X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from aspensprings.uwyo.edu ([129.72.10.32] verified) by logan.com (CommuniGate Pro SMTP 6.0c2) with ESMTPS id 5908388 for flyrotary@lancaironline.net; Wed, 28 Nov 2012 10:56:46 -0500 Received-SPF: none receiver=logan.com; client-ip=129.72.10.32; envelope-from=SBoese@uwyo.edu Received: from ponyexpress-ht5.uwyo.edu (extlb.uwyo.edu [172.26.4.4]) by aspensprings.uwyo.edu (8.14.4/8.14.4) with ESMTP id qASFtvMT015271 (version=TLSv1/SSLv3 cipher=AES128-SHA bits=128 verify=FAIL) for ; Wed, 28 Nov 2012 08:56:11 -0700 (MST) (envelope-from SBoese@uwyo.edu) Received: from ponyexpress-m10.uwyo.edu ([fe80::60dd:cb9e:6f71:3d48]) by ponyexpress-ht5.uwyo.edu ([fe80::addc:5ab0:b0f8:ab9e%13]) with mapi id 14.02.0318.001; Wed, 28 Nov 2012 08:55:35 -0700 From: "Steven W. Boese" To: Rotary motors in aircraft Subject: RE: [FlyRotary] Re: Oil Injection Pump setting Thread-Topic: [FlyRotary] Re: Oil Injection Pump setting Thread-Index: AQHNzXGZFwpCC9ErvESptNgQR/Q8Rpf/YJTL Date: Wed, 28 Nov 2012 15:55:34 +0000 Message-ID: <3E8191F276108F4481AB0721BBA9269E05EC56FD@ponyexpress-m10.uwyo.edu> References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: x-originating-ip: [75.196.207.214] Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable MIME-Version: 1.0 Tracy, On my 1986 13B, I connected a cable from the throttle body to the OMP adjus= ter lever and operated it similar to how it was in the car: minimum lever t= ravel at idle and maximum at WOT. If the throttle was adjusted so that it = was closed just enough to avoid decreasing MAP when at max MAP at altitude,= the average oil delivery was between 0.9 and 1.0 oz/gal. If the throttle = was opened farther without increasing the MAP, oil would accumulate in the = crankcase. I don't have the oil delivery rate number for that condition bu= t might be able to go back in my records and get an estimate. Whether or n= ot this was a good arrangement may be in question since this is the engine = that developed apex seal chatter marks, wore through the chrome of the roto= r housing, and lost compression after about 300 hr of aircraft use. The post 2008 Renesis that I have has two solenoid driven pumps, one supply= ing two nozzles (1 for each rotor) and the other supplying four nozzles (2= for each rotor). These could be driven with a driver similar to a fuel in= jector driver with the frequency determining the oil delivery rate since th= e piston stroke is not variable. I haven't tried to use them since togethe= r, they weigh over 4 lb. Steve Boese RV6A, 1986 13B NA, RD1A, EC2 ________________________________________ From: Rotary motors in aircraft [flyrotary@lancaironline.net] on behalf of = Tracy [rwstracy@gmail.com] Sent: Wednesday, November 28, 2012 7:05 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Oil Injection Pump setting How have you guys using the OMP adjusted the injection amount? Have you f= ound it good enough to set it to maximum and just let the engine rpm vary t= he amount? If not, about what percentage of the adjuster lever travel di= d you end up with and what oz per gal of fuel did that equal? Any info appreciated! Tracy -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.= html=