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[220.235.107.246]) by smtp.gmail.com with ESMTPSA id d21-20020a17090ad3d500b002309279baf8sm148421pjw.43.2023.03.14.19.38.40 for (version=TLS1_2 cipher=ECDHE-ECDSA-AES128-GCM-SHA256 bits=128/128); Tue, 14 Mar 2023 19:38:41 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 16.0 \(3731.400.51.1.1\)) Subject: Re: [FlyRotary] Coolant barbs Date: Wed, 15 Mar 2023 10:38:27 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <590E02C4-5028-45BF-95C3-3E8258A4D508@gmail.com> X-Mailer: Apple Mail (2.3731.400.51.1.1) Hi Mark. Thats what I have done re throttle body and heater with my Renesis. Do you have a line from the top of rear iron(front in the aeroplane) to = purge air from the top of the motor back to a highest point in the = system? I tapped and plugged the hole between the pump in and out circuits below = to OEM thermostat, but I didn=E2=80=99t put a hole in the plug for air = to escape from the inlet side. Is that recommended by the experts? Perhaps I missed that advice. When I remove a screw on cap where the original thermostat used to = lived, and my highest point in the system there is never any air = trapped. For clearance with cowl I cut off the Renesis thermostat housing and = welded a screw on cap on top and an inlet barb onto the side so the flow = is pretty much directly inline with the pump entry in the front housing. I have from memory a 5/8=E2=80=9D restrictor in the inlet to the pump.=20= Basically a piece of 1=E2=80=9D aluminium tube that fits through the cap = entry I welded on, that blocks the inlet except for 5/8=E2=80=9D holes = drilled through both sides of the tube inline with the flow.=20 I removed that restrictor recently and the temps went up considerably, = which I put down to the pump cavitating well below my take off RPM limit = to 7500. My Renesis is Series 1 and I understand the pumps are known to cavitate = at higher rpm.=20 I=E2=80=99m thinking, by removing the thermostat and smoothing the flow = path I've lowered the rpm of the pump cavitating. I=E2=80=99m presently considering changing the pump to an NZ pump many = racers use (The impeller looks similar to the US Re-medy pump).=20 Basically an improved impeller designed to reduce cavitation at high = rpm. I might then be able to reduce the restriction and perhaps increase the = flow rate, which will perhaps increase cooling. Has anyone else changed pump, used a larger pulley to slow the pump, and = has data to share? Cheers Steve Izett Flying - Glasair Super IIRG Genesis 4 Port RD1-C EC2 EM3 > On 15 Mar 2023, at 9:37 am, Mark McClure mark.mcclure.m3@gmail.com = wrote: >=20 > Planning my coolant flow for my engine setup on test stand only. Want = to minimize unnecessary water lines. In searching the list/rx-8 forums I = couldn=E2=80=99t find any reason I cannot just block the in and out = spots for the throttle body and heater cores.=20 >=20 > Will be bypassing the thermostat with center plug and hole tapped for = air bubble. Only other line will be from radiator to expansion tank.=20 >=20 > Am I mis understanding something? >=20 > Regards, > Mark >=20 >=20 > <2CD7ED4F-3167-4AD8-87D3-6B01C6CD72D9-compressed.pdf>-- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html