RotaxEngines-List Digest Archive

Sun 02/10/08


Total Messages Posted: 12



Today's Message Index:
----------------------
 
     1. 05:42 AM - Re: Disappointment in Rotax 9 series (Thom Riddle)
     2. 06:09 AM - Re: Disappointment in Rotax 9 series (rampil)
     3. 07:18 AM - Re: Disappointment in Rotax 9 series (Thom Riddle)
     4. 10:31 AM - Re: Re: Disappointment in Rotax 9 series (Steve Hagar)
     5. 10:35 AM - Disappointment in Rotax 9 series (D Wysong)
     6. 01:38 PM - Re: Disappointment in Rotax 9 series (rampil)
     7. 01:56 PM - Re: Disappointment in Rotax 9 series (rampil)
     8. 02:20 PM - Re: Re: Disappointment in Rotax 9 series (Gilles Thesee)
     9. 02:24 PM - Re: Disappointment in Rotax 9 series (jetboy)
    10. 02:47 PM - Re: Disappointment in Rotax 9 series (rampil)
    11. 03:39 PM - Re: Re: Disappointment in Rotax 9 series (Gilles Thesee)
    12. 04:46 PM - Re: Disappointment in Rotax 9 series (Ivan)
 
 
 


Message 1


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    Time: 05:42:40 AM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "Thom Riddle" <riddletr@gmail.com>
    rampil, I do not know where you got your data but attached is a snapshot of the cover page from my Katana Manual and the page with the performance and fuel consumption table data. See attachments. As you can see there is nothing indicating a variance in fuel flow AT A CONSTANT POWER SETTING regardless of variations in altitude. Per my training, knowledge and experience, fuel flow is a nearly linear function of power being produced, regardless of altitude at which it is being produced. I have never had a fuel flow meter on any of the airplanes I've owned with the 912 series engine but have flown a good bit of cross country time in them at known power settings at widely varying altitudes, and the fuel required to fill the tank after these flights has always been within 1/2 gallon of my projections based on time and power setting during these long continuous power flights at varying altitudes. Also, the EGTs on my 912 read pretty constant at a constant power setting at varying altitudes. Thom Riddle Retired Mechanical Engineer FAA Certificated Powerplant Mechanic http://riddletr.googlepages.com/a%26pmechanix Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163281#163281 Attachments: http://forums.matronics.com//files/da20cruisedata_729.jpg http://forums.matronics.com//files/katanaafmcover_116.jpg


    Message 2


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    Time: 06:09:06 AM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "rampil" <ira.rampil@gmail.com>
    Hi Tom, Again, the data was for the DV-20-100 912S3 not the DA-20 912. Yes my DA-20 manual looks the same (I have about 150 hours in them) but the manual does not specify what altitude the measurement was made, and since my time was in a rental, I did not bother to try. Re the DA-20 manual, certainly you dont believe the carbs compensated up to the max altitude of 13000? Nobody I spoke every claim claimed they compensated for altitude over 8000, including Eric Tucker who I spoke to at Oshkosh 2005 at some length when he was hanging out at the CPS booth. Unrepentant Electrical Engineer AME Eastern Region -------- Ira N224XS Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163282#163282


    Message 3


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    Time: 07:18:33 AM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "Thom Riddle" <riddletr@gmail.com>
    rampil, I appreciate your bringing this increased fuel flow with increased altitude data to us. It was news to me and a bit of a surprise. The good news is that at higher altitudes you get higher TAS with a given power setting, which helps compensate for the increased fuel flow. If my current airplane were certificated experimental I would be tempted to try the adjustable mixture control (HACman) that you mentioned. But then again, most of my current flying is at low altitudes so it might not be an economical solution for me anyway. I'm happy that I can run methanol free 87 octane autogas in our 912UL and burn between 4.0-4.2 gph at 75% power. I still like the 912 series better than any other engine I've flown with. -------- Thom Riddle N221FA Allegro 2000 912UL N197BG FS1/447 -------------------- Believe nothing, no matter where you read it or who has said it, not even if I have said it, unless it agrees with your own reason and your own common sense. - Buddha Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163287#163287


    Message 4


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    Time: 10:31:49 AM PST US
    From: "Steve Hagar" <hagargs@earthlink.net>
    Subject: Re: Disappointment in Rotax 9 series
    The carbs on my Europa are almost indistinguishable from the carbs on my old BMW pushrod motorcycle. So there should be no moaning and groaning that you are not getting "altitude compensating" carbs. What you have are "constant velocity" motorcycle carbs. Those diaphrams on top of the slides keep you from opening up the bores too much for the mass of air that can flow through them and get a relatively good mixture. Supposedly to give you better or smoother throttle response when cranking it on a motorcycle. As noted before fuel consumption is directly related to hp produced. Leanable carbs only reduce fuel consumption by allowing you to keep the gas/air (oxygen) ratio proper (stoiciometric?). You can keep the throttle wide open. What you probably get with the bings is the fact at altitude the mass of air going through at altitude will not allow the diaphrams to pull the slides up all the way even though the throttle is opened up fully. The 914 shouldn't care as it should think it is at sea level to 16K I believe. Steve Hagar A143 Mesa AZ > [Original Message] > From: Thom Riddle <riddletr@gmail.com> > To: <rotaxengines-list@matronics.com> > Date: 2/10/2008 8:21:21 AMa > Subject: RotaxEngines-List: Re: Disappointment in Rotax 9 series > <riddletr@gmail.com> > > rampil, > > I appreciate your bringing this increased fuel flow with increased altitude data to us. It was news to me and a bit of a surprise. The good news is that at higher altitudes you get higher TAS with a given power setting, which helps compensate for the increased fuel flow. > > If my current airplane were certificated experimental I would be tempted to try the adjustable mixture control (HACman) that you mentioned. But then again, most of my current flying is at low altitudes so it might not be an economical solution for me anyway. I'm happy that I can run methanol free 87 octane autogas in our 912UL and burn between 4.0-4.2 gph at 75% power. > > I still like the 912 series better than any other engine I've flown with. > > -------- > Thom Riddle > N221FA Allegro 2000 912UL > N197BG FS1/447 > -------------------- > Believe nothing, no matter where you read it or who has said it, not even if I have said it, unless it agrees with your own reason and your own common sense. > - Buddha > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=163287#163287 > >


    Message 5


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    Time: 10:35:32 AM PST US
    From: "D Wysong" <hdwysong@gmail.com>
    Subject: Disappointment in Rotax 9 series
    > > Has anyone performed actual, careful engine performance flight > test. I'd like to, but my new EFIS has the output of my FloScan > bouncing all over creation to the point where it is unusable. > Hello Ira. We saw the same erratic behavior out of our FloScan and EFIS (MGL RDAC-X). The solution was to pull the signal line (white wire) up through a resistor to clean up the signal. I'll send you a sketch of the schematic if you're interested. D


    Message 6


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    Time: 01:38:55 PM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "rampil" <ira.rampil@gmail.com>
    Hi D, Thanks for the offer. Supposedly the EFIS I have has a 10k ohm pullup to the 5v rail internally. A pullup makes sense when the optical transistor inside the Floscan does not generator enough voltage swing on it's collector. I don't think that is the problem in my case, but I will check the waveform with my scope. I think my problem is that the company has a strange idea of how much digital filtering (smoothing after conversion from pulse interval to flowrate) they do to this particular signal. -------- Ira N224XS Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163338#163338


    Message 7


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    Time: 01:56:09 PM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "rampil" <ira.rampil@gmail.com>
    Steve, I think we both know what a carb is supposed to do. You are just off track when you compare aircraft to motorcycle applications. I cant think of the last time I gunned my rotax throttle at the stop line ;-) The constant "depression" in Euro-speak or constant pressure in USA English is in fact supposed to provide altitude compensation, the goal in the case of the Rotax, to run just rich of peak at all altitudes. This is the stated and advertised goal of using the Bing 64 instead of a single conventional carb. What is in fact happening is that the engine IN FACT is running richer and richer with DA when it should should reduce fuel flow to match the reduced air mass charge. As for increased TAS with DA, well you don't need a Rotax for that! A rubber band motor will do exactly the same thing! -------- Ira N224XS Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163339#163339


    Message 8


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    Time: 02:20:30 PM PST US
    From: Gilles Thesee <Gilles.Thesee@ac-grenoble.fr>
    Subject: Re: Disappointment in Rotax 9 series
    rampil a crit : > > Hi Gilles, > > I think you are an experienced thoughtful guy, but what does it mean > to have an opinion on these carburetors . On the other hand, what you told Ivan is absolutely > true from my hands on experience with both engines, > > We are not talking about health food nonsense or placebo. We must talk > engineering, these are deterministic systems, they either work > or they do not work. > > The DATA says they do not work, in fact, they perform WORSE > than just leaving full rich on a Lycoming. > > I may well be wrong due to lack of sufficient data, but the DATA > so far says the 912S3 is CONTRACOMPENSATING. > Ira, Not sure what your point is, but what I'do first is double check the printed data. Especially when they seem indicate something contrary to engine physics. > Please explain to me my error. Opinions can not count > I may have missed something, but could you provide a link to this particular manual ? > Well, unless someone can prove the following data wrong now, this > Altitude compensation is a complete crock. I'd say it the other way "unless you can prove our engines and carbs are wrong, these data you're referring to are not reliable". Best regards, -- Gilles http://contrails.free.fr


    Message 9


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    Time: 02:24:27 PM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "jetboy" <sanson.r@xtra.co.nz>
    I would like to add here that although the carbs used on the 912 are similar to those on the Jabiru, the Jabiru ones now have a much different profile needle which gives the standard Continental / Lycoming aero engine profile of leaner mixture below 75% power and progressively richer above 75%. This saves 1 or 2 litres/hr of fuel flow over the original needle profile. Above 8,000 feet the needle should not be able to enrich the mixture even at full throttle setting although I have not tested this recently. they wont be able to compensate above this altitude however the Jabiru needle keeps a much leaner mixture due to the different taper. You might consider purchasing more appropriate needles for the 912. Downloading the latest Jabiru SB-18 gives good guidance. Ralph Gilles.Thesee(at)ac-greno wrote: > Ivan a crit : > > > I have owned a 912UL for about 4 years and definitely it does not have > > an altitude compensating carburetor. As I go up in altitude I must > > allow for increased fuel usage. As I go from 2000 ft to 9500 ft I > > increase my fuel consumption by 20%. This makes sense to me since I > > am burning richer as I go up in altitude. The new LSA's have the Bing > > compensating carburetor and thus no mixture control. > > > > My Jabiru engine has the Bing compensating carburetor. As I go up in > > altitude I dont see much change in my EGT because in stead of the > > engine running richer, the carburetor compensates to keep the mixture > > the same as evidenced by a contant EGT. So I know for a fact that the > > Bing compensating carburetor works well as stated. I dont know why > > Rotax states the fuel cosumption is increasing with altitude. My > > engine does the opposite and I run most efficiently at high altitude > > on my cross countries. > > > > > > > > Ivan, > > Would you care to elaborate on the "compensating" and "non compensating" > carbs ? > As far as I could see, there is no particular difference between the > Bings 64 on the Rotax, and the Bing 64 on the Jabiru. Also, except for > the particular engine jetting, there is no apparent technical difference > between the carbs in each engine documentation : the Jabiru manual shows > the same picture as the Rotax. > > In my opinion, the Bing carb provide *some degree* of altitude > compensation due to the constant vacuum design. > > Best regards, > -- > Gilles > http://contrails.free.fr -------- Ralph - CH701 / 2200a Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163344#163344


    Message 10


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    Time: 02:47:51 PM PST US
    Subject: Re: Disappointment in Rotax 9 series
    From: "rampil" <ira.rampil@gmail.com>
    Gilles, I wish it were so simple as to have wrong data. Here is the URL you seek for your own official copy straight from Austria. http://www.diamond-air.at/dv20_afm_bas+M52087573ab0.html I refer you to page 73 in the PDF corresponding to page 5-04 on paper. -------- Ira N224XS Read this topic online here: http://forums.matronics.com/viewtopic.php?p=163349#163349


    Message 11


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    Time: 03:39:28 PM PST US
    From: Gilles Thesee <Gilles.Thesee@ac-grenoble.fr>
    Subject: Re: Disappointment in Rotax 9 series
    rampil a crit : > I wish it were so simple as to have wrong data. > Ira, Had a look at the manual. Concentrated on the 75 % power numbers. The 8000 ft numbers are in close agreement with every other 100 hp Jabiru/Rotax engine : in the 22-23 L/hr ballpark. At this altitude, 75 % power is obtained with full throttle and max allowable RPM. Nothing wrong with those data. Now at lower altitudes, one can choose between different MP/RPM combinations. The lower the RPM and the higher the MP, the lower the fuel burn for a given % output. So it is normal to burn *less* at those settings. Any atmospheric engine behaves like that. So I'd rather say : at lower altitudes it is possible to burn slightly less fuel for a given % output. At 1000 ft you also can use the 8000 ft settings. You'll burn a little more fuel because you'll be at part throttle. But at 75 % any atmospheric 100 hp engine will burn about 22-24 L/hr at 8000 ft : Lyc, Conti, Rotax, Jabiru or whatever. At 75 %, our 914 (same carbs) burns around 22 L/hr. Best regards, -- Gilles http://contrails.free.fr


    Message 12


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    Time: 04:46:59 PM PST US
    From: "Ivan" <imap8ntr@cox.net>
    Subject: Re: Disappointment in Rotax 9 series
    Gilles Supposedly the "altitude compensating carburetor" is one that self compensates for changes in atmospheric pressure and adjusts the fuel flow accordingly. Thus even without a mixture control as you go up in altitude with a constant power setting the carburetor compensates and decreases the fuel flow, thus giving the engine less fuel when there is less oxygen and thus doesnt let the mixture get rich but keeps it about constant. This has been my finding on my Jabiru 3300 since the EGT(a measure of mixture) stays about the same as my altitude is increasing. There is a little error due to different temperatures from day to day which thus a colder day with the same barametric pressure can lean out the mixture slightly as evidenced by slightly higher EGT's for that day. The carburetor ONLY compensates for air pressure and not air temperature(which indirectly may affect pressure.) And that is the way I see it as evidenced by by EGT probes. My fuel usage is basically constant at about 5.1 gal/h on cruise at 75% power (2850 RPM) on my 120hp engine. Hope this lightens things rather than confues them, Ivan Phoenix, AZ ----- Original Message ----- From: "Gilles Thesee" <Gilles.Thesee@ac-grenoble.fr> Sent: Saturday, February 09, 2008 2:43 PM Subject: Re: RotaxEngines-List: Disappointment in Rotax 9 series <Gilles.Thesee@ac-grenoble.fr> Ivan a crit : > I have owned a 912UL for about 4 years and definitely it does not have an > altitude compensating carburetor. As I go up in altitude I must allow for > increased fuel usage. As I go from 2000 ft to 9500 ft I increase my fuel > consumption by 20%. This makes sense to me since I am burning richer as I > go up in altitude. The new LSA's have the Bing compensating carburetor > and thus no mixture control. > My Jabiru engine has the Bing compensating carburetor. As I go up in > altitude I dont see much change in my EGT because in stead of the engine > running richer, the carburetor compensates to keep the mixture the same > as evidenced by a contant EGT. So I know for a fact that the Bing > compensating carburetor works well as stated. I dont know why Rotax > states the fuel cosumption is increasing with altitude. My engine does > the opposite and I run most efficiently at high altitude on my cross > countries. > Ivan, Would you care to elaborate on the "compensating" and "non compensating" carbs ? As far as I could see, there is no particular difference between the Bings 64 on the Rotax, and the Bing 64 on the Jabiru. Also, except for the particular engine jetting, there is no apparent technical difference between the carbs in each engine documentation : the Jabiru manual shows the same picture as the Rotax. In my opinion, the Bing carb provide *some degree* of altitude compensation due to the constant vacuum design. Best regards, -- Gilles http://contrails.free.fr




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