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Thu, 17 Aug 2017 05:00:20 +0000 To: Rotary motors in aircraft Subject: Re: [FlyRotary] oil flow Thread-Topic: [FlyRotary] oil flow Thread-Index: AQHTFw9ivpB2yYuYa0STygl93NoAV6KH96NC Date: Thu, 17 Aug 2017 05:00:20 +0000 Message-ID: References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: x-originating-ip: [69.146.88.60] x-ms-publictraffictype: Email x-microsoft-exchange-diagnostics: 1;CY1PR05MB2442;6:+itTxWUERAfZ2xXjLOHHPFYb6HDjxEO5w8UbZ1tipRjeoYUDBKBtg0k0qujZxm+dgwHLaOOclXY7eUBuRCRMqe8luZlZL6C6IEsVGBhi5eXCxcjGzKLobQi+wSXLOg0rx4OxIfEJbn5hnoEQKz2T0QWNHWRqcHRFwnt640VIjFnPg0jh/nO0JpKqcVQdFI5DoLHBVYFN7ZzTRdXIqe+mG5I+yacwyz8ma/kueYMgU+kGy0VHYnQClBxpv2/yl43g9kxlqffHfsn5+TsfenpPVfQvnIqFrccwe7hZvWuMXqFt46c23uavM9xAzNPMrbxHgAcHAkU2CfSHxuatYN+yRw==;5:Zz8QDKo0Gg/8wUTb/DhslNviifpvEMRQBUHnN5OtXzq2iKZLhdnEAN5puojwe/EukOgm9qipQf6gENA2wjjr/uhNikXiqZzJJznNNav9Yo3rHibbk4OH4BQcdKk5L+tp3tBwh21tjp1G5+fI4jJk1mSwdOwFL+KOjb775FQl0Q8=;24:iyZeyzuHgRzy7ZQAC6d4cpchVkA9y6Fpfhu/FcjepjT271S5A3imSsvuGD5X3gw+QkRomLEn43CQb548/ptXW3p/aF90lXzrxaJYIYqJo78=;7:EKiyHcBkbbppVL/KB5V3QqRO//f41ABjVGvy8hLMVuZAegDpOlPuklIvJBhiHj2QKj8gFO/cZWQnH6clt5XHTG8SY//YSZxa9286OJG5K+RloRt83jpptGlVf3HAl723o5n9RnZheSeU7OF+pkNJFB0Hwr6SAvVnU6L5Iuyru8uuJAFB2kkq5BMcOG9onkvcfKDel1gGL+YJL4xwY9Gs59w3R+IRe4xTkwZfqhYkmu0= x-ms-office365-filtering-correlation-id: 153698e7-70d3-4e3f-f385-08d4e52cdc55 x-microsoft-antispam: UriScan:;BCL:0;PCL:0;RULEID:(300000500095)(300135000095)(300000501095)(300135300095)(22001)(300000502095)(300135100095)(2017030254152)(300000503095)(300135400095)(2017052603157)(201703131423075)(201703031133081)(201702281549075)(300000504095)(300135200095)(300000505095)(300135600095)(300000506095)(300135500095);SRVR:CY1PR05MB2442; 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received-spf: None (protection.outlook.com: uwyo.edu does not designate permitted sender hosts) spamdiagnosticoutput: 1:99 spamdiagnosticmetadata: NSPM Content-Type: multipart/alternative; boundary="_000_CY1PR05MB1915D95897481C719D36DFE4B9830CY1PR05MB1915namp_" MIME-Version: 1.0 X-OriginatorOrg: uwyo.edu X-MS-Exchange-CrossTenant-originalarrivaltime: 17 Aug 2017 05:00:20.3399 (UTC) X-MS-Exchange-CrossTenant-fromentityheader: Hosted X-MS-Exchange-CrossTenant-id: f9cdd7ad-825d-4601-8e9c-a325e02d52da X-MS-Exchange-Transport-CrossTenantHeadersStamped: CY1PR05MB2442 --_000_CY1PR05MB1915D95897481C719D36DFE4B9830CY1PR05MB1915namp_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Andrew, Turning the engine by hand and collecting the oil delivered by the pump gav= e: 1986 13B: 426 revolutions per gallon or 11.7 gal/min at 5000 rpm 2010 Renesis: 392 revolutions per gallon or 12.7 gal/min at 5000 rpm. I haven't tested a pre-2009 Renesis. As long as you are not using a restrictive oil cooler like those from a sto= ck 13B, the oil will not be returned to the sump by the front OCV during no= rmal operation. All the oil will go through the cooler and the cooled oil = will either pass through the bearings and EC shaft jets or be returned to t= he sump by the rear iron oil pressure relief valve. It would be good to verify that your oil cooler is not restrictive. If you= want more oil passing through the bearings and jets, you could possibly ru= n higher oil pressure by using a higher pressure rear iron relief valve. Steve Boese ________________________________ From: Rotary motors in aircraft on behalf of = Andrew Martin Sent: Wednesday, August 16, 2017 10:13:52 PM To: Rotary motors in aircraft Subject: [FlyRotary] oil flow Has anyone ever had a flow transducer in the oil circuit? If so, what was t= he peak flow? Does anyone know the cc/rev specs and gearing ratio of the oil pump? If there was past discussion on this on the list please let me know, but as= yet I have not been able to find anything. Bit of background, Steve Boese's oil cooler experiments from a few years ba= ck has helped me much but got me searching more for the effect of oil flow = on heat rejection in the entire system. My temps are much better on the ground now that I've relocated the heat exc= hangers, but I am reluctant to fly again until I know I can get to a decent= altitude before encountering max temps. I dont think flow of oil through an engine built with tight specs would cha= nge appreciably from idle to max rpm, but flow through the OCV will rise sh= arply. My engine is a 2004 Renesis with a front cover OCV. I think I could= get much better control of the oil temp if I could get higher flow through= the cooler. I think its all about controlling the average deltaT. so a tig= hter engine is going to need much higher deltaT through the cooler as flow = will be lower. There are probably many ways that would give me a solution. * less oil restriction in engine (should have modified those eccentric = oil jets). this may be the best solution but I don't really want to open th= e engine again just yet. * I could put an external OCV set at lower pressure than front cover OC= V inline after heat exchanger, more oil is being cooled. * A bigger heat exchanger would also do the job, but I don't think its = the best solution as its just a guess on how big to go. * What I might do is. plumb in a lower pressure or adjustable OCV and s= olenoid valve in series on oil "out" port on engine, dump oil into a extra = heat exchanger then back to sump. with solenoid off, oil flows as it does n= ow, with it on =3D extra cooling on demand, basically all that happens is o= il that would be returned straight back to sump is diverted to a cooler, en= gine would just see the slightly lower pressure from the second OCV. My theory is that Oil pressure is nice to know but kind of meaningless. Its= possible to have high pressure but flow going to the wrong place (sump), w= hich is not good. Pump is fixed displacement so oil has to go somewhere. Ul= timately, Maybe an engine with lower pressure due to less restriction withi= n the rotating parts is probably best as it results in higher flow oil to w= here its needed. Any thoughts Cheers Andrew --_000_CY1PR05MB1915D95897481C719D36DFE4B9830CY1PR05MB1915namp_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Andrew,


Turning the engine by hand and collecting the oil delivered by the pump = gave:

1986 13B: 426 revolutions per gallon or 11.7 gal/min at 5000 rpm

2010 Renesis: 392 revolutions per gallon or 12.7 gal/min at 5000 rpm.


I haven't tested a pre-2009 Renesis.


As long as you are not using a restrictive oil cooler like those from a = stock 13B, the oil will not be returned to the sump by the front OCV during= normal operation.  All the oil will go through the cooler and the coo= led oil will either pass through the bearings and EC shaft jets or be returned to the sump by the rear iron oil= pressure relief valve.


It would be good to verify that your oil cooler is not restrictive. = ; If you want more oil passing through the bearings and jets, you could pos= sibly run higher oil pressure by using a higher pressure rear iron relief v= alve.


Steve Boese


From: Rotary motors in airc= raft <flyrotary@lancaironline.net> on behalf of Andrew Martin <fly= rotary@lancaironline.net>
Sent: Wednesday, August 16, 2017 10:13:52 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] oil flow
 
Has anyone ever had a flow transducer in the oil circuit? If so, what = was the peak flow?
Does anyone know the cc/rev specs and gearing ratio of the oil pump?
If there was past discussion on this on the list please let me know, b= ut as yet I have not been able to find anything.

Bit of background, Steve Boese's oil cooler experiments from a few years ba= ck has helped me much but got me searching more for the effect of oil flow = on heat rejection in the entire system.

My temps are much better on the ground now that I've relocated the heat exc= hangers, but I am reluctant to fly again until I know I can get to a decent= altitude before encountering max temps.

I dont think flow of oil through an engine built with tight specs would cha= nge appreciably from idle to max rpm, but flow through the OCV will rise sh= arply.  My engine is a 2004 Renesis with a front cover OCV. I think I = could get much better control of the oil temp if I could get higher flow through the cooler. I think its all ab= out controlling the average deltaT. so a tighter engine is going to need mu= ch higher deltaT through the cooler as flow will be lower.

There are probably many ways that would give me a solution.
  • less oil restriction in engine (should have modified those eccentric oi= l jets). this may be the best solution but I don't really want to open the = engine again just yet.
  • I could put an external OCV set at lower pressure than front cover= OCV inline after heat exchanger, more oil is being cooled.
  • A bigger heat exchanger would also do the job, but I don't think i= ts the best solution as its just a guess on how big to go.
  • What I m= ight do is. plumb in a lower pressure or adjustable OCV and solenoid valve = in series on oil "out" port on engine, dump oil into a extra heat= exchanger then back to sump. with solenoid off, oil flows as it does now, = with it on =3D extra cooling on demand, basically all that happens is oil that would be returned straight = back to sump is diverted to a cooler, engine would just see the slightly lo= wer pressure from the second OCV.
My theory is that Oil pressure is nice to know but kind of meaningless= . Its possible to have high pressure but flow going to the wrong place (sum= p), which is not good. Pump is fixed displacement so oil has to go somewher= e. Ultimately, Maybe an engine with lower pressure due to less restriction within the rotating parts is probab= ly best as it results in higher flow oil to where its needed.

Any thoughts
Cheers  Andrew




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