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Jorgen
Unregistered
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Posted Friday, July 29, 2011 @ 03:42 AM
Fournieteers,
now we're talking! This is like Merlin the magician showing his different magic wands. I'll see if I can find my modified pistonring compressor....
May the 4's be with you/ Jörgen
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eugenio
Unregistered
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Posted Monday, August 1, 2011 @ 01:51 PM
Yes Collin, this is the tool I was talking of.
Eugenio
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Donald
Unregistered
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Posted Saturday, August 13, 2011 @ 05:36 PM
Despite Bob's statement somewhere else on this board that swapping pistons and barrels can be done in a day it took me two days plus another to refit all the other bits and pieces. In my defence I had taken the opportunity of the dismantle to refurbish many of the ancillaries so that took some extra time. I also installed a CHT gauge.
Yesterday I started my engine with it's new barrels and pistons, slightly apprehensive about what would happen. Would it overheat, would it seize, would it even start? I ran through Eugenio's test protocol recording RPM, CHT, oil temp and oil pressure at one minute intervals, though I broke the protocol into 3 sections to allow the engine to cool and to 'feel' how the engine was when turned over by hand. Maximum CHT recorded during the entire set was 145°C during the full throttle 2 minute run at the end, though most of my recorded numbers are in the 125°C - 130°C range. Eugenio's numbers gave an anticipated CHT of 180°C with a 'Do Not Exceed' of 220°C, so I was comfortably within those. Oil temperature peaked at 62°C. Running was initially a little 'rough' but evened out some as the test progressed.
Afterwards I went over the engine looking for and tightening anything that had loosened, the sump cover nuts being the most obvious slackers.
This morning while it was cold I reset the valve rocker screws, added a couple of little baffle extras and checked the oil. This afternoon I had two flights totalling 90 minutes, mostly flown at 3000 RPM, where I saw and recorded CHT and oil temperatures broadly similar to the ground test figures. One very noticeable result of the change is that the engine now runs very much smoother so I suppose my motor has being deteriorating for years but so slowly as not to be noticed.
Having flown it, next task when it's cold is to re-torque the head studs before continuing the break in, but I'm pleased with how it seems to be going and with the results so far.
Donald
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Jorgen
Unregistered
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Posted Sunday, August 14, 2011 @ 02:31 AM
WEll done Donald,
thanks for that report. The obvious question is of course: do you notice any increased "grunt" of the engine?
May the 4's be with you/ Jörgen
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Donald
Unregistered
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Posted Sunday, August 14, 2011 @ 03:29 AM
Jorgen, I've not noticed any yet but the engine is still a little tight and in any case it was not my focus during the first flights where monitoring temperatures was the name of the game.
One of the prompts for doing the work was that one side of my engine had become smokey. At first I thought it was a mixture problem or maybe an induction bias, though why that should develop I could not figure. Latterly, as well as light smoke staining I'd been seeing evidence on the starboard fuselage side and wing root of tiny oil smuts leading me to the conclusion it was oil getting past the rings and ejected through the exhausts. The old piston crowns show a markedly blacker top on the right side than the left with the front right being the blackest and oiliest. Based on plug condition and exhaust staining that pot was the prime suspect as source of the smuts.
Based on very scant evidence there are tentative signs that fuel burn might have reduced. This is not a firm conclusion but I'll monitor that as well and see what conclusions I can come to. I suppose if volumetric efficiency has been restored it should be better but it will be useful to quantify. Spreadsheets are great tools for tabulating and analysing this stuff.
I must see if I can figure out how to post pictures on this board. I think I have to upload them somewhere first and I haven't yet figured out how to do that other than to Picasa.
Donald
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Jorgen
Unregistered
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Posted Sunday, August 14, 2011 @ 04:29 PM
Donald,
I'm sure you will notice some more power at times, but as I've said before I put more trust in the long glider wings than the thrust of the engine. I've read your excellent posts about the carburator so I bet you already checked the needle seat- and you only had soil on one side, right?
For posting pictures try signing up with "Image Shack" (find it via Google). That's what I've been doing and it's not difficult. You sign up, upload your picture and copy-paste the image adress in your post. You have to delete some part of the adress which should start with [IMG] and end with [/IMG], just delete the rest before and after. Bob Grimstead wrote a thread with a checklist for how to post pictures, but I can't find it right now.
PLease keep us updated on your engine running-in.
May the 4's be with you/ Jörgen
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Donald
Unregistered
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Posted Monday, August 15, 2011 @ 03:09 AM
Thanks Jorgen,
I know how to insert the URL into a post but it was the business of getting the pictures uploaded that I was struggling with. I'm feeling my way with the wiles of FTP.
Also, I've been through and through my carburettor in the past and I'm confident it's as good as it can be given its age. I've also taken care to align the induction manifold joins to eliminate any possibility of user induced induction bias, but it was the appearance of the smuts that persuaded me I had oil getting past the rings.
OK, here is a picture of my old pots. They are in the same order as when on the plane, top of the picture is the front of the engine and left is left. Front right was the oily one:
New pistons and cylinders on the left:
Typical clamping to measure the deck height:
New pistons and cylinders on the right:
All copiously slathered in oil.
[Edit by Donald on Monday, August 15, 2011 @ 03:45 AM]
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jb92563
Unregistered
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Posted Monday, August 15, 2011 @ 10:11 AM
Love the look of shinny new pistons and cylinders!
The old ones certainly tell a story of less than optimum functioning.
It could take up to 25 hours to really get the new piston/cylinders run in so you should be seeing improving
performance for a while yet.
Statistics show that most engine failures occur near the end of an engines TBO and right after an overhaul
with many years of very reliable performance in between so it would likely be a good idea to be a bit more
vigilant for a little while.
Of course the VW always been a very reliable engine even in our aircraft so you are unlikely to have any problems
with it in any case.
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Donald
Unregistered
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Posted Tuesday, August 16, 2011 @ 03:06 AM
Thanks Ray.
The old pistons look horrific, don't they, although it appears to be surface deposits rather than erosion of the crowns. The strange thing is, though, that even like that the engine ran rather well. My only observation about its output is that the Fournier's cruise speed has been less that it used to be though the climb seemed as good as ever, but my prop has been slowly deteriorating too. Everything counts and I'm in the process of either getting a new one or having the old refurbished. Awaiting quotes.
I'm rather hoping that having posted the photo of the old pistons someone with more knowledge than I will diagnose the cause. In particular I'd like to understand the right/left imbalance. An obvious suspect would be a left-side induction manifold leak leaning the mixture on that side, but I've been over that in the past and I don't believe it's the cause.
[Edit by Donald on Tuesday, August 16, 2011 @ 03:11 AM]
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Jorgen
Unregistered
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Posted Tuesday, August 16, 2011 @ 04:00 AM
Donald,
thanks for the pictures- it makes an excellent base for discussions. I don't have any good suggestions and maybe it's a far fetched thought, but might differences in cooling (baffling) play a role? (Hotter=leaner burn)
I have to say though that judging by the pictures, your baffles look much more neat than mine.
May the 4's be with you/ Jörgen
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Bob Grimstead
Unregistered
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Posted Tuesday, August 16, 2011 @ 05:23 AM
Hi Donald,
Well done! And very meticulously accomplished, as you apparently do everything.
A couple of possible tips:
In general --
Wet black pistons/heads/plugs = high oil consumption.
Dry black pistons/heads/plugs = excessively rich mixture.
To me, your pistons seem quite dry.
Over-rich mixture on one side of the engine would also explain those slightly increased vibrations.
If there are no leaks in the left induction system, maybe there was a small obstruction somewhere on the right side, like an ill-fitting gasket, or a flap of rubber cut out of the rubber tubing by the metal tubing as it is inserted?
Or, of course, it could simply be 'just one of those things'.
Propellers:
We are getting Rupert Wasey of Hercules propellers to make us a custom RF3/4 1400 propeller.
He thinks he can provide us with even more performance than we get from our special Australian ones.
We will do some very specific test flying with a prototype or two before the final version is cast in CNC.
If you can wait a couple of months, that might be your best option.
They cost around £750.
As to posting photos on this forum, see http://sbeaver.com/cgi-bin/fournier/cutecast.pl?session=iWFbaxinVPrj2RUndKyjJ6i8pu&forum=18&thread=455
Good luck.
Yours, Bob
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Donald
Unregistered
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Posted Thursday, August 18, 2011 @ 04:08 AM
Don't be fooled Bob. I'm far from meticulous about everything I do, but your diagnostic reasoning is the same as mine and I'd already considered the possibilities you mention as well as that one of the steel induction pipes had perforated. I'll see how things develop with the new parts but I'll have to be reliant on plug condition, unless someone knows of an inexpensive borescope.
As to props, I don't think I have the same freedom of choice as those with Permits to Fly. It's either the Hoffman or the EVRA, although at some time in it's history my RF3 somehow acquired approval to use a Chris Lodge, a very good prop, though no longer available. My EVRA awaits a decision on its fate while my Chris Lodge flies. One of the Cubs in my hangar has a new Hercules prop. It looks very nice indeed but I'd like to see how that resin leading edge stands up to weather. I rather like the metal leading edge on the EVRA and the Lodge.
Jorgen, the baffles were the first parts I made for the RF3 many years ago and by and large I think the baffling is reasonably good.
Donald
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Donald
Unregistered
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Posted Thursday, August 18, 2011 @ 04:52 AM
Looking through my photographs I came across these two from 2006 which show that things were already going downhill 5 years ago. That front right muffler shows staining compared to the left side set and the right rear also shows light traces. There's also indication of the cowling fretting against the metal shield on the fuselage side but it would be another 3 years before this intruded itself firmly enough into my awareness that I began to investigate.
I suppose it's safer to have a slow degradation rather than a sudden failure but it makes the trend more difficult to spot. I don't need my glasses for hindsight, it's always 20/20.
Donald
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Jorgen
Unregistered
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Posted Thursday, August 18, 2011 @ 02:23 PM
Donald,
your meticulous Fournieresearch is getting downright eerie. The front right was the bad one on yours, eeh? Please tell me it's just a coincidence mine looked like this when I checked today:
Left side:
Maybe you have unraveled another Fournier characteristic? If so, is it related to the fact that the front exhausts seem to crack more often?
May the 4's be with you/ Jörgen
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Donald
Unregistered
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Posted Thursday, August 18, 2011 @ 03:28 PM
Spooky, Jorgen. Is this going to develop into a "Show us your mufflers" topic? But yours aren't as differentiated as mine were so if this truly is a diagnostic technique I'd say you don't have much to worry about. That said it might be interesting to take annual shots for comparison. Add it to your spark plug and compression checks but variations in fuel used might alter the appearance in the short term.
PS. if you swap yours over from right to left there will be less chance of rain entering and pooling in the mufflers.
[Edit by Donald on Thursday, August 18, 2011 @ 03:28 PM]
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jb92563
Unregistered
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Posted Thursday, August 18, 2011 @ 06:21 PM
Donald, I noticed that the ends of your muffler are crimped completely closed or is that just the perspective of the picture?
My RF4D has the tail end of the exhaust crimped down to a 1/4" wide opening.
I wonder if the extra back pressure you are getting due to the tight crimp is degrading the efficiency of the motor
and perhaps effecting the mixture balance of air/fuel since overall air flow is restricted?
Higher flow improves power I thought due to more air and the corresponding more fuel for the proper mixture.
Unequal back pressure could effect individual cylinders air/fuel mixture I think, since the airflow and hence air volume could be different.
Anyone else want to comment on the size of your exhaust crimp opening for comparison?
My RF4D had dark deposits like that after an episode of flooding and over rich condition that I have since resolved.
[Edit by jb92563 on Thursday, August 18, 2011 @ 06:25 PM]
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Donald
Unregistered
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Posted Friday, August 19, 2011 @ 01:47 AM
Ray, that's just the POV of the photograph. They're not crimped shut. Not sure it's 1/4" but it's something like that. However you do raise a point and one I hadn't previously considered. When I first got the aircraft I used to run on avgas all the time and the row of perforations were forever getting blocked with lead ash. I'll have a look with a fresh eye next time I'm out.
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Mike-RM
Unregistered
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Posted Friday, August 26, 2011 @ 03:19 PM
Hi Donald - re Bob's comment about Rupert's Hercules prop, an alternative is a Newton prop. Our 52" x 36" Newton prop has been approved by the LAA for RF3's and I'm very happy with it. I took Bob's advice on pitch with the 1400cc conversion and the general cruise performance is greatly improved without a great loss of climb performance - it's still better than with the standard prop and 1200cc. The Newton has a polyurethane injected leading edge which seems to work really well - better than a metal leading edge I think, it seems really well bonded in. The Rupert Wasey may get better performance - don't know. The Newton prop was just over £500 so may be a bit cheaper. However, as you say, the problem you are likely to have with either is permission to fit to your CofA aircraft as the Newton prop doesn't come with a Form 1, don't know about the Hercules, but you may be stick with having to use a very expensive certified prop that has already been approved on an RF3 if you want to upgrade the prop. I suspect that Vincent Pesche has a coarser pitch prop on his RF3.
[Edit by Mike-RM on Friday, August 26, 2011 @ 03:21 PM]
[Edit by Mike-RM on Friday, August 26, 2011 @ 03:26 PM]
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Bob Grimstead
Unregistered
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Posted Tuesday, August 30, 2011 @ 10:59 AM
Hi Guys,
A small point about exhaust cracks.
My experience has been that the rear pipes (the short, straight ones) crack much more frequently than the front ones, and Bobby Warren the Skyhawks engineer confirms that.
Yours, Bob
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jb92563
Unregistered
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Posted Tuesday, August 30, 2011 @ 11:38 AM
I was going to wrap my exhaust pipes with some Muffler tape I bought from aircraft spruce, in
order to help keep the under cowl temps down.
I also read that it improves engine efficiency for reasons I can't recall.
Something about the dynamics of the expanding hot exhaust gasses I think.
Does anyone think that might cause cracking problems if I do that?
My common sense tells me that insulation will slow down the expansion and contraction cycles
in the exhaust pipe and maybe reducing the stresses that cause cracking.
On the other hand the pipe will reach higher temps when wrapped because it can not transfer heat out of the metal as fast so the expansion itself may be a bit greater perhaps.
Comments?
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Donald
Unregistered
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Posted Tuesday, August 30, 2011 @ 01:00 PM
Is that Thermo-Tec? I've just read their puff on the Aircraft Spruce site and frankly I'd be sceptical of their claim that it increases power. They talk about improved scavenging but with the little short pipes we have I'd be amazed if you could measure a difference.
Also, in 15 years I've never had a cracked pipe. I replaced them long ago due to corrosion in one stub where a carb heat muff had been added, but no cracks.
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Jorgen
Unregistered
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Posted Tuesday, August 30, 2011 @ 01:14 PM
Maybe exhaust cracks are related to frequent aerobatic flying, more G's and higher power settings (=more heat)?
May the 4's be with you/ Jörgen
("Write a gubbe" Sofi suggested)
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Donald
Unregistered
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Posted Saturday, September 10, 2011 @ 01:55 PM
Update on a couple of things.
I've flown about 6 hours since changing my barrels and pistons and my fuel consumption seems to be down to under 8 litres/hour. OK none of that has been at maximum continuous cruise but it's not been just loitering about either. Compare that to my fuel consumption to and from the CFI Husbands Bosworth meet in July when I averaged around 9.5 l/hr.
I've also got hold of new, single-port cylinder heads, same part number as the ones on the plane. These are not refurbished items but are 'New Old Stock', that is they're old but have never been on an engine.
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Bob Grimstead
Unregistered
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Posted Tuesday, September 13, 2011 @ 09:16 AM
Hi Donald,
Just be careful that you've got the mixture correct for the 1400cc capacity.
Several Fournicators have told me proudly how much less fuel their 1400 engines use compared to their former 1200s, withut apparently stopping to think why.
If you are using less fuel in a bigger capacity engine you must be running leaner.
Leaner means hotter at full throttle.
Hotter at full throttle means much more valve and head stress = shorter engine life (sometimes significantly shorter if a valve head comes off).
Any engine getting a 17% capacity increase should show a 17% fuel consumption increase.
If not, it's running weak/lean.
Yes, you will save money on fuel in the short term, but it will cost you lots (including grief) in the long term.
Compare your current fuel consumption with the graph in the original Rectimo brochure/manual, and check you are using 17% more fuel, or beware!
Yours, Bob
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Donald
Unregistered
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Posted Tuesday, September 13, 2011 @ 02:20 PM
Hi Bob,
Yes but remember I have not just increased my engine to 1400cc. It's been that capacity since 1989. What I've done is maintenance not a modification.
Donald
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Bob Grimstead
Unregistered
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Posted Tuesday, September 13, 2011 @ 03:45 PM
Sorry Donald, blame a failing memory and excessive concerm for fellow Fournicators.
Yours, Bob
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Bob Grimstead
Unregistered
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Posted Monday, February 13, 2012 @ 00:03 AM
Hi again Donald, everyone,
To give you some idea of what fuel a 1400cc VW should consume in an RF4D, here are the figures for my Nordic tour:
2073nm in 29:25hrs at various power settings used 257.7 litres of fuel, giving 8.75 litres per hour (consumption 8.04nm per litre) and 70.5kt or 81mph groundspeed.
That's the whole round trip, but when I was flying downwind I throttled right back to let the wind blow me along.
Coming home all the way at high speed cruise (3,000 rpm with my propeller) took 15:20, and I burned 147.2 litres, which I make 9.6 litres per hour.
This gave me 69 knots ground speed in a variety of different winds.
I would suggest that if you are burning much less than 9.5 litres per hour you are running lean, and if you use less than 8 litres per hour you are running dangerously lean.
In the past couple of years we have had several RF4 1400cc and 1600cc engine failures immediately after take-off in very cold but dry weather because they have been using the original carburettor with the original standard main jet and needle valve, and without checking the fuel flow at the main jet or the fuel consumption to ensure they are running rich enough.
The problem is that some pilots (glider pilots especially) think that a low fuel consumption is a great thing.
But it is not. Much of the fuel you burn in an air-cooled engine is used to cool the valves and cylinder heads. All air-cooled engines should run slightly rich at full throttle or you're going to have trouble.
The engine may run fine in the summer, when the air is warm and thin, because the mixture has just enough fuel in it to provide continuous combustion.
This is the same as flying high. Your engine will run richer when the air is thinner.
But on a cold day in winter, when the air gets more dense, if you're running with the original carb & jets there may just not be enough fuel to sustain combustion.
You're OK at first, while the engine is not fully warm, but once it gets warm there just ain't enough gas to keep it going, and the engine fails at 100 or 200 feet.
If you can get past that barrier and climb to 1,500 feet say, then you'll be OK, because the air there is thinner.
But then what happens when you need to go-around after going back down to low level?
To me this is just bleedin' obvious. If you've increased the engine's capacity by 17% and its compression ratio from 7:1 to 8.2:1 (which is precisely what you do with the 1400cc conversion) you will increase power output by perhaps 25%.
And you do notice a huge difference in performance.
But you should also see 20% to 25% increase in fuel consumption, to give you that extra power.
If you don't see that fuel consumption increase, you're running lean, and that means higher internal head temperatures, a short engine life, and a high likelihood of having a valve head snap off (and then you DO have problems).
Another symptom is a loss of compression and the need to grind the valves more frequently that at 1,000-hour intervals.
If you're having to remove the heads and grind the valves because of a loss of compression after as little as 200 hours, then you're running lean.
I've said enough.
Don't blame me you lean-running guys if you have an engine failure after take-off, but if you smash up your Fournier in the process, you can expect visits from lots of angry Fournicators.
Yours, Bob
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Jorgen
Unregistered
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Posted Monday, February 13, 2012 @ 05:05 PM
Thanks Bob,
that makes sense to me and makes me feel better about XST's fuel burn, which I figure is slightly less than 10 liter/ hour. Do you think there is a risk of running too lean with the 1400 engine if you drilled up the carb inflow as we discussed in an earlier thread? Also, I "thermal loiter" quite a lot on 2200 rpm, do you think that might be unhealthy for the engine?
We still have a harsh winter here, the lakes have a 30 cm ice. I'm not complaining of course (4 hour tourskate/skatesail session today), but I think I'll let XST rest until the return of some warmth....
May the 4's be with you/ Jörgen
P.S. Reviewing the Nordic trip? May we hope for a story...? D.S.
P.P.S. A friend recently sent me a copy of that article of yours (Pilot, dec 2005; he had cleaned out his attic). It's exquisitely well written and the pictures are of the highest standard. Keep up your exemplary Fournication, will you? D.S.
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Bob Grimstead
Unregistered
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Posted Monday, February 13, 2012 @ 08:30 PM
Hi again Jorgen,
I think if you've opened out your needle valve to 2.5 mm and the main jet to around 1.3mm you will be fine.
When I get a spare half-day I shall run my 1400cc engine with the NGK AFX lambda sensor to get readings to confirm those figures, but I've been using the blue one with those jets for seven years and have had no problems.
Loitering at 2200 rpm should cause no problems at all. The engine will be nice and cool, even in the low cooling airflow of low thermalling airspeeds, because the throttle will be nearly closed. Also you are presumably fairly high, and of course the higher we go with a fixed jet carburettor, the more rich the mixture becomes. It's the sea level take-off on a cold dry day that causes most problems with a lean running engine.
PS I have submitted my Nordic trip article to Philip Whiteman at Pilot magazine and Francois Besse at Pilotes. Both say they will probbly use it 'one day'.
Christina Lindberg at Flygrevyn does not want to use it because 'it was so long ago'.
Thank you very much for your praise of my Fournier air test article. You're very kind, but I think the joint one we submitted to the on-line EAA magazine was better, partly because it was longer, so there was more information in it, but also because it was the work of several people, so had a broader information base.
I did enjoy taking the inverted photos for the Pilot article though!
Very soon Pilot should be running my more recent (but more quickly written) account of my golf course landing.
I have also submitted that to Flygrevyn (together with my piece on learning formation aerobatics).
We shall just have to wait to see whether Christina wants to use them.
Meanwhile, enjoy your ice-sailing, and let us hope that all of Europe and America have a summer of good weather this year.
Yours, Bob
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Bob Grimstead
Unregistered
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Posted Saturday, March 3, 2012 @ 11:10 PM
Hi Guys,
Very quickly, because I am going back to the airfield for more testing today, I did run HDO with the NGK AFX lambda sensor yesterday.
I made several ground runs to get the mixture right with the ram-air intake, but the most important thing is that the sensor confirms that the 1.32mm main jet I have been running gives a perfect mixture throughout the engine's rev range from idling at 1,000 rpm to full throttle at 3,000 rpm.
Matthew and I originally decided on this jet size by comparing performance climbs and spark plug colours, but this sensor scientifically confirms that our empirical conclusions were exactly right.
The full-throttle mixture is slightly richer than the max-power optimum, as it should be on all aero engines for combustion chamber cooling, with cruising power being a bit leaner for best economy.
I'll post the full results tomorrow, but if you're running a 1400cc VW engine in your Fournier and you have not opened out your main jet to 1.32mm, you can expect your engine to fail or at least not to last very long.
What you save in fuel burn in the short term will be more than outweighed by the expense of a top overhaul (or worse) in the long term.
Yours, Bob
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