Mailing List flyrotary@lancaironline.net Message #16878
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: P port intake
Date: Thu, 10 Feb 2005 09:21:55 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Tom, Its really fascinating (to me) the complexities of what goes on in an intake - especially with the  rotary.
 
You would be interested in the Mazda Dynamic Effect Intake (DEI).  There those Mazda engineers actually use the large magnitude pulse created in the intake by the expelling of residue exhaust gas to improve performance (when as you suggested, it would seem likely that it would hinder performance).  Basically, They send the large magnitude pulse created by the opening of the intake (and caused by the sudden bursting out of the exhaust residue into the intake) port of one rotor though the interconnected intake to the intake of the second rotor.  IF the timing is correct (rpm, porting and runner length are primary factors) then when the pulse arrives at the second port - it will arrive just as the port is closing on its compression stroke.  Normally approx. 20% of the intake charge already sucked into the combustion chamber is pushed back out by the compressing rotor upstroke before the port closes - commonly called "reversion". 
 
In any case, when this high magnitude pulse arrives at the other rotor, its dynamic energy translates into a significant increase in local
manifold pressure.  This increase is sufficient to over come most of the reversion effect (provided the timing is correct) and therefore you retain approx 15% of the 20% of the charge that would normally be lost.  The Mazda performance charts showed a 15% improvement in HP at 6000 rpm using this effect.
 
There are two induction processes that occur and it can get confusing.  There is the macroscopic movement of the airmass caused by the pressure differential as the ports open and close and there is the Finite Amplitude Wave (FAW) pulses.  The FAW pulse travel at the speed of sound and while of short duration can produce pressure in the vicinity of 10-15 psi.  They occur in both the intake and exhaust.  They can either assist the inflow of air or oppose it (and do both at differing rpms).  This is one reason why so frequently what would appear to be a good intake design does not work as expected.  The FAW pulse interact with each other and the walls of the intake unlike sound waves and undergo transformations depending on what they encounter.  Its only fairly recently that programs and home computers have reached the stage that permits their analysis on anything other than a main frame.
 
But, while there is no doubt that anything such as exhaust gas that gets ingested reduces the amount of power producing mixture, its amazing how the Mazda engineers turned what could have been a detriment into an asset.  But, if you have overlaps of intake and exhaust ports (like the 13B or a PP13B ) you will always have some exhaust gas in the intake at some rpm.
 
Ed
 
 
 
----- Original Message -----
From: Tom
Sent: Thursday, February 10, 2005 2:16 AM
Subject: [FlyRotary] Re: P port intake

That is interesting Ed.  Just thinking about it and now it would seem that the expelled residue would be the first thing that got sucked back thru a dedicated runner, also having a negative effect.

Ed Anderson <eanderson@carolina.rr.com> wrote:
Tom,
 
One reason that Jerry would not want to do that is that there is overlap between intake and exhaust.  That means while one rotor is trying to suck air in its intake port - the intake port of the other rotor may be expelling some residue exhaust gas out its intake and opposing any incoming air.  I think the engine would certainly  run but I don't think you would develop best power.  Now it would probably  be a different story with the Renesis which by moving the exhaust ports to the side housings has eliminate the exhaust/intake overlap.
 
FWIW
 
Ed A
----- Original Message -----
From: Tom
Sent: Wednesday, February 09, 2005 8:58 PM
Subject: [FlyRotary] Re: P port intake

Jerry,
Since only one rotor chamber is drawing fuel/air at any given time, why would you not feed them both from a single throttle body?
Tom

Jerry Hey <jerryhey@earthlink.net> wrote:
George, originally I was going to hook up with a piece of hose over the
butted pieces with a couple of hose clamps. That is how I will attach
the other end at the throttle bodies. But, we have been considering
welding and also building some type of flange. Certainly, for starters
I will use the hose and clamp method. Jerry





On Wednesday, February 9, 2005, at 08:43 PM, George Lendich wrote:

> Jerry,
> Is that a but weld, OR does the tube go into the  bellmouth end OR a
> flange that they both go into.
> George ( down under) 
>
> ----- Original Message -----
> From: Jerry Hey
> To: Rotary motors in aircraft
> Sent: Thursday, February 10, 2005 9:35 AM
> Subject: [FlyRotary] Re: P port intake
>
> Yes, it is 1.61 inches.
>
>
> On Wednesday, February 9, 2005, at 05:39 PM, Tom wrote:
>
> Jerry,
> Do you have an i.d. measurement for the narrow end?
>  
> TIA
> Tom
>
> Jerry Hey wrote:
>
> Today UPS brought the bell mouths for the P port intake. They are
> three inches o.d. across and have a smooth gradual taper down to the
> runner size ...
>
>
>
>
>
>
> Do you Yahoo!?
> Yahoo! Search presents - Jib Jab's 'Second Term'
>


Do you Yahoo!?
Yahoo! Mail - Easier than ever with enhanced search. Learn more.


Do you Yahoo!?
Yahoo! Search presents - Jib Jab's 'Second Term'
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster