Return-Path: Received: from [24.25.9.100] (HELO ms-smtp-01-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 3075589 for flyrotary@lancaironline.net; Fri, 12 Mar 2004 08:32:34 -0500 Received: from edward (clt78-020.carolina.rr.com [24.93.78.20]) by ms-smtp-01-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id i2CDWUSn014282 for ; Fri, 12 Mar 2004 08:32:32 -0500 (EST) Message-ID: <001601c40836$31859230$2402a8c0@edward> From: "Ed Anderson" To: "Rotary motors in aircraft" Subject: Performance Report on Prototype EDDIE Manifold Report Date: Fri, 12 Mar 2004 08:30:32 -0500 MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----=_NextPart_000_0012_01C4080C.486A6AE0" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 X-Virus-Scanned: Symantec AntiVirus Scan Engine This is a multi-part message in MIME format. ------=_NextPart_000_0012_01C4080C.486A6AE0 Content-Type: multipart/alternative; boundary="----=_NextPart_001_0013_01C4080C.486A6AE0" ------=_NextPart_001_0013_01C4080C.486A6AE0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Hi Folks, Well, I have now conducted 12 ground runs with my new variable = length intake manifold. This was a prototype using some old manifold = components I had laying around for the lower manifold (see photo of = slab lower manifold). The maximum port to port length of the manifold = was restricted to 47.8" as a results of using some of these make-shift = components. My design calls for one able to extend this distance to = 51-52" which I could not do due to limited space and these components. = The turn from the my lower manifold into the block is not optimum as it = makes a 90 deg turn with no inside radius - certainly not conducive to = good airflow there.Also my throttle body plenum has less that an optimum = air path from throttle body to the runners. =20 Now with the caveats out of the way here is the bottom line. My 91 street ported turbo II has Tracy's 2.17 gearbox and swings a 68x72 = Performance Prop - this is the same set up that Tracy Crook has on his = Rv-4. My nominal static engine rpm is (not too surprising) is the same = as Tracy has reported 5200 rpm. So that is what I take as my baseline. With the variable length manifold at its full extension of 47.8" inches = (port to port) the distance from intake port to throttle body is 1/2 = that or 23.9" for those who might be wondering how I stuffed 47" under = the cowl. At that setting and with the OAT at 65F my static rpm increased from = 5200 to 5600 rpm or a 400 rpm increase. That of course equates to = approx. 200 rpm increase in static prop speed. I believe that had I = been able to extend it to 50" I would have been able to pick up another = 100-150 engine rpm. My fuel flow while the engine howled at 5600 rpm = (really had the RV bouncing and a rocking) was between 16.5 - 17 GPH. = My best estimate based on the numbers is that the engine picked up = 12-17HP. When I decreased the length of the intake from its 23.9" to = 21.4" the rpm dropped back to 5200 rpm indicating (as I would have = expected) that the shorter length raised the EDDIE RPM out of the reach = of my static rpm range. My equations indicated that assuming a 55F increase in air temp from OAT = (65F) to a manifold temp of 130F (I had previously used 180F for the = calculations but am now convinced that's a bit on the high side for the = air temp inside the intake manifold) that for the full extension of = 23.9" length, that the EDDIE RPM would occur at an rpm of 5650. This = appears to correlate well with the 5600 rpm I observed. The minimum = length of 21.4" would have an EDDIE rpm of 6500. 6500 rpm is of course = much higher RPM than I can reach on the ground (with a prop {:>)). It = appears that the 5650 EDDIE rpm was close enough to pull my static rpm = up into that "EDDIE bucket".=20 However, it was not all peaches. I had hoped that my aluminum tubes = sliding inside aluminum tubes might not require Nickel plating as I = originally planned. In the work shop the tubes slide inside each other = without any problem. On the aircraft, however, after 12 ground runs, I = noticed that the tubes were beginning to fret in places. It appears = that the pounding on these tubes caused by the DIE pulse as it races = from intake to intake is considerable, either that or perhaps the = vibration combined with the sliding action is the cause. In any case = there is fretting, the end results is that the tubes began to show signs = of unequal drag as my small 1/90 HP motor started groaning. The = rectangular tube that houses the movement mechanism also needs to be = mounted more rigid. So while I would have liked to have make a couple = of flights to evaluate the higher rpm operation before going on to the = next design, it was not to be. So although disappointed I was unable to test the EDDIE at higher rpm, = I am satisfied with the results of the prototype and plan to go to the = next stage of building with a new lower manifold with better airflow and = to lower it a bit so I can get the extra couple of inches in. =20 My initial thoughts for the next manifold is to use one of the = aftermarket IDA Webber type manifolds that I believe Paul Conner and = Rusty used. This would replace my "slab" lower manifold providing = improved airflow in that region. I believe it would also lower the = profile of the intake permitting me to add another couple of inches to = the runners. The Webber manifold I am currently using has the centers = of the tubes 90mm apart. At the top of the tubes where the throttle = body is attached is the path is also 90 mm (approx. 3.5") apart which I = believe does two undesirable things. There is insufficient room for a = good airflow route from the throttle body to each individual tube and = the manifold path is curved a tight 180 deg to round the top and connect = the two parallel tubes. My suspicion is that when the pulse starts to = round the curve this causes additional pressure on the walls of the path = in that area as the outside of the pulse is now being pushed by the = outside of the path wall to change the pulse direction rounding the = curve and going to the parallel tube for the other port. Since my air = inlet from the throttle body is in that same region, I suspect that some = of the pulses energy is blasting out the throttle body port. I believe = that may be one reason why Mazda has their manifold "round the curve" = before the throttle body opening. =20 The IDA Webber aftermarket manifold has a 120mm (4.7") distance between = its openings which would provide more room for a better airflow path = from the throttle body and a less drastic 180 deg curve for the pulse. So the bottom line is I was not able to fully test the prototype as I = had hoped and I clearly will need to have the tubes nickel plated to = hopefully prevent the fretting and galling. If anyone has one of the IDA "Webber" type manifolds, I would appreciate = it if you would provide me two measurements. =20 1. The vertical distance from the block-mating surface of the manifold = to the center of the opening of the intakes of the manifold - looks like = it might be 2-3 inches. 2. The distance from one of the rear center block attachment bolt holes = to the front surface of the front of the manifold - should be on the = order of 8-10 inches. Thanks Ed. =20 Ed Anderson RV-6A N494BW Rotary Powered Matthews, NC ------=_NextPart_001_0013_01C4080C.486A6AE0 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Hi Folks,
 
    Well, I have = now conducted=20 12 ground runs with my new variable length intake manifold.  This = was a=20 prototype using some old manifold components I had laying around for the = lower=20  manifold (see photo of slab lower manifold).  The maximum = port to=20 port length of the manifold was restricted to 47.8" as a results of = using some=20 of these make-shift components.  My design calls for one able to = extend=20 this distance to 51-52" which I could not do due to limited space and = these=20 components.  The turn from the my lower manifold into the block is = not=20 optimum as it makes a 90 deg turn with no inside radius - certainly not=20 conducive to good airflow there.Also = my throttle=20 body plenum has less that an optimum air path from throttle body to the=20 runners. 
 
Now with the caveats out of the way = here is the=20 bottom line.
 
My 91 street ported turbo II has = Tracy's 2.17=20 gearbox and swings a 68x72 Performance Prop - this is the same set up = that Tracy=20 Crook has on his Rv-4.  My nominal static engine rpm is (not too=20 surprising) is the same as Tracy has reported 5200 rpm.  So that is = what I=20 take as my baseline.
 
With the variable length manifold at = its full=20 extension of 47.8" inches (port to port) the distance from intake port = to=20 throttle body is 1/2 that or 23.9" for those who might be wondering how = I=20 stuffed 47" under the cowl.
 
At that setting and with the OAT at 65F = my static=20 rpm increased from 5200 to 5600 rpm or a 400 rpm increase.  That of = course=20 equates to approx. 200 rpm increase in static prop speed.  I = believe=20 that had I been able to extend it to 50" I would have been able to pick = up=20 another 100-150 engine rpm.  My fuel flow while the engine howled = at 5600=20 rpm (really had the RV bouncing and a rocking) was between 16.5 = - 17=20 GPH.  My best estimate based on the numbers is that the engine = picked up=20 12-17HP.  When I decreased the  length of the intake from its = 23.9" to=20 21.4" the rpm dropped back to 5200 rpm indicating (as I would have = expected)=20 that the shorter length raised the EDDIE RPM out of the reach of my = static=20 rpm range.
 
My equations indicated that assuming a = 55F increase=20 in air temp from OAT (65F) to a manifold temp of 130F (I had previously = used=20 180F for the calculations but am now convinced that's a bit on the high = side for=20 the air temp inside the intake manifold) that for the full extension = of =20 23.9" length, that the  EDDIE RPM would occur at an rpm of 5650. = This=20 appears to correlate well with the 5600 rpm I observed.   The = minimum=20 length of 21.4" would have an EDDIE rpm of = 6500.  6500=20 rpm is of course much higher RPM than I can reach on the ground = (with a=20 prop {:>)).  It appears that the 5650 EDDIE rpm was close enough = to pull=20 my static rpm up into that "EDDIE bucket".
 
However, it was not all peaches.  = I had hoped=20 that my aluminum tubes sliding inside aluminum tubes might not require = Nickel=20 plating as I originally planned.  In the work shop the tubes slide = inside=20 each other without any problem.  On the aircraft, however, after 12 = ground=20 runs, I noticed that the tubes were beginning to fret in = places.   It=20 appears that the pounding on these tubes caused by the DIE pulse as it = races=20 from intake to intake is considerable, either that or perhaps the = vibration=20 combined with the sliding action is the cause.  In any case there = is=20 fretting, the end results is that the tubes began to show signs of = unequal drag=20 as my small 1/90 HP motor started groaning.  The rectangular tube = that=20 houses the movement mechanism also needs to be mounted more = rigid.  So=20 while I would have liked to have make a couple of flights to evaluate = the higher=20 rpm operation before going on to the next design, it was not to = be.
 
So although disappointed I = was unable=20 to test the EDDIE at higher rpm,  I am satisfied with the = results=20 of the prototype and plan to go to the next stage of building with a new = lower=20 manifold with better airflow and to lower it a bit so I can get the = extra couple=20 of inches in. 
 
My initial thoughts for the next = manifold is to use=20 one of the aftermarket IDA Webber type manifolds that I believe Paul = Conner and=20 Rusty used.  This would replace my "slab" lower manifold providing = improved=20 airflow in that region.  I believe it would also lower the profile = of the=20 intake permitting me to add another couple of inches to the = runners.  The=20 Webber manifold I am currently using has the centers of the tubes 90mm=20 apart.  At the top of the tubes where the throttle body is attached = is the=20 path is  also 90 mm (approx. 3.5") apart which I believe does two=20 undesirable things.  There is insufficient room for a good airflow = route=20 from the throttle body to each individual tube and the manifold path is = curved a=20 tight 180 deg to round the top and connect the two parallel tubes.  = My=20 suspicion is that when the pulse starts to round the curve this causes=20 additional pressure on the walls of the path  in that area as = the=20 outside of the pulse is now being pushed by the outside of the path wall = to=20 change the pulse direction rounding the curve and going to the parallel = tube for=20 the other port.  Since my air inlet from the throttle body is in = that same=20 region, I suspect that some of the pulses energy is blasting out the = throttle=20 body port.  I believe that may be one reason why Mazda has their = manifold=20 "round the curve" before the throttle body opening. 
 
The IDA Webber aftermarket manifold has = a 120mm=20 (4.7") distance between its openings which would provide more room for a = better=20 airflow path from the throttle body and a less drastic 180 deg curve for = the=20 pulse.
 
So the bottom line is I was not able to = fully test=20 the prototype as I had hoped and I clearly will need to have the tubes = nickel=20 plated to hopefully prevent the fretting and galling.
 
If anyone has one of the IDA "Webber" = type=20 manifolds, I would appreciate it if you would provide me two = measurements. =20
 
1.  The vertical distance from the = block-mating surface of the manifold to the center of the opening of the = intakes of the manifold - looks like it might be 2-3 = inches.
 
2.  The distance from one of the = rear center=20 block attachment bolt holes to the front surface of the front of the = manifold -=20 should be on the order of 8-10  inches.
 
Thanks
 
Ed. 
 
Ed Anderson
RV-6A N494BW Rotary=20 Powered
Matthews, NC
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