KR> Tip tanks

2011-10-19 Thread laser...@juno.com
Outboard tanks, tips or not, increase the structural ability of the wing
to handle sudden increases in lift.  Tip tanks, if canted like the later
310's for instance, are thought to decrease tip drag.   

The KR wing is strong enough that carrying fuel in the tips isn't
relevant for strength issues, to my mind.  And disturbing the tip vortice
is more easily done than by building a fake tank.  

If someone wants to do it though, why not?  Potential imbalance issues
can be provided for easily.  

Mike
KSEE



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KR> Fly your KR

2011-10-19 Thread Mike Sylvester

I sent this to the net a few days ago and it never came back, I'm sending it 
again. Sorry if you get it twice.
Hey Guys, If your needing a flyin destination this weekend ? SERFI is this 
weekend in Evergreen Al. A great place to be Saturday. Our Birmingham EAA 
Chapter will be working it again this year. See ya there.

Mike Sylvester 
kr2s builder 
Birmingham,AL.

Cell no.205-966-3854  


KR> 6 year anniversary

2011-10-19 Thread joe.kr2s.buil...@juno.com
Hey Guys,Today is the 6 year anniversary of the first flight of 357CJ with the 
3100 corvair. I was hoping to get a morning flight in to celebrate but heavy 
rain, strong winds, and ceilings lower than a snakes belly all went against it. 
Anyway it has been some of the best 6 years of my life, I have a total of 646 
hours and over a 1000 landings. I have flown around 80,000 miles (645 x 125 
mph). I have had a few hick ups but never gave up. I feel this is the 
privileged life, I don't need Warren Buffets means to have it all, Great 
friends, great travel, great opportunity to share with my kids, Great plane and 
engine that started it all. I stood in the hanger the other day after a flight 
and just said out loud "I love my plane" There is so much fun out there 
to be had. Get out in that shop today, file something, cut something, glue 
something, assemble something, anything-- one part at a time and all of a 
sudden one day you look around and there aren't any more parts left over but 
there is a magic carpet sitting there in what ever form you had imagined it to 
be. It will be great! it will be beautiful! It will be your ride into a whole 
new world. Be brave and bold, move forward today.Joe Horton,Coopersburg, Pa.

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KR> Tip tanks

2011-10-19 Thread Fred Johnson
Scott wrote:



I can tell you for a fact that a 60 lb imbalance between tanks with them
located at the inboard end of the wing panels is quite significant. I tested
that condition in my KR. I'd sure hate to have to try to land a KR with a 60
lb imbalance at the wing tips. 

 So I'll ask the question a bit differently. Other than the coolness factor
or asthetic look of tip tanks, what would be the motivating factor for
moving fuel farther outboard in the wing where it can create a potentially
fatal imbalance condition when there is adequate space to build tanks where
it can be safely carried closer to centerline? Perhaps I'm just a bit thick,
but I don't see the advantage.

[Fred Johnson] 

Scott, there are two reasons I have considered it besides the extra fuel.
One, as Pazmany pointed out in his book, safety. The farther away from the
occupants fuel is, the less likely it will be an issue if a crash were to
happen (excluding, as you have pointed out, being the cause of an accident).
Second, is tip tanks have two other advantages; wing tanks increase the
effective aspect ratio, and two, they reduce wing tip vortices and hence
reduce drag, much like a winglet does.

So, besides being able to add more fuel, we have increased the wings
efficiency.

I'm not saying it doesn't have it's draw backs, I'm just curious as to
everyone's comments and experiences with them. also, the T33/ F80 had wing
tanks, and the few pilots I have know who flew them didn't indicate any
issues with them? perhaps I'm wrong?

I can forward a PDF copy of Pazmany's book if you want?

Fred Johnson
Reno, NV



KR> Tip tanks

2011-10-19 Thread Jeff Scott
I can tell you for a fact that a 60 lb imbalance between tanks with them 
located at the inboard end of the wing panels is quite significant. I tested 
that condition in my KR. I'd sure hate to have to try to land a KR with a 60 lb 
imbalance at the wing tips. 

 So I'll ask the question a bit differently. Other than the coolness factor or 
asthetic look of tip tanks, what would be the motivating factor for moving fuel 
farther outboard in the wing where it can create a potentially fatal imbalance 
condition when there is adequate space to build tanks where it can be safely 
carried closer to centerline? Perhaps I'm just a bit thick, but I don't see the 
advantage.

 Jeff Scott
 Los Alamos, NM

- Original Message -
From: Fred Johnson

 Lastly, I haven't read any accounts of the Pazmany aircraft who use only wing 
tanks of having the same issue as the twins? Not to mention that we are talking 
about roughly only 60 pounds of fuel in each tank, though on a KR that might 
seem like a lot. Fred Johnson Reno, NV


KR> Tip tanks

2011-10-19 Thread Fred Johnson
Jeff wrote:



"As Victor points out with the Cessna twin tip tanks, they may look cool,
but they come at a pretty high cost to safety. Carrying tip tanks gives you
the capability whether by accident or by mechanical failure to have the
lateral balance so far out that the plane becomes uncontrollable at slow
speed. Why create a safety problem when the same volume of fuel can be
safely carried either in the wing stub, or the inboard section of the outer
wing panel? Part of the flight testing on my KR included slow flight and
landings with one wing tank full and the other empty. I designed the tank
loads specifically to ensure the plane was always controllable regardless of
the fuel load and configuration. Even with my wing tanks located at the
inboard end of the wing panels, it doesn't take but a few gallons of
imbalance for the plane to start to fly wing heavy towards the fuller side.
"


I agree, if that is your only fuel source, but if it's used as additional
fuel source for long range flights, and the fuel is transferred to your main
tanks, or burned directly. Also, so they drain simultaneously, you can run
both tanks to a single pump to be used directly by the engine or to transfer
to the main tanks. Most likely it would be easier to just burn the fuel
directly. 

Lastly, I haven't read any accounts of the Pazmany aircraft who use only
wing tanks of having the same issue as the twins? Not to mention that we are
talking about roughly only 60 pounds of fuel in each tank, though on a KR
that might seem like a lot.

Fred Johnson
Reno, NV



KR> Tip tanks

2011-10-19 Thread Bob Glidden
. Creating conditions to get you an unrecoverable spin or an uncontrollable
wing heavy condition at landing speed are things that can get you killed.

 Jeff Scott
 Los Alamos, NM


Jeff is spot on here. Just think if they had only three gallons each and for
our purpose fuel weighs in at 6 LBS a gallon. If your fuel don't transfer
out of one tank you got 18 lbs sitting on the wing tip. When you get slow
the plane is going to be like a teeter-totter. On final is not the place to
practice spin recovery. I don't care how good you think you are it only
takes one time. Some of the best pilot of our time are no longer with us
because of one mistake why increase our odds. Build smart...fly safe..



KR> Tip tanks

2011-10-19 Thread Jeff Scott
As Victor points out with the Cessna twin tip tanks, they may look cool, but 
they come at a pretty high cost to safety. Carrying tip tanks gives you the 
capability whether by accident or by mechanical failure to have the lateral 
balance so far out that the plane becomes uncontrollable at slow speed. Why 
create a safety problem when the same volume of fuel can be safely carried 
either in the wing stub, or the inboard section of the outer wing panel? Part 
of the flight testing on my KR included slow flight and landings with one wing 
tank full and the other empty. I designed the tank loads specifically to ensure 
the plane was always controllable regardless of the fuel load and 
configuration. Even with my wing tanks located at the inboard end of the wing 
panels, it doesn't take but a few gallons of imbalance for the plane to start 
to fly wing heavy towards the fuller side.

 Additionally, while most pilots don't spin their KRs, the enertia of a load of 
fuel mounted at the outboard end of the wing will make spin recovery 
significantly more difficult.

 These are very real safety issues with tip tanks. Creating conditions to get 
you an unrecoverable spin or an uncontrollable wing heavy condition at landing 
speed are things that can get you killed.

 Jeff Scott
 Los Alamos, NM


KR> Tip tanks

2011-10-19 Thread velocityo...@yahoo.com
I have about 500 hours in Cessna 421's and 414's as well as a lot of time in 
310's. In all of these there is a fuel pump in the aft end of the tank that 
moves fuel from the front to the back of the tank where the pickups are. These 
pumps run all the time. These are the main tanks on all of these airplanes ie 
you takeoff and land on the tips. 
In these aircraft loosing a pump means you will loose an engine on that side as 
soon as you pitch down. 
In all but especially in the 421 loosing a tip tank fuel pump means terminating 
the flight. You can crossfeed for a while until you run out of aileron. More 
than half of all crashes in the 421 have been from fuel starvation while having 
plenty of fuel onboard. 
Bottom line, they look great, they work great. However there MUST be a method 
of transferring fuel between the two rather than an equalizing tube. The reason 
is that should you have an unequal fuel flow and correct it with aileron you 
won't know you are in trouble until you slow down and discover that you don't 
have enough aileron. 
Victor Taylor
Irvington, Alabama

Sent from my iPhone


KR> tip tanks

2011-10-19 Thread David Mullins
I liked the looks of tip tanks and have some
fake ones made them to go onto my wings.

Dave Mullins
Nashua, NH


Fred Johnson wrote:
> Rudi wrote:
>
> "Sakkie's plane with tip-tanks, ZS-UKU, is currently being restored after 
> standing for many years, more information available here: 
> http://www.avcom.co.za/phpBB3/viewtopic.php?f=100=79408[Fred Johnson] "
>
>
>
> This is great. I have been reading Pazmany's article about the PL-1 and it
> got me thinking about this on a KR. According to him, they increase wing
> efficiency the same as winglets. They also increase the aspect ratio.
>
> Does anyone know if his tip tanks actually held fuel?
>
>
>
> Fred Johnson
> Reno, NV
>
>
> ___
> Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
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>
>   



KR> POT OHM OR K?

2011-10-19 Thread John Martindale
Well actually Jeff, the current in the circuit stays the same. Refer

http://www.allaboutcircuits.com/vol_1/chpt_5/2.html

The brightness is a function of power (watts) which equals volts times amps.
Since amps remain the same, a resistor/rheostat drops the voltage across the
bulb thus dimming it. The associated voltage drop across the resistor times
the amps equals the watts that the resistor must give off as heat. The sum
of the voltage drops must equal the voltage of the battery (12volts).

In summary, electrons out of a battery terminal equals electrons in at the
other. Those little fizzers have to go somewhere :-).

John Martindale
29 Jane Circuit
Toormina NSW 2452
Australia

ph:61 2 6658 4767
m:0403 432179
email:john_martind...@bigpond.com

-Original Message-
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf
Of Jeff York
Sent: Wednesday, 19 October 2011 2:46 AM
To: KRnet
Subject: Re: KR> POT OHM OR K?

Ok, It has been a long time since I was in Electrical Engineering 101.
.snip