Mailing List flyrotary@lancaironline.net Message #45090
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: RE: [FlyRotary] Re: renesis intake possibility
Date: Sat, 7 Feb 2009 17:32:29 -0500
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Hi BW,

 

My comments were not intended to discourage your use of the TWB intake, just convey my experience.  The fact that your throats are smaller in diameter may give you a much better intake velocity than I had and better performance.  Also the fact that you are putting it on a Renesis which winds to higher rpm will also help.

 

So go for it!.  You can get a rough estimate of your runner mixture velocity by taking the CFM of air flow at your specified rpm and dividing that by your Total runner cross sectional area.  It’s not a perfect approach as the air is not steady but is pulsating but it can give you an idea.  From what I have read the runner velocity should be in the vicinity of 200-300 ft/sec.  Higher than 600 ft/sec and you can choke the intake with shock waves.

 

 

 That is the nice thing about experimenting – you may find just the right combination for your installation by doing such.  I actually change my induction system around 5 times before I got exactly what I wanted.  The last change being to use two part polyurethane casting resin to mold my TB mounting/plenum (see photos).  I went from using the 5 lb Stock Mazda TB to a 10 oz mustang TB and the plastic TB mount all knocked the intake weight from 26 lbs down of 11 lbs – and it looks neater.  Yes, the runner length is adjustable for a bit of fine tunning.

 

However, the increase in performance I mentioned was based solely on the change in intake – I did not convert from the 2.17 to the 2.85 gear box for another several years. 

 

However, now that you mention it, the conversion from 2.17 to 2.85 was exactly the last major configuration alteration that made my somewhat heavy RV-6A into a much stronger performer in the take off and climbs out regime.  It helps top speed a couple miles per hour but the major significance was in the low end performance.  My static went from a decent 5200 rpm to 6000 – 6200 rpm even with the larger 74x88 prop.  The result of off loading the engine – of course, there is much more torque at the prop end but the prop is turning slower.  That pretty much mandates a large diameter prop since you have the torque to turn it.  And the prop theory indicates that slower turning larger diameter props are more efficient at converting rotation motion to thrust.  In fact, I have so much “P” factor/Torque/Wind whirl that I do not have sufficient rudder at WOT until around 40 MPH.  So it’s either keep tapping the right brake until reaching 40 mph or else slowly ease in the throttle until 40 mph.

 

It’s also good to keep in mind that seemingly minor difference between installations can have a significant impact on results.  So unless it is an exact copy – your system is a different system and may give different results.

 

Enjoy!

 

Ed Anderson

Rv-6A N494BW Rotary Powered

Matthews, NC

eanderson@carolina.rr.com

http://www.andersonee.com

http://www.dmack.net/mazda/index.html

http://www.flyrotary.com/

http://members.cox.net/rogersda/rotary/configs.htm#N494BW

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bryan Winberry
Sent: Saturday, February 07, 2009 12:42 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: renesis intake possibility

 

Ed,

Thanks for your thoughts.

I think Tracy just spoke the other day about feeding 4 runners from 2 mains.  So, I thought that using 4 TB's and reducing from 48mm (1.65in) to 1-1/4 would avoid what you described.

Do feel that the reduction ratio had any effect on your performance?

 

Another plus with setup, is that the fuel rail is on the cold side of the engine.  Which brings up another question.  Which is better; injectors near or far from the port?

 

Discuss,

BW  

--- On Sat, 2/7/09, Ed Anderson <eanderson@carolina.rr.com> wrote:

From: Ed Anderson <eanderson@carolina.rr.com>
Subject: [FlyRotary] Re: renesis intake possibility
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Date: Saturday, February 7, 2009, 10:33 AM

Hi Bryan,

 

Welcome.  Here is my experience using a TWM throttle body (a different model than you are looking at).  Back in 1992 there was no one around that I was aware that could provide any answers to what made a good induction configuration for a flying rotary.  So I turned to the only “rotary aware” crowd around and that was those racing with rotary engines.

 

So after discussing my needs, I purchase a TWM throttle body with 4 injector positions.  It was a two throat (Webber style) design with each throat 2” in diameter.  Two injectors per port (I used MSD 32 lb/hr injectors that fit the injector holes) for a total of 4 injectors on the TB.  The TWM throttle body was then bolted to a cast aluminum  “Webber” style rotary intake manifold which then took the two TB channels and divided them into 4 (two primary and two secondary) distribution runners.

 

I estimate that the best HP I ever made with that set up was around 130-140HP.  My static rpm was 4800 swinging a 68x72 two bladed wooden prop using the 2.17:1 gear ratio.

 

I later replaced that arrangement with 4 tubes of smaller diameter (1 ¼” for primary and 1 ½” for secondary), made the runners longer in length and install the stock Mazda 3 port TB which had considerably smaller openings than the TWM arrangement.

 

I immediately picked up over 300 fpm increase in my ROC and top speed moved from 186 MPH TAS to 195 MPH TAS.

 

As I learned over the years, it became apparent that what works great for the racers turning 9000 + rpm may well suck (but may not suck very well – pun intended)  at 5000-6000 and was therefore of questionable use for aircraft.  As best I could figure out the problem, it appears that with the large runner openings and runners that the mixture velocity in the runners was very much lower than optimum.  That meant the air mass had little momentum and did a poor job of filling the combustion chambers during the short time they were open.  By going to smaller runners, the mixture velocity increased considerably and resulted in more mixture in the combustion chamber and more power.   Now if I could of somehow (using a shifting gear box?) have gotten my rpm range up into the 8000 + range, then that intake system might have been the cat’s meow – but, of course, I could never get above 4800 rpm static (and about 5400 once airborne)

 

Now the TWM Throttle body in the photo based on your description may not have the same problems as it does have a considerably smaller throat than the one I used.  I personally do not believe the use of the four throats would give you what you are looking for – however, the use of two of the throats (one module) might work.  You could always place your second injectors else where on the secondary part of the intake. 

 

Just my opinion, of course, if the price is really good, you have little to lose if it doesn’t work out.

 

I now use a $25 65 mm dia Mustang throttle body which is much lighter (and much, much cheaper) than the TWM model I purchased back over 15 years ago.

 

Good luck on your project

 

Ed


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bryan Winberry
Sent: Saturday, February 07, 2009 8:57 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] renesis intake possibility

 

Hello all,

I have a chance to purchase a TWM throttle body(see attch pic) at a very low price.  I have a couple questions for the group.

 

The inlets are 42mm (appx 1.65 in.).  Is this too big to the point that they would be incompatible with the injectors?  I plan on using 1-1/8 and1-1/4 in runners.

 

Also, the bosses are sized for Bosch, Rochestor, or Lucas injectors.  Does this necessarily eliminate my using the stock Renesis injectors?

 

This setup also would allow the use of a lightweight airbox  thus simplifying the intake system from a manufacturing standpoint.

 

Thanks in advance,

Bryan

RV7, Renesis,RD-1C,EC3,EM3 (in the pipeline I hear)

 

 

 



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