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From: "Tracy Crook" <lors01@msn.com>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
References: <list-868589@logan.com>
Subject: Re: [FlyRotary] Re: Rx-8 Rotors
Date: Fri, 15 Apr 2005 22:33:28 -0400
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Here's my take (FWIW as usual).  Ed's answer is essentially correct.  =
But there is another reason for the greater depth of the 2nd - 3rd gen =
apex seals.  The increased contact area in the groove is needed to =
transfer heat from seal to rotor.  So no milling down the RA seals to =
fit RX-8 rotors in RX-7 engines.  (but hell, it might work anyway). =20

Also, the center of mass of the rotor DOES rotate in a perfect circle.  =
No monkey motion is ever involved. =20

Another question was about why counter weights were required if the =
rotors ballanced each other out.  They are not in the same plane of =
rotation which creates what is known as a "rocking couple".  The =
counterweights make another rocking couple (out of phase) to cancel out =
that of the rotors.

Tracy (still at SnF)

  Hi Doug,

  Some good thoughts and questions, of which I would like to know the =
answers to as well.  I believe the reason the experts are recommending =
milling the RX-8 rotors for the older seals (when used in the older =
rotor housings with peripheral exhausts) is that the RX-8 seal was not =
designed to withstand the forces of crossing the exhaust port (in the =
Peripheral wall) opening unsupported. Its rather skinny and long.  =
Mazdatrix reported the RX-8 seals warped as a consequence of the the hot =
exhaust gas blowing over them and primarily the lack of wall support at =
the exhaust opening(on the older housings).  The combination of the =
additional heat and lack of wall support appears to be more than the 8 =
seal can take.

  However, I am in basic  agreement with you why machine the rotor when =
perhaps a new/modified seal is the answer.  I want to check with Tracy =
Crook since his seals are reportedly 800% stronger than stock apex seals =
to see whether the seals could be machined down/created so that they fit =
in the RX-8 rotor  standard apex slot and still be strong enough - say =
300% stronger than stock {:>).  Since they are not made of typical "gray =
iron" alloy that the stock and most other seals are made and chill/case =
hardened, they may be amenable to machining.

  Yes, having airports scattered around in just about every county and =
sometimes three or more in a county, the geography is much kinder to =
engine-out excursions here on the east coast.  Fly High, Glide long!  =
Better yet, keep running on both rotors.

  Ed A


    ----- Original Message -----=20
    From: Shearbond@aol.com<mailto:Shearbond@aol.com>=20
    To: Rotary motors in aircraft<mailto:flyrotary@lancaironline.net>=20
    Sent: Thursday, April 14, 2005 10:10 AM
    Subject: [FlyRotary] Rx-8 Rotors


    So.....since the rotors weigh the same within measurement error, the =
ability to rev to the 9,000s range vs. 7,000s range is not related to =
the orbiting mass of the rotor.  (Note: the motion is NOT truly =
circular, it is an epicycloid path that the center of mass of the rotor =
takes.  That 10 lb. rotor flops around plenty (technical term) and 10 =
lb. is lots heavier than an aluminum piston!

    It is apparent from an article on the "other" site, that the wall =
thicknesses and casting detail are lots more refined on the RX8 rotors =
than on earlier models...for more uniform and desirable heat transfer =
and uniformity.....oil cooling the rotor, etc.

    The mass being basically the same, it becomes a high probability =
that since centripetal force is F =3D (Mass x rotational velocity =
squared)/radius of rotation, {F=3D(m x w^2)/r}, it must be the weight of =
the seals themselves that are the critical element?  The force at 8,500 =
vx. 6,500 is (8.5/6.5) squared or 1.71 times greater.  Might this be why =
seal wear on the original seals goes up substantially at around 6,500 =
rpm?

    Tell me....why would one increase the depth of the seal groove of an =
RX8 rotor to allow a heavier seal????  On the RX8, 3.25mm/9.5mm =3D> =
approx. 34% reduction in apex seal mass!!  A lighter seal means a whole =
lot less force of the seal against the housing at 8,500 rpm!!  Anyone =
want to go back to old seals and rev to 8,500 rpm? =20

    Note:  the seal force against the housing at 8,500 rpm on the RX8 is =
still higher than the old seal at 6,500.... (.66 x 1.71 =3D 1.129).  Not =
much more, but there are probably even more very small details that we =
are not at first glance able to know and understand?  Seal =
material/housing material compatability is probably one significant =
factor??  (I used 9,000 vs. 7,000 and the numbers still come out about =
10% higher seal force on the RX8, even with the lighter seals.) =20

    Having been an R&D engineer at FoMoCo, it is hard to explain to most =
persons the creativity, detail, imagination, trial and testing and =
testing and testing and testing and ...... which goes into making an =
engine acceptable for production in quantities of XXX,XXX's and higher.  =
(One simply can't be wrong...it could bankrupt even the largest OEM.)  =
And....those Mazda engineers have done what many OEM's gave up on many =
years ago.  How?  Through their persistence and incredible insight into =
the issues.

    Before one gets the wire EDM out and starts going counter to what =
Mazda no doubt spent many $$$$ (more than all of our annual incomes put =
together??) on how to increase HP in an RX8, more information is needed =
before we start mixing and matching just because the parts will fit.  I =
know we are experimenters here, but lives of some who may not understand =
the "physics" limitations will ultimately be at stake.

    Above all:  Just because something works for 100 miles in a sprint =
race DOES NOT mean it will work while hummmming along for 5 hours at a =
crack at 75-80% max. HP on a cross-country over and over and over =
again....hopefully.  So far, my Lyc is a piece of 30's era design and =
materials...but it has run for 2,000 hours (350,000 miles) at 75-100% =
without fail!!

    Most of us aren't as lucky as Ed and his "on airport" emergency =
landings.  Perhaps it is that his green carpet (Carolina's) is lots more =
friendly than our granite peaks out here?

    Doug in Colorado
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<DIV style=3D"FONT-SIZE: 10pt; COLOR: #000000; FONT-FAMILY: Arial">
<DIV>Here's my take (FWIW as usual).&nbsp; Ed's answer is essentially=20
correct.&nbsp; But there is another reason for the greater depth of the =
2nd -=20
3rd gen apex seals.&nbsp; The increased contact area in the groove is =
needed to=20
transfer heat from seal to rotor.&nbsp; So no milling down the RA seals =
to fit=20
RX-8 rotors in RX-7 engines.&nbsp; (but hell, it might work =
anyway).&nbsp;=20
</DIV>
<DIV>&nbsp;</DIV>
<DIV>Also, the center of mass of the rotor DOES rotate in a perfect=20
circle.&nbsp; No monkey motion is ever involved.&nbsp; </DIV>
<DIV>&nbsp;</DIV>
<DIV>Another question was about why counter weights were required if the =
rotors=20
ballanced each other out.&nbsp; They are not in the same plane of =
rotation which=20
creates what is known as a "rocking couple".&nbsp; The counterweights =
make=20
another rocking couple (out of phase) to cancel out that of the =
rotors.</DIV>
<DIV>&nbsp;</DIV>
<DIV>Tracy (still at SnF)<BR></DIV>
<BLOCKQUOTE dir=3Dltr=20
style=3D"PADDING-RIGHT: 0px; PADDING-LEFT: 5px; MARGIN-LEFT: 5px; =
BORDER-LEFT: #000000 2px solid; MARGIN-RIGHT: 0px">
  <DIV>Hi Doug,</DIV>
  <DIV>&nbsp;</DIV>
  <DIV>Some good thoughts and questions, of which I would like to know =
the=20
  answers to as well.&nbsp; I believe the reason the experts are =
recommending=20
  milling the RX-8 rotors for the older seals (when used in the older =
rotor=20
  housings with peripheral exhausts) is that the RX-8 seal was not =
designed to=20
  withstand the forces of crossing the exhaust port (in the Peripheral =
wall)=20
  opening unsupported.&nbsp;Its rather skinny and long.&nbsp; Mazdatrix =
reported=20
  the RX-8 seals warped as a consequence of the the hot exhaust gas =
blowing over=20
  them and primarily the lack of wall support at the exhaust opening(on =
the=20
  older housings).&nbsp; The combination of the additional heat and lack =
of wall=20
  support appears to be more than the 8 seal can take.</DIV>
  <DIV>&nbsp;</DIV>
  <DIV>However, I am in basic &nbsp;agreement with you why machine the =
rotor=20
  when perhaps a new/modified seal is the answer.&nbsp; I want to check =
with=20
  Tracy Crook since his seals are reportedly 800% stronger than stock =
apex seals=20
  to see whether the seals could be machined down/created so that they =
fit in=20
  the RX-8 rotor&nbsp; standard apex slot and still be strong enough - =
say 300%=20
  stronger than stock {:&gt;).&nbsp; Since they are not made of typical =
"gray=20
  iron" alloy that the stock and most other seals are made and =
chill/case=20
  hardened, they may be amenable to machining.</DIV>
  <DIV>&nbsp;</DIV>
  <DIV>Yes, having airports scattered around in just about every county =
and=20
  sometimes three or more in a county, the geography is much kinder to=20
  engine-out excursions here on the east coast.&nbsp; Fly High, Glide=20
  long!&nbsp; Better yet, keep running on both rotors.</DIV>
  <DIV>&nbsp;</DIV>
  <DIV>Ed A</DIV>
  <DIV>&nbsp;</DIV>
  <DIV>&nbsp;</DIV>
  <BLOCKQUOTE dir=3Dltr=20
  style=3D"PADDING-RIGHT: 0px; PADDING-LEFT: 5px; MARGIN-LEFT: 5px; =
BORDER-LEFT: #000000 2px solid; MARGIN-RIGHT: 0px">
    <DIV style=3D"FONT: 10pt arial">----- Original Message ----- </DIV>
    <DIV=20
    style=3D"BACKGROUND: #e4e4e4; FONT: 10pt arial; font-color: =
black"><B>From:</B>=20
    <A title=3Dmailto:Shearbond@aol.com=20
    href=3D"mailto:Shearbond@aol.com">Shearbond@aol.com</A> </DIV>
    <DIV style=3D"FONT: 10pt arial"><B>To:</B> <A=20
    title=3Dmailto:flyrotary@lancaironline.net=20
    href=3D"mailto:flyrotary@lancaironline.net">Rotary motors in =
aircraft</A>=20
    </DIV>
    <DIV style=3D"FONT: 10pt arial"><B>Sent:</B> Thursday, April 14, =
2005 10:10=20
    AM</DIV>
    <DIV style=3D"FONT: 10pt arial"><B>Subject:</B> [FlyRotary] Rx-8 =
Rotors</DIV>
    <DIV><BR></DIV><FONT id=3Drole_document face=3DArial color=3D#000000 =
size=3D2>
    <DIV>So.....since the rotors weigh the same within measurement =
error, the=20
    ability to rev to the 9,000s range vs. 7,000s range is not related =
to the=20
    orbiting mass of the rotor.&nbsp; (Note: the motion is NOT truly =
circular,=20
    it is an epicycloid path that the center of mass of the rotor =
takes.&nbsp;=20
    That 10 lb. rotor flops around plenty (technical term) and 10 lb. is =
lots=20
    heavier than an aluminum piston!</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>It is apparent from an article on the "other" site, that the =
wall=20
    thicknesses and casting detail are lots more refined on the RX8=20
    rotors&nbsp;than on earlier models...for more uniform and desirable =
heat=20
    transfer and uniformity.....oil cooling the rotor, etc.</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>The mass being basically the same, it becomes a high =
probability that=20
    since centripetal force is F =3D (Mass&nbsp;x rotational velocity=20
    squared)/radius of rotation,&nbsp;{F=3D(m x&nbsp;w^2)/r}, it must be =
the=20
    weight of the <U><STRONG>seals</STRONG></U> themselves that are the =
critical=20
    element?&nbsp; The force at 8,500 vx. 6,500 is (8.5/6.5) squared or =
1.71=20
    times greater.&nbsp; Might this be why seal wear on the original =
seals goes=20
    up substantially at around 6,500 rpm?</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Tell me....why would one increase the depth of the seal groove =
of an=20
    RX8 rotor&nbsp;to allow a heavier seal????&nbsp; On the RX8, =
3.25mm/9.5mm=20
    =3D&gt; approx. 34% reduction in apex seal mass!!&nbsp;&nbsp;A =
lighter=20
    seal&nbsp;means a whole lot less force of the seal against the =
housing at=20
    8,500 rpm!!&nbsp; Anyone want to go back to old seals and rev to =
8,500=20
    rpm?&nbsp; </DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Note:&nbsp; the seal force against the housing at 8,500 rpm on =
the RX8=20
    is still higher than the old seal at 6,500.... (.66 x 1.71 =3D =
1.129).&nbsp;=20
    Not much more, but&nbsp;there are probably even more very small =
details that=20
    we are not at first glance able to know and understand?&nbsp; Seal=20
    material/housing material compatability is probably one significant=20
    factor??&nbsp; (I used 9,000 vs. 7,000 and the numbers still come =
out about=20
    10% higher seal force on the RX8, even with the lighter =
seals.)&nbsp; </DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Having been an R&amp;D engineer at FoMoCo, it is hard to =
explain to=20
    most persons the creativity, detail, imagination, trial and testing =
and=20
    testing and testing and testing and ......&nbsp;which goes into =
making an=20
    engine acceptable for production in quantities of XXX,XXX's and=20
    higher.&nbsp; (One simply can't be wrong...it could bankrupt even =
the=20
    largest OEM.)&nbsp; And....those Mazda engineers have done what many =
OEM's=20
    gave up on many years ago.&nbsp; How?&nbsp; Through their =
persistence and=20
    incredible insight into the issues.</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Before one gets the wire EDM out and starts going counter to =
what Mazda=20
    no doubt spent many&nbsp;$$$$ (more than all of our annual incomes =
put=20
    together??) on how to increase HP in an RX8, more information is =
needed=20
    before we start mixing and matching just because the parts&nbsp;will =

    fit.&nbsp; I know we are experimenters here, but lives of some who =
may not=20
    understand the "physics"&nbsp;limitations will ultimately be at =
stake.</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Above all:&nbsp; Just because something works for 100 miles in =
a sprint=20
    race <STRONG>DOES NOT</STRONG> mean it will work =
while&nbsp;hummmming along=20
    for 5 hours at a crack at 75-80% max. HP on a cross-country over and =
over=20
    and over again....hopefully.&nbsp; So far, my Lyc is a piece of 30's =
era=20
    design and materials...but it has run for 2,000 hours (350,000=20
    miles)&nbsp;at 75-100% without fail!!</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Most of us aren't as lucky as Ed and his "on airport" emergency =

    landings.&nbsp; Perhaps it is that his green carpet =
(Carolina's)&nbsp;is=20
    lots more friendly than our granite peaks out here?</DIV>
    <DIV>&nbsp;</DIV>
    <DIV>Doug in =
Colorado</DIV></BLOCKQUOTE></BLOCKQUOTE></FONT></DIV></BODY></HTML>

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