X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=NYOYKFL4 c=1 sm=1 tr=0 a=99SZI+B64J60o7343nyXDw==:117 a=ssLVzwRQRmYksP1d/+CGUg==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=sTwFKg_x9MkA:10 a=pGLkceISAAAA:8 a=Ia-xEzejAAAA:8 a=pjdaNNIBAAAA:8 a=0OYo5GGMAAAA:8 a=7g1VtSJxAAAA:8 a=0kqfyza-pE00PMVTfD0A:9 a=vDBjhwOW_TXxJ_SS:21 a=cfgZujWGhjT07SNs:21 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=S0wkRrzPavQA:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=pnywrGd5FeincJp7Izph:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pl1-f170.google.com ([209.85.214.170] verified) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 224171 for flyrotary@lancaironline.net; Sat, 09 May 2020 05:22:05 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.214.170; envelope-from=stephen.izett@gmail.com Received: by mail-pl1-f170.google.com with SMTP id u10so1796870pls.8 for ; Sat, 09 May 2020 02:22:07 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=from:content-transfer-encoding:mime-version:subject:date:references :to:in-reply-to:message-id; bh=nRpja2/XnLnpwuWhmmNTIMQuNKOvU43FDlB1s7KZvNs=; b=cMQYkAJCVXDBwA9iUxha9jPfFqYmV9fUnr7AgQa5sWbBhzaPhF7em+B0zc5y2hnFv9 sKo/vEKSXRQqn091rr8J/CFxSdfXsHCR9ZuhvwiNBJhmfHNQWf1hL68sRKDHhF2pOr/P Zo9av3yKIWDLNUkuWuyLLtkZHRgHVquwfKB7/F0oXTSwek6CnhOQUKez8hDsFHYi6Us0 IQD4agTjDL6LnU452S4HkAtrEVA04jn3fEVz77Nb2BuJJJoh6F17mKmvV7O28XD11nbx 8cBlrg6vD5mDgauzivF3q9115/fXFIw3lr/ZI2e+3jkTQ3ffsqdTmVLsJ88cVg+NqLFR 1Ucg== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:from:content-transfer-encoding:mime-version :subject:date:references:to:in-reply-to:message-id; bh=nRpja2/XnLnpwuWhmmNTIMQuNKOvU43FDlB1s7KZvNs=; b=dATcSSMq1pe/zb6++chnBJyDcuHvOncusXsC2J2z7KPEWmwFM8vdDfZAi1D4fBhQeb Z/yr3GYmpE61mTrWAartASzrWbaE2sguDbpu8lcMhHsf8mELXoeT+aJL9lcQAhJGq2M8 sCJgXcwq8TnIBfL0ThxyPicJ9OaYULDIr2iie1QU6YLqTtjH/kLn9wNC+KEV8ztDM7h2 BdbUVyhzHQLH6JNDdZwVoIe/c8He2TQKCdiXaapFZjai/wM1m9q5B5ASsDaXyhm8d2vw 2ZRpX0NsjjU4zbO+CPyymoj8y3QHSALE/PcwEzrCl9c7OkYsKAuuduELkSlxVQJAsrCi oQlQ== X-Gm-Message-State: AGi0PubAHrJzvLM2XxD2FqghmSKksOp1RrdZQwAoBCLkD8KWmTCs6UgV PMCqK275JWAcqwtMVayH8hIGAxAE X-Google-Smtp-Source: APiQypL66owImrRhfgxhNmfd8PwccEYwI46AhpVlBTo+1EFTYyPmg3kXzSn6R4OxiHzccs0Z4iubIA== X-Received: by 2002:a17:90a:1ae9:: with SMTP id p96mr10480549pjp.75.1589016108514; Sat, 09 May 2020 02:21:48 -0700 (PDT) Return-Path: Received: from macbook-pro.lan ([118.209.160.247]) by smtp.gmail.com with ESMTPSA id c10sm3944044pfm.50.2020.05.09.02.21.46 for (version=TLS1_2 cipher=ECDHE-ECDSA-AES128-GCM-SHA256 bits=128/128); Sat, 09 May 2020 02:21:48 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 12.4 \(3445.104.11\)) Subject: Re: [FlyRotary] Re: Turbos Date: Sat, 9 May 2020 17:21:44 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <94462409-AFE3-4B4B-ACB1-E96FE41FF116@gmail.com> X-Mailer: Apple Mail (2.3445.104.11) Thanks Todd. Is there such a thing as a controller that references ambient pressure = as the reference so that charge remains constant. I=E2=80=99m asking more from interest than wanting this in the future. I = thought cars might use such a system to adjust for altitude. Cheers Steve > On 9 May 2020, at 4:00 pm, Todd Bartrim bartrim@gmail.com = wrote: >=20 > Hi Steve; > I did use the standard actuator until the diaphragm burst during = take-off resulting in a very impressive climb rate. I replaced it with = this one on ebay > https://www.ebay.com/itm/262896884959 > It is a piston rather than a diaphragm. The diaphragm will react = faster than a piston, but for our application it shouldn't matter, but = the piston is far more reliable. To rebuild this is simply changing the = o-ring. The mounting bracket that comes with it will fit if your = compressor outlet is in the stock configuration, but as mine has been = rotated to have the outlet at the 9:00 position, I had to heavily modify = it to fit. Not a big deal if you can weld aluminum. > For boost control I use a TurboSmart electronic boost controller like = this one > https://www.turbosmart.com/product/eboost2-60mm-black/=20 > Mine is the earlier version (not the 2) and was no where near this = pricey (I think it was around $400cad), but as far as I can see, just as = functional. Now keep in mind that it won't reduce your boost to = pressures below the spring pressure, so use the lowest spring that you = can get and that will be your minimum boost pressure. Then you preset = your desired boost levels in the controller and at the touch of a button = you can get increased boost. It works simply by switching a small = Numatics 3-way solenoid to vent some of the air pressure from the hose = connecting the compressor outlet to the actuator. Simple but effective. > I have a 6psi spring and have my setpoints set at 9psi and 12psi. = I've not needed to use them yet, so this expense could probably be = saved. >=20 > Todd Bartrim > C-FSTB > RV9 > 13B Turbo Rotary Engine >=20 >=20 > On Fri, May 8, 2020 at 4:15 PM Stephen Izett stephen.izett@gmail.com = wrote: > Hi guys. > Another turbo question. > Do you guys just use a standard waste gate actuator (perhaps with = basic controller allowing different boost settings) and run out of boost = at x altitude, or do you have some kind of altitude compensation? > Thanks > Steve Izett >=20 >=20 > > On 9 May 2020, at 6:24 am, 12348ung@gmail.com = wrote: > >=20 > > Dave and contributors, > > Spent yesterday finally = getting specific answers that I should have had 12 months ago. The guru = that I sent the stock turbo to in the end had no idea as to an upgrade = for temp in the hot section. The up grade that Dave suggested is = approx. $900 USD. Real problem at the moment is the exchange rate with = all the bank charges, the great Ozzie dollar is approx. half. Then = freight---- I see freight on a turbo from the US at up to $800 Oz = dollars!! Then internal freight in OZ, plus labour costs --- I will = have to sell 2 kidneys! > > Then considering I do not have a stock RX7 manifold = to bolt the turbo to =E2=80=93 I am manufacturing an adaption of the = stock Renesis manifold, so whatever turbo I get it means work to make = it fit and I am =C2=BE down that path. So having already having a = =E2=80=9Cdummy spit=E2=80=9D due to 12 months lost, I lauch out to find = a new turbo in OZ. I find that Garret and others have a hot section = wheel that will stand 1050 degrees C!! Wow that fixes anything that the = rotary puts out with no phone calls involved trying to explain. Once = again I make the usual; mistake telling the company with all these shiny = new turbos that I want it for a drone!! Thought that would by pass the = usual arguments---- silly boy, NO they do not supply for aeronautical = applications!! So I am back to =E2=80=9Cdune buggy=E2=80=9D even though = the nearest beach is 300 miles away. Seems the turbo I require is the = smallest they make. Price is yet to enter the discussion. > > Will update as I get abused. I am asked continually = for Make, Model, Vin Number, year of manufacturer! All I want is a = turbo! > > Thanks to all, > > Neil. > > =20 > > From: Rotary motors in aircraft =20 > > Sent: Friday, May 8, 2020 11:17 PM > > To: Rotary motors in aircraft > > Subject: [FlyRotary] Re: Turbos > > =20 > > Hi Neil, > > It all depends on how you size and operate your turbo. > > In general, the pressure relief, or pop-off valve is not needed in = aircraft. Those come more into play during the fast throttle closures = that occur in highly boosted race cars during shifting. They spend = almost all of their time closed. These valves are not intended to be = the primary pressure regulation and would not function well in such a = capacity. They only limit peak pressure but do not do so with a high = level of accuracy or control ability. They would also be highly = inefficient if used in this manner, as the turbo would be producing = continuously higher back pressure than needed. The turbo would be short = lived and your fuel consumption would suffer greatly. > > =20 > > The wastegate issue is a much bigger question but the short answer = is that yes, you probably want/need one. The only exception might be a = large turbine turbo that is sized so big that the max boost was only = achieved at WOT operating conditions. Even then, you would be limiting = the usefulness of your turbo at altitude because if it were sized for = WOT at sea level, it would not be very useful at altitude. If sized for = WOT at altitude you could use throttle to control boost down low, but = you always run the risk of overboost. Similarly, a fixed exhaust bypass = would allow a smaller turbo to be used in the same manner but with less = efficiency and shorter life. I have experimented with my turbo in this = configuration. By removing the flapper valve from my wastegate and = creating a fixed bypass I was able to run at WOT and have approximately = the boost I wanted, but only at a very specific altitude. Any higher = and boost drops off precepitously. Any lower and throttle is needed to = control boost. There is not much of a sweet spot as the natural = variations in conditions created a oscillating situation that is simply = not tolerable. But for maximum benefit from your turbo, longest life = and efficiency there is no substitute for a wastegate of some sort. > > =20 > > Dave Leonard > > N4VY, Turbo Rotary RV-6 > > =20 > > On Thu, May 7, 2020 at 2:47 PM 12348ung@gmail.com = wrote: > > Can anyone help me with the following? With a turbo, can I just = use a pressure relief valve and negate the wastegate totally?? = Looking for simplicity and weight saving. Neil. >=20 >=20 > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html