X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from nm19-vm0.bullet.mail.sp2.yahoo.com ([98.139.91.216] verified) by logan.com (CommuniGate Pro SMTP 5.3.10) with SMTP id 4578915 for flyrotary@lancaironline.net; Sun, 14 Nov 2010 17:11:47 -0500 Received-SPF: none receiver=logan.com; client-ip=98.139.91.216; envelope-from=keltro@att.net Received: from [98.139.91.66] by nm19.bullet.mail.sp2.yahoo.com with NNFMP; 14 Nov 2010 22:11:11 -0000 Received: from [98.139.91.16] by tm6.bullet.mail.sp2.yahoo.com with NNFMP; 14 Nov 2010 22:11:11 -0000 Received: from [127.0.0.1] by omp1016.mail.sp2.yahoo.com with NNFMP; 14 Nov 2010 22:11:11 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 866567.96578.bm@omp1016.mail.sp2.yahoo.com Received: (qmail 35009 invoked by uid 60001); 14 Nov 2010 22:11:11 -0000 DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=att.net; s=s1024; t=1289772671; bh=Vse7J1fOyYC26VS5K3Y9IoqaHD/anwZLruKPACGXBIs=; h=Message-ID:X-YMail-OSG:Received:X-Mailer:Date:From:Subject:To:MIME-Version:Content-Type; b=0BqfLm2Rypqb1DQS5UNt2nwvJvdsIYUVNxkhUrsa+rvLLYH/DURRUNJM19Xx5zt3rQcOc2a9jxpShaofJclsicfVFp5uKM1+9MpDiSzcXIxJgN/6znnB4dItmWIc9nQcQp1ARRHwUdhLtqHoJJetkAk15ub6blTO2ij1TFxL+Uc= DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=att.net; h=Message-ID:X-YMail-OSG:Received:X-Mailer:Date:From:Subject:To:MIME-Version:Content-Type; b=0MfETKXpHVyZUJ4E/YwvUpuL2udh8mkiheFBUkqeePBegPvLdDQGQ+EesXZjXvAC5j0kK15rv651xfdtqkj+rGcyxHi6Y0xc0nqRAQiNtw7kN1LNrxNeW+3dzrSqPCL8LR9mIK/WBzxcBWagBj2oPxoC6RQP03eIh7L09lkUkJc=; Message-ID: <484621.6828.qm@web83909.mail.sp1.yahoo.com> X-YMail-OSG: ART2.VUVM1m4zXJ7qBYesokd4hkzgKuiizK4xkhTylb9YRB wr_9kZN2mmS6U0eK4PqaGDPPzd0hbULIzb9uGzp2SffEA8.u5JyR6Ta.e3Zq XjY5f5JF8s67_EM.WWi58g0Gpq9BY2Y2Jn7tn7rXzZfGeIXXl7BAgHUSxC1G 1aREkQPdQ3.Bluim13oGyOcfEvGJwjuJku2YujER6Ct1LLLaMH3llBEV8cy9 06lllC1ZVyS175t7VZuscHrQBQRIg7BurSDRIkjbCeB8jTrSwQuFlGz8EcaI QR_vgT8A0PLZ_E9wvX2Pw1cNMzHN7rw-- Received: from [208.114.36.189] by web83909.mail.sp1.yahoo.com via HTTP; Sun, 14 Nov 2010 14:11:11 PST X-Mailer: YahooMailRC/504.5 YahooMailWebService/0.8.107.285259 Date: Sun, 14 Nov 2010 14:11:11 -0800 (PST) From: Kelly Troyer Subject: TURBO INFO To: Rotary motors in aircraft MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-1500083687-1289772671=:6828" --0-1500083687-1289772671=:6828 Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Perhaps of interest to those of the group contemplating a "TURBOCHARGER" fo= r =0Atheir project.............=0A=C2=A0=0AKelly Troyer=0A"DYKE DELTA JD2" = (Eventually)=0A"13B ROTARY"_ Engine=0A"RWS"_RD1C/EC2/EM2=0A"MISTRAL"_Backpl= ate/Oil Manifold=0A"TURBONETICS"_TO4E50 Turbo=0A=0ATurbo Oil Needs=0ATurbos= rotate at very high speeds and their center bearings require a continuous = =0Asupply of pressurized, clean and cool oil. Sleeve-type bearings need =0A= considerably more oil than ball-bearing turbos but in either case, if the o= il =0Asupply is ineffective, the turbo will soon fail. The same importance = also =0Aapplies to the oil exit: if the oil cannot freely escape, it will f= orce itself =0Athrough the seals, causing smoke. =0A=0AThe specific oil ne= eds vary from turbo to turbo, however, as an example, the =0Amanufacturer= =E2=80=99s data sheet for the small Garrett GT12 shows the turbo requires a= =0Asupply of engine oil:=0A=09* Filtered at a 20 micron level =0A=09* Fed = to the turbo through a minimum internal diameter line of 3.2mm =0A=09* At a= minimum pressure of 2 Bar (ie 29 psi) at peak engine torque =0A=09* Not le= ss than 0.7 Bar (10 psi) at idle =0A=09* At a temperature below 130 degrees= C=0ABall-bearing turbos use a restrictor (normally positioned on the oil i= nlet) so =0Athat the amount of oil that flows through the turbo bearing is = less than in a =0Aconventional turbo.=0AThe oil drain from a turbo operates= via gravity. That is, the pressure drop =0Aacross the turbo bearing is nea= rly complete and it is only gravity that causes =0Athe oil to flow back to = the sump. In fact, it cannot really be termed =E2=80=98oil=E2=80=99 as =0Aa= fter it has passed through the turbo, the oil becomes an aerated foam =E2= =80=93 one =0Areference suggests it looks like =E2=80=98dirty whipped cream= =E2=80=99. It=E2=80=99s therefore important =0Athat:=0A=09* The drain line = is much larger in diameter than the pressure feed line =0A=09* The connecti= on to the sump is made above the oil level =0A=09* The drain pipe is kept a= s close to vertical as possible=0AIf the sump drain joins at a level below = the oil, the much lower density of the =0Aaerated oil will cause it to sit = on top of the sump oil, gradually backing-up to =0Athe turbo. =0A=0AIn appl= ications where the turbo is positioned too low relative to the engine for = =0Anormal drain-back to occur, an electric or mechanical scavenge pump can = be =0Afitted. (This approach is adopted in many piston aircraft engines.) I= n this =0Asituation a small sump must be installed beneath the turbo allowi= ng the oil to =0Aaccumulate within it, with the pump then drawing from this= sump. Turbos mounted =0Aremote from the engine (eg at the back of the car)= also use a scavenge pump to =0Areturn the oil to the engine. =0A=0AThe oi= l requirement of the turbo will have an affect on the engine oiling =0Asyst= em. System oil pressure will drop a little, a major reason why factory turb= o =0Aversions of naturally aspirated engines often use a larger oil pump. I= n =0Aaftermarket applications, the fact that the engine oil pump is normall= y a little =0Aover-sized is taken advantage of to allow for the extra suppl= y to the turbo. =0AHowever, in applications where a turbo hasn=E2=80=99t pr= eviously been fitted to the =0Aengine, system oil pressure measurements sho= uld be taken after fitment of the =0Aturbo to ensure that adequate oil pres= sure is maintained at the engine. =0AManufacturer=E2=80=99s oil pressure sp= ecs can be used to ascertain if this is the case. --0-1500083687-1289772671=:6828 Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: quoted-printable
=0A
Perhaps of interest to those of the = group contemplating a "TURBOCHARGER" for their project.............
&nbs= p;
=0A

Kelly Troyer
"DYKE DELTA JD2" (Eventually)

=0A

"13B ROTARY"_ Engine=
"RWS"_RD1C/EC2/EM2
"MISTRAL"_Backplate/Oil Manifold

=0A

"TURBON= ETICS"_TO4E50 Turbo

=0A
 
=0A
=0A

Turbo Oil Needs=0A

Turbos rotate at very high speeds and their center bearings requir= e a continuous supply of pressurized, clean and cool oil. Sleeve-type beari= ngs need considerably more oil than ball-bearing turbos but in either case,= if the oil supply is ineffective, the turbo will soon fail. The same impor= tance also applies to the oil exit: if the oil cannot freely escape, it wil= l force itself through the seals, causing smoke.

=0A
3D"Click =0A

The specific oil needs vary from turbo to turbo, however, as an e= xample, the manufacturer=E2=80=99s data sheet for the small Garrett GT12 sh= ows the turbo requires a supply of engine oil:

=0A
    =0AFiltered at a 20 micron level =0A
  • Fed to the turbo through a minimum in= ternal diameter line of 3.2mm =0A
  • At a minimum pressure of 2 Bar (ie 29 = psi) at peak engine torque =0A
  • Not less than 0.7 Bar (10 psi) at idle = =0A
  • At a temperature below 130 degrees C
=0A

Ball-bearing tur= bos use a restrictor (normally positioned on the oil inlet) so that the amo= unt of oil that flows through the turbo bearing is less than in a conventio= nal turbo.

=0A

The oil drain from a turbo operates via gravity. That i= s, the pressure drop across the turbo bearing is nearly complete and it is = only gravity that causes the oil to flow back to the sump. In fact, it cann= ot really be termed =E2=80=98oil=E2=80=99 as after it has passed through th= e turbo, the oil becomes an aerated foam =E2=80=93 one reference suggests i= t looks like =E2=80=98dirty whipped cream=E2=80=99. It=E2=80=99s therefore = important that:

=0A
    =0A
  • The drain line is much larger = in diameter than the pressure feed line =0A
  • The connection to the sump i= s made above the oil level =0A
  • The drain pipe is kept as close to vertic= al as possible
=0A

If the sump drain joins at a level below the = oil, the much lower density of the aerated oil will cause it to sit on top = of the sump oil, gradually backing-up to the turbo.

=0A

In applicatio= ns where the turbo is positioned too low relative to the engine for normal = drain-back to occur, an electric or mechanical scavenge pump can be fitted.= (This approach is adopted in many piston aircraft engines.) In this situat= ion a small sump must be installed beneath the turbo allowing the oil to ac= cumulate within it, with the pump then drawing from this sump. Turbos mount= ed remote from the engine (eg at the back of the car) also use a scavenge p= ump to return the oil to the engine.

=0A
3D"Click
=0A

The oil requirem= ent of the turbo will have an affect on the engine oiling system. System oi= l pressure will drop a little, a major reason why factory turbo versions of= naturally aspirated engines often use a larger oil pump. In aftermarket ap= plications, the fact that the engine oil pump is normally a little over-siz= ed is taken advantage of to allow for the extra supply to the turbo. Howeve= r, in applications where a turbo hasn=E2=80=99t previously been fitted to t= he engine, system oil pressure measurements should be taken after fitment o= f the turbo to ensure that adequate oil pressure is maintained at the engin= e. Manufacturer=E2=80=99s oil pressure specs can be used to ascertain if th= is is the case.

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