Today's Message Index:
----------------------
1. 07:55 AM - Re: CJ electric fuel pump? Winter project (keithmckinley)
2. 07:57 AM - Re: GT propeller blades on V530 hubs (Rick VOLKER)
3. 08:37 AM - Re: Propellers for Yaks (Rick VOLKER)
4. 09:59 AM - Drag with MTV-9 props (Richard Goode)
5. 10:12 AM - Re: Drag with MTV-9 props (kevin kimball)
6. 02:52 PM - Re: New Digital Tach from Flight Data Systems (Craig Winkelmann)
7. 03:00 PM - Re: Re: New Digital Tach from Flight Data Systems (doug sapp)
8. 05:02 PM - MiG-23 first taxi (Jon Boede)
Message 1
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| Subject: | Re: CJ electric fuel pump? Winter project |
Hello All,
I appreciate all the feedback!
While I understand the plumbing of the CJ fuel system I don't fully understand
the plumbing associated with some of the great ideas I've seen posted. I knew
that an electric pump can replace the wobble pump but I'm not sure how some of
the systems I've seen posted work. In particular the use of the electric pump
to replace the primer as well. It seems from reading a couple of the posts that
the electric pump is switched on to allow prime which is then controlled by
a solenoid activated switch, THEN shut off after engine start unless the engine
driven pump quits.
Here's what I think I know from the posts:
The pump is installed with a primer line downstream. The pump has an on/off switch.
The primer line has a solenoid controlled by a momentary switch. Not sure
about any additional check valves, by pass etc.
Would anyone care to share a plumbing and electrical schematic? I'm sure it would
be a great asset for the list (it would be for me for sure)
In any case, thanks for sharing ll the pump info.
Cheers,
--------
Keith McKinley
700HS
KFIT
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=269820#269820
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| Subject: | Re: GT propeller blades on V530 hubs |
Kevin,
I choose to fly with an MTV9-260-29 prop on my SU26M. It has
more low end thrust, better climb rate, more vertical penetration,
and more time on vertical than the other props currently available.
Aircraft behavior during gyroscopic maneuvers such as snap rolls,
lomcevaks, flat spins, mulleroids, knife edge spins, etc. is dampened
and more predictable than with other props I have tried. This allows
more consistency and hence a lower safe altitude for the same
maneuvers. The lower power-on stall speed gifted by the static
thrust is only part of the reason for this. It is joined by an
increased braking effect. The decreased speed of this prop gives me
more time on downlines. I do not like the braking effect during the
landing phase. In the power-off, opposite-the-numbers-on-downwind
type of curving approach, most props give a user friendly glide
angle. The MTV9-260-29, even when rpm is pulled back to 70%, requires
a trickle of power. There is no brief glide at 1 inch above the
runway. It becomes more of a short field spot landing. I like the MT
large spinner for enhanced CHT cooling and appearance. I believe the
stresses on the airframe and crankshaft during extreme gyroscopic
maneuvers are lower with a 3 blade prop than with a 2 blade prop. MT
has the only proven track record in Unlimited aircraft with M14P
engines. The GT prop is about 10 pounds heavier than the MTV9. This
gives the impression of creating higher gyroscopic forces on the
aircraft. Snaps are snappier. Tumbles seem to explode and last
longer. This is great fun! But this, again, adds more stress on the
airframe and crank.
I am not suggesting that Sukhoi owners should switch to a 2
blade GT 250cm. Interesting that Jurgis Kairys apparently has
suggested that a 270cm GT 2-blade prop will almost certainly have
more static thrust than the MTV9. I do not have enough ground
clearance to try that. My reason for testing on the SU26M :
convenience. it is my aircraft and I know it well. My application
is a very narrow niche indeed. Air shows are the only use for my
SU26M. A Yak 52 enjoys much higher utility and would enjoy a prop
that is a 'jack of all trades'.
And so would Yak 18's, CJ's, Murphies and a host of other general
purpose M14P powered aircraft. The GT is a viable alternative to MT
for an owner that already possesses a V530 hub or wishes to maintain
a 2 blade vintage appearance. That is the point. Most Yak 52
owners do not do a dozen extreme gyroscopic maneuvers every day as I
do in my Sukhoi, and will appreciate the larger aerobatic envelope of
the GT 250 combined with less vibration, improved build quality, and
repairability of the design. Pitts Model 12 owners that would
aspire to fall into the Unlimited ranks would be better served with
an MT.
Many pilots(myself included) have always felt that 2 blade
props were inferior to 3 blade props for most applications. GT
propellers changed this perception. Having borrowed V530 props on
Sukhois in the past, this certainly was reinforced. After static
balancing, they exhibited much higher vibration, lower climb rate,
and lower static thrust than the 3 blade MT's. The planform of the
GT blade is much different than the V530 blade. The character of the
GT 250 blades is immediately different than the V530 blades. They
have a lower, smoother sound. They have significantly less vibration.
The static thrust is somewhere between the old MTV3 and new MTV9-
much higher than the V530. I found the speed to be as high as any
prop on my 360hp SU26M. I believe there is a valid niche for the GT
prop in high utility applications. They now have a spinner that is
the same general size as the large MTV9 spinner. It retrofits to V530
hubs. This alone may be an attractive and CHT reducing option for
V530 hub owners.
Rick Volker
On Oct 26, 2009, at 10:58 PM, kevin kimball wrote:
> Rick,
>
> A follow up question or two.
>
> Which prop do you chose to fly on your Sukhoi and why? What are
> the most important factors for you in prop selection for your M14P
> powered airplanes?
>
> For us as used on the model 12, the key selection factors are:
> Availability new, service, spinner choice, colors, appearance and
> most important, overall performance on our airplane.
>
>
> Sincerely,
>
> Kevin Kimball, Vice President
> Jim Kimball Enterprises, Inc.
> PO Box 849
> 5354 Cemetery Road
> Zellwood, FL 32798-0849
> 407.889.3451 phone
> 407.889.7168 fax
> www.pittsmodel12.com
> www.jimkimballenterprises.com
> Email: Kevin@jimkimballenterprises.com
>
>
> On Oct 26, 2009, at 10:16 PM, Rick VOLKER wrote:
>
>> In reading my original prop comparison post, you will notice my
>> "for more information, contact:". I chose not to display all
>> information due to quantity, hoping any interested parties would
>> contact me for the details. Let me fill you in:
>>
>> On September 11,2009 at KIAG airport;
>> Flight one-1300 local time: MTV3. SU26M, full fuel. Density
>> altitude 778'. Each test repeated three times during 25 minute
>> flight with test average noted.
>> Flight two-1430 local time: V530. SU26M, full fuel. Density
>> altitude unchanged at 778'. Each test repeated three times during
>> 25 minute flight with test average noted.
>> Flight three-1630 local time: GT 250 cm blades on V530 hub. SU26M,
>> full fuel. Density altitude 774'. Each test repeated three times
>> during 25 minute flight with test average noted.
>>
>> On September 15,2009 at KIAG airport:
>> Flight one-1130 local time:MTV9. SU26M, full fuel. Density
>> altitude 1037'. Altitude for tests changed to adjust for different
>> density altitude. Each test repeated three times during 25 minute
>> flight with test average noted.
>>
>> Note;
>> -Aircraft weight was identical for each flight. Oil and fuel were
>> exactly the same. The Profile for each flight was identical so
>> that the weight of the aircraft would be identical for each part
>> of the flight compared. Weather data can be confirmed via online
>> sources.
>> -Static thrust was not directly measured, however stall speed
>> tests under full power with this weight aircraft allowed gross
>> comparisons of relative thrust at close to zero airspeed.
>> Differences between aircraft were marked and statistically
>> significant.
>> -The MTV9 was dynamic balanced on this aircraft before flight.
>> Other props were not. I agree that dynamic balance performed on
>> other aircraft are next to useless. Dynamic balance of V530 prop
>> is more difficult on Yak 52 because of the proximity of blade to
>> the ground allowing buffeting to limit ground run rpm and the lack
>> of a spinner backplate for fine tuning.
>>
>> The purpose of my post was to alert Yak 52 owners to
>> a good alternative to MT if the original V530 blades must be
>> replaced or if performance enhancements are desired. The price is
>> not so expensive if you already have a good V530 hub. The MTV3 and
>> MTV9-260-29 were owned by me and do not represent all of the
>> choices in selecting a new MT prop.
>> My experience with MT has been mixed. A new
>> MTV9-260-29 prop was so rough in flight that MT eventually sent me
>> a new set of blades that corrected the problem, after 3 dynamic
>> balance attempts with 2 complete tear-downs/inspections in
>> between. But this all took one year. They do not yet know what was
>> wrong with the original new blades. I had to find other props to
>> get me through my air show season. MT did not have a loaner. I had
>> a spare MTV3. GT Propellers also offered to loan me their blades
>> for a spare V530 hub that I owned. A friend with a Yak 52 offered
>> me a 20 hr TT V530. I compared them out of curiosity. It would
>> have been much better to have an MTV9 of the proper length and
>> type blade design with a Yak 52 to compare. The MTV3 has been
>> around and many M14P pilots are familiar with them. The
>> MTV9-260-29 is an airshow-only prop that is not suited for 90% of
>> the types of flying done by Yak 52 pilots. I am satisfied with my
>> MTV9-260-29 for my application. It allows me to do things that can
>> not be done with any other prop. But you pay a price for this
>> extreme. The high static thrust comes with a loss of max and
>> cruise speeds. It also gives a crazy power off glide ratio that
>> makes for some exciting air show antics. A well known MT dealer
>> promised that his tests showed the MTV9-260-29 prop did everything
>> well. Imagine that.
>> I was so impressed by the performance of the GT prop
>> when compared with the original V530 blades, that I suggested to
>> GT that I would sell them in the US. They have built a prop using
>> the same construction techniques for a Spitfire Mk IX with
>> 1700hp. The GT blades allow the Spitfire to remove manifold
>> pressure limitations of all past designs and have been pull tested
>> to prove their strength. This suggests that GT has the know how
>> to build a prop that is strong enough for the M14P application. I
>> hope that certification is achieved soon as scientifically done
>> performance testing has been very convincing in GT's favor. I
>> will look forward to seeing more testing done by others to compare
>> the GT 250cm with the current MTV9 model offered for Yak52 V530
>> replacement.
>>
>> Rick Volker
>>
>> On Oct 26, 2009, at 2:03 PM, Richard Goode wrote:
>>
>>> I am disappointed by the lack of objectivity in Rick Volker's
>>> posting. Before anything else, and before I am accused of
>>> bias, could I make the following clear.
>>> I am a MT agent and sell a large number of MT propellers for a
>>> variety of applications.
>>> In Europe we have a significant problem of propellers, since MT,
>>> while excellent are expensive, and we can ONLY use certificated
>>> propellers. With ground strikes; old age etc we are running out
>>> of blades for our V-530s, and there simply are no other
>>> substitutes we can use.
>>> I have been a keen supporter of GT Propellers, and indeed am
>>> currently assisting them to get full European certification with
>>> EASA (our overall aviation controlling body)
>>> I have always been concerned about the safety of propellers.
>>> Some years ago I had a major failure on a propeller (not V-530/
>>> MT!) which was very nearly disastrous, and this is a fundamental
>>> reason why I am very careful about the propellers behind which I
>>> will fly, and which propellers I will recommend. There have
>>> been a number of high-profile propeller failures of non-
>>> certificated props, and, in my view, until a propeller has been
>>> properly tested AND certificated, I believe that any purchaser
>>> should tread very carefully.
>>> To deal with the statistical evidence, I re-emphasise that I am
>>> very keen for the GT propellers to perform well against the more
>>> established props. Having said that I have been involved in
>>> extensive propeller trials, and I have concerns about the
>>> following issues:
>>> Ricks figures are a single figure for each propeller and each
>>> perameter. For properly objective tests you need to run each
>>> perameter at least three times.
>>> they are not mentioned so possibly he did them, but I doubt if
>>> there were proper corrections for temperature and pressure
>>> changes, which make a huge difference to these things. I am
>>> very aware of how long it takes to contact these tests, and
>>> things can change quite rapidly, particularly during the time
>>> that it takes to change from one propeller to another.
>>> Aircraft weights need to be exactly identical - it is all too
>>> easy to contact one test; fly again, without precisely filling
>>> fuel and oil to the same level.
>>> Rick refers to "more static thrust" - I do not see any figures,
>>> so wonder whether these were properly measured.
>>> Rick refers to "dynamically balanced", but clearly these props
>>> are being removed and put back on again, in which case the
>>> dynamic balance will certainly be lost. IF these propellers
>>> were not being immediately put on, then how long and over what
>>> period were the tests being conducted, and certainly if time has
>>> been taken to re-dynamically balance each propeller, then there
>>> must have been climatic changes.
>>> It is also slightly misleading to refer to the MTV3 propeller -
>>> this is an old design, long out of production, and only likely to
>>> be available second hand.
>>> For pricing, Rick is somewhat misleading to suggest that the GT
>>> propeller is half the price of MT. He gives a price of US
>>> $8,428, but this is only for two GT propeller blades. The
>>> current list price for a complete MTV-9-250 or 260 is US
>>> $15,600. This is of course for a factory new propeller,
>>> absolutely complete, whereas the GT price of US $8,428 is simply
>>> for two blades, so you then need to get a hub; overhaul it;
>>> install the blades; balance etc.
>>> So to conclude, I am very much a supporter of GT propeller, and I
>>> am hoping that we are able to obtain full certification for their
>>> blades. BUT any performance / cost comparisons between
>>> propellers MUST be done scientifically and objectively!
>>>
>>> Richard Goode Aerobatics
>>> Rhodds Farm
>>> Lyonshall
>>> Herefordshire
>>> HR5 3LW
>>> United Kingdom
>>>
>>> Tel: +44 (0) 1544 340 120
>>> Fax: +44 (0) 1544 340 129
>>> www.russianaeros.com
>>>
>>>
>>> href="http://www.matronics.com/Navigator?Yak-List">http://
>>> www.matronics.com/Navigator?Yak-List
>>> href="http://forums.matronics.com">http://forums.matronics.com
>>> href="http://www.matronics.com/contribution">http://
>>> www.matronics.com/contribution
>>>
>>>
>>
>>
>>
>> ===================================
>> p://www.matronics.com/Navigator?Yak-List
>> ===================================
>> nics.com
>> ===================================
>> w.matronics.com/contribution
>> ===================================
>>
>
>
>
>
Message 3
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| Subject: | Re: Propellers for Yaks |
To Richard Goode,
My figures suggest that the MTV9-260-29 had the highest thrust.
The power-on stall speed with the MTV9-260-29 was not measurable and
listed as < 50 kph because the aircraft was hovering in place. While
the GT 250 would barely hover in a slip, the MTV 9 would do so in a
vertical orientation.
The MTV9 had the highest climb rate, vertical penetration, and time
on vertical, all by a significant margin over the GT250. This falls
in line with what you and Kevin have found.
My Sukhoi has the 360 hp engine. After repeated tests, the
MTV9-260-29 was slower than the V530 at max. cruise and full power
settings. I did not test other power settings. It is likely that a
400hp engine will use more of the MTV9-260-29's longer blades to
change the results toward what you have experienced. There is some
variability in actual horsepower produced my different M14P engines.
My M14P has less than 50 hr TT since new and may be producing more or
less horsepower than spec. I suspect this particular example is
stronger than average. I do not plan on dynamometer testing, so will
have to assume 360 hp.
Rick Volker
On Oct 27, 2009, at 10:48 AM, Richard Goode wrote:
> To Rick Volker - thanks for the extra figures - that makes a lot
> more sense.
>
> Certainly the figures from Kevin Kimball make a lot of sense, and
> are broadly in line with my own experience.
>
> I am however surprised that there should be less thrust from a
> MTV-260-29 than from a 250. Certainly the tests that we have
> done with MT showed that the 260 gives significantly more static
> thrust, but loses out a bit in terms of top speed.
>
> I was also interested that Rick says that the MTV-9 is slower than
> the V-530, whereas Kimball says the reverse, and again that is my
> experience.
>
> The practicality is that the V-530 is fifty year old technology,
> and obviously things have moved on.
>
> Richard Goode Aerobatics
> Rhodds Farm
> Lyonshall
> Herefordshire
> HR5 3LW
> United Kingdom
>
> Tel: +44 (0) 1544 340 120
> Fax: +44 (0) 1544 340 129
> www.russianaeros.com
>
>
Message 4
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| Subject: | Drag with MTV-9 props |
MT assume that people who buy these props are using them for aerobatics,
so they have the fine-pitch stop to allow the propeller to go very fine
when the throttle is pulled back.
This causes a lot of drag, but it is deliberate.
If people do not like it, it is very easy to adjust the stop to reduce
the drag!
Richard Goode Aerobatics
Rhodds Farm
Lyonshall
Herefordshire
HR5 3LW
United Kingdom
Tel: +44 (0) 1544 340 120
Fax: +44 (0) 1544 340 129
www.russianaeros.com
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| Subject: | Re: Drag with MTV-9 props |
RIchard,
We have found the prop drag useful on approach too. The model 12 can
have the throttle fully closed on downwind before turning base and use
the prop to control the glide path/decent rate until in the flair when
it is pushed full flat and really slow the airplane for touchdown.
Very cool feature.
Sincerely,
Kevin Kimball, Vice President
Jim Kimball Enterprises, Inc.
PO Box 849
5354 Cemetery Road
Zellwood, FL 32798-0849
407.889.3451 phone
407.889.7168 fax
www.pittsmodel12.com
www.jimkimballenterprises.com
Email: Kevin@jimkimballenterprises.com
On Oct 28, 2009, at 12:31 PM, Richard Goode wrote:
> MT assume that people who buy these props are using them for
> aerobatics, so they have the fine-pitch stop to allow the propeller
> to go very fine when the throttle is pulled back.
>
> This causes a lot of drag, but it is deliberate.
>
> If people do not like it, it is very easy to adjust the stop to
> reduce the drag!
>
> Richard Goode Aerobatics
> Rhodds Farm
> Lyonshall
> Herefordshire
> HR5 3LW
> United Kingdom
>
> Tel: +44 (0) 1544 340 120
> Fax: +44 (0) 1544 340 129
> www.russianaeros.com
>
>
Message 6
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| Subject: | Re: New Digital Tach from Flight Data Systems |
As of 28 October 2009
We have tested and confirmed that two T-30 Tachometers can be driven
simultaneously from a single magneto. This will allow installation of
a second tachometer in the rear instrument panel if desired. We have
also completed the software upgrade to allow a user setting for 9
cylinder engines.
We will have production units available to ship next week.
Thanks for your patience,
Charles Newman
Flight Data Systems
346 Keokuk Street
Petaluma, CA 94952
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=269905#269905
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| Subject: | Re: New Digital Tach from Flight Data Systems |
Craig and all,
I have also asked him to modify his enclosed install instructions to reflect
the installation of a second T-30 in the rear pit.
Always Yakin,
doug
On Wed, Oct 28, 2009 at 2:51 PM, Craig Winkelmann <capav8r@gmail.com> wrote:
>
> As of 28 October 2009
>
> We have tested and confirmed that two T-30 Tachometers can be driven
> simultaneously from a single magneto. This will allow installation of
> a second tachometer in the rear instrument panel if desired. We have
> also completed the software upgrade to allow a user setting for 9
> cylinder engines.
>
> We will have production units available to ship next week.
>
> Thanks for your patience,
>
> Charles Newman
> Flight Data Systems
> 346 Keokuk Street
> Petaluma, CA 94952
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=269905#269905
>
>
--
Maybe life is not the party that we were expecting,
but in the mean time, we're here and we can still dance....."
Douglas Sapp
Doug Sapp LLC
18B Riverview Road
Omak WA 98841
PH 509-826-4610
Fax 509-826-3644
Message 8
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| Subject: | MiG-23 first taxi |
As there are some people who seem to be curious about the Cold War Air Muse
um's MiGs... a minor update. Got it started and taxied it today.
Gas to start MiG-23: $250
Crane to pull MiG out of the mud: $381.05
Teasing the driver for the next two weeks: Priceless!
( I was not the driver ) Despite being about 28=2C000 lbs=2C the MiG-23 us
es a pneumatic braking system that y'all would be COMPLETELY familiar with.
Apparently they didn't fully charge the nitrogen system before going out
for a spin.
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