KR> fire in the engine compartment video link enclosed

2017-03-21 Thread Kayak Chris via KRnet
Tommy what did you do in those two cases?

On Tue, Mar 21, 2017 at 11:59 AM, Tommy Waymack via KRnet
 wrote:
> Good video.Reminds me of the time I saw fuel running down the passenger
> window in a 182.And oh yeah,the fuel running on to my boot in the tcraft.
> Thanks for the reminder. The video has a lot of things we don't think about
> until it is too late.Tommy W.
>

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Re: KR> Progress?

2017-03-25 Thread Kayak Chris via KRnet
way to go larry!


> I received my rebuilt rods this past week and between the overhaul manual
> and Mark Langford I was convinced I understood the correct orientation and
> location on the crank.  I installed the rods and torqued them according to
> the manual.  As nothing ever goes exactly to plan they sent me 8 cotter pins
> and I screwed one of them up.  I'll order several more with some other minor
> items I need and start to assemble the case next week so I can install the
> cylinders when they arrive.  Progress, finally..
>
> Larry Flesner

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KR> rearward engine placement

2017-03-28 Thread Kayak Chris via KRnet
hi all,  I am hoping to replicate the first KR1.   one major asthetic
change seems to be from the engine in that was mounted to two alum
channels at the firewall, allowing for short nose.  looks like about a
5" space from rear case to fw.

the magneto was belt driven and mounted high and I am sure this is why
that "shelf" exists at the firewall.

I have seen electronic ignition which populates the distributor hole
and is low profile, and think that would eliminate the magneto need. a
starter I think could go there at that shelf

anyway, just tossing that out there to try and keep the nose as short
as the original.

since todays VW engines are bigger displacement than ken's original
which I believe was quite smakll less than 1500cc IIRC, but are they
longer now too, or same case dimension?

suggestions for ignition would be appreciated as well.

thanks as always for any advice

cp

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Re: KR> In-flight Fire

2017-01-30 Thread Kayak Chris via KRnet
I never liked header tank in the KR and planned to leave it out. I
also vote to get the fuel way out in the wings. And wear a chute.


> reaffirms my decision to eliminate a header tank and put all fuel in the
> outboard wing tanks.
>
> I wish your friend a speedy recovery.
>
> Larry Flesner
>
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Re: KR> New Years day flight

2017-01-01 Thread Kayak Chris via KRnet
Thats really nice to hear Larry about your flight, maybe someday I'll
be able to say the same. As to the Toyota, we BOUGHT my wife's at that
kinda mileage if not higher, and not the least concerned about it. All
cars today last much much longer than 20 years ago (with a little
maintenance and no abuse).

On Sun, Jan 1, 2017 at 2:18 PM, Larry Flesner via KRnet
 wrote:
>
>
> I made it to the airport this morning for a New Year's day flight.  Still
> IFR on arrival so I spent time sorting through my tools and giving extras to
> the line guys.  Ceilings lifted and I got in a half hour flight.  Two low
> passes at a local grass strip and two landings back at home base.  Great way
> to start the new year.  Only downer was my truck odometer rolled  to 172,000
> when I pulled in to the driveway but it's a Toyota so it might still outlast
> my driving days.
>
> Happy New year to all
>
> How many days till Lee Summitt?
>
> Larry Flesner
> P.S.  I thing that Insta-crank at the drug store comes in pill form.  So
> crush it and dissolve in oil before putting it in the crankcase.
>
>
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KR> Fwd: New Years day flight

2017-01-01 Thread Kayak Chris via KRnet
oops, re:my last reply, gmail doesnt make it aparent the old text is
still there. testing to see if this one was cleaned properly...

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Re: KR> KR 1 project

2017-01-02 Thread Kayak Chris via KRnet
very cool!  question, I think you said it had retracts, if so where
does the nosegear retract to?

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Re: KR> KR 1 project

2017-01-02 Thread Kayak Chris via KRnet
ok no retracts, duh, shoulda gone back and looked.  ideally I'd like
to build a tri-retract, original size KR1, with engine back against
the firewall as original, and with a normalizing turbocharger. the
main retracts are easy. the nose can swing back halfway into a center
pocket (I think). as to a small normalizing turbocharger, tight
squeeze and heat issues. which is why it would most likely be added
later, in a phase two.

point being, I am happy to see some added complexity is possible with
enough thought and skill!

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Re: KR> KR 1 project

2017-01-02 Thread Kayak Chris via KRnet
what is the estimated empty weight, did he mention a number?

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Re: KR> Pitch sensitivity

2017-01-12 Thread Kayak Chris via KRnet
with all this talk about pitch sensitivity, one common mention is
using forward CG. What is up with that? My last plane really liked aft
CG (within the envelope obviously) and flew MUCH better there. What
happens to a KR at aft CG?

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Re: KR> Pitch sensitivity

2017-01-12 Thread Kayak Chris via KRnet
> Could you go into further detail about "how" it flew better with a forward
> CG than an aft CG?

Sure, the plane under normal conditions (no baggage) would require
significant up trim to unload the stick, and when pulling power, would
drop the nose unless you held onto the stick. "Lawn dart"is a
description used more than once.

Conversely, with plenty of stuff in the baggage compartment (at or
near aft CG limit), the plane seemed to "float" in balance and handled
much better and was faster to boot. A pure dream to fly.

This was discussed often. It was considered by some to be good
practice to ignore the front half of the CG envelope.

It is possible that the CG envelope was shifted a bit forward than it
should have been and in fact I spoke with someone in good authority
that the aft limit was quite conservative and flying AT the published
aft limit would in fact produce good results, and it did.



> See http://www.n56ml.com/wb/index.html for more on the KR aft CG, which I'm
> pretty sure is common to most aircraft.  This story should scare you...it
> certainly scared me!

I actually had read that last year, another well written piece and in
fact I am sure I saved it to PDF as well in my KR own knowlege base.

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