X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=BpPjPrf5 c=1 sm=1 tr=0 a=s7do9I3oYpzFMb2JXGrRmQ==:117 a=jwdzGWXwq1FKgEr3WMqByA==:17 a=jpOVt7BSZ2e4Z31A5e1TngXxSK0=:19 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=Jdjhy38mL1oA:10 a=pGLkceISAAAA:8 a=Ia-xEzejAAAA:8 a=o1OHuDzbAAAA:8 a=7g1VtSJxAAAA:8 a=I6UqoNSsRDEzO18D-xIA:9 a=_9F4x4W7pjf8VTlE:21 a=3SjOeeOwmWz8t255:21 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=5YQ6H4ZxyGn-KoBYtt8s:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pg1-f179.google.com ([209.85.215.179] verified) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 13377049 for flyrotary@lancaironline.net; Thu, 09 Jan 2020 02:18:58 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.215.179; envelope-from=stephen.izett@gmail.com Received: by mail-pg1-f179.google.com with SMTP id z124so2758330pgb.13 for ; Wed, 08 Jan 2020 23:19:00 -0800 (PST) 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=vb6QuLlIv+VwKNvs7LABoO1AVGZ+h3QUSVGFiDmP6oY=; b=iOR9gA0ZijkRt6cgKAXJknMmpP2KKcPTSxOrHmUZcYJXx99+oF4JEGd37//3J286+y 9SoSCV0+5SC7otfeqJEtYmXqzPDzqgBJboE737hQtkFdmbj7HacjcKWsj+2Tlp3dcA4h LYh8iY2X/kcVQj2jKNFS7EvmUTyPfM1eVwXKptOjdH/uI08b7WXIpMUH8qafFdRdEGA6 hwVI7tUUKQmQVTMLuLNZ1AX1klwLHTWdojsj503KjgnXybA7TYeHmyysJLUQmxJaaBeB BrfAjU594gq3rBQ0sOk7q1rztCINO8G2dmwJzaRQEJ8Ed6WfOWTHXW32rJmNx8g/jaRy YJMw== 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=vb6QuLlIv+VwKNvs7LABoO1AVGZ+h3QUSVGFiDmP6oY=; b=B+/GZNqJ/dyPLmk8LnS1r+N+yvsO6Op0wlUAW4Iid1AnlsMEmPCzZuETNAasQcQsAE BjWR9BNu5e+z2b4Wh0684pP0m5RwBIaB88IhzyTG/r+P2CvmiN8GNSToz/yKNSe8yH8E 2ykUcuNnEeE/+TnaH9TtpmIjnV4VUZFGIzoomEKxT8ZnRuyyPy3W2AMeLdVIVqO/sqKl Yzc8Xa+IDGanIakxWX3/3Xif/gmjQQspNcjIW4s0XSsvmdIU6qf2MU/IpPg7R8/470Z8 8Q9+wFQGhcfwPbXLIEz595SBR9WPer6a4+SMvKyIJS7g30lZiNBYD2IUtO2RCiWqRyVB 8otg== X-Gm-Message-State: APjAAAXlcbfzK5jF+8SDUaZNe2eGibxkwdLsCeYAndXRL3MLR+HJ/SBx n1Cl2C6zRmdjx3fHtHQE06QoC8wz X-Google-Smtp-Source: APXvYqx5KaPiiXel65Gnyz3zUOj102J1ekhzniPiReeaFu+4J9dZaksmPErUFhF0+3NsolrMA5twOg== X-Received: by 2002:a65:66ce:: with SMTP id c14mr10032629pgw.262.1578554321654; Wed, 08 Jan 2020 23:18:41 -0800 (PST) Return-Path: Received: from macbook-pro.lan ([118.208.171.56]) by smtp.gmail.com with ESMTPSA id l9sm5666208pgh.34.2020.01.08.23.18.39 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Wed, 08 Jan 2020 23:18:41 -0800 (PST) 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: Using the EM3's EGT/CHT inputs for reading MPX10 pressure sensors Date: Thu, 9 Jan 2020 15:18:37 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: X-Mailer: Apple Mail (2.3445.104.11) Hi Charlie I was thinking of referencing everything to the aircrafts static system = and reading air pressure (not pitot as in velocity) so as to determine = the pressures around the cowl. So perhaps various points in front of an exchanger cores and various = points behind the cores. This would then give us the flow through the cores. =20 Thanks Matt for highlighting the cheap modules available. So you=E2=80=99ve got me thinking: Why not use a barometric sensor (absolute) unit with pressure and temp = at the location your wanting to measure, rather than a hose back into = the cockpit or micro. As an example, the BMP280 has a pressure range 300-1100 hPa =3D 4.35 - = 15.95 psi. So this unit can measure a pressure of 1.25psi above atmospheric at sea = level and progressively higher pressures at higher altitudes. They can handle up to 85C or 185F which I thought would be OK. Unfortunately the units appear to have a fixed I2C address, so we = can=E2=80=99t simply daisy chain them and address them in software. It looks like they will require a hard Chip Select for each device. So what about a small multicore from a micro (arduino or micromite etc) = through the firewall to a node with connectors for any number of sensors = to reticulate around the cowl. Each of these connectors has its own Chip Select line from the micro so = each is addressable. Another of these units could be connected to the static of the aircraft = to provide a local pressure reference for all measurements. It looks like I could get 10 such boards for $20AUD on eBay. Does this make sense? Steve Izett > On 9 Jan 2020, at 10:02 am, Charlie England ceengland7@gmail.com = wrote: >=20 > On the subject of static source, are we talking about measuring = cooling air *velocity* inside the ducts, etc? If so, I believe that = you'll need to put the static source in the same air as the pressure = ('pitot') source. >=20 > If you're looking for pressure ('piccolo tubes') differential, then = I'd think you'd want a differential sensor with one port in the high = pressure plenum area and the other in the exit plenum, which likely will = also be at a higher pressure than the a/c's static pressure. >=20 > FWIW, >=20 > Charlie >=20 > On 1/8/2020 5:47 PM, Stephen Izett stephen.izett@gmail.com wrote: >> Thanks very much Finn >>=20 >> Thats what I was a after. >> As you mention, I=E2=80=99m not needing hi res data to understand = whats happening in the cowl and ducts at various speeds. >> Unfortunately I removed the data log option years ago (not enough = space in that panel) and the Skyview logs the engine data well. >>=20 >> Do you have the schematics for the EC2 and 3? & EM3? >>=20 >> I thought it was just a question of whether I wanted to spend the = extra time knocking up a string of amps for the 5 sensors I=E2=80=99ve = got. >> But after thinking about it overnight, displaying the data in the = cockpit is no where near as helpful as logging and analysing the data on = the ground. >> I use a micromite system so the reading and writing to a mem card = will be simple. >> The benefit of building a little batt powered unit as you suggested = Matt is we could use it to diagnose other=E2=80=99s temp issues. >>=20 >> So you guys have been helpful as usual. >> With my 5 MPX10DP sensors we could log airspeed and 4 pressure inputs = referenced to the ships static. >> Perhaps temps for each press input would be helpful as Matt = suggested. >>=20 >> Being realistic, I=E2=80=99m a bit slow, so I would need a week to = fab it all up. >> But it would be super helpful to me and possibly many others. >> Only over the weekend we had a first flight of a lyc powered machine = put down in a field adjacent to our strip due to overheating. = Fortunately both pilot and machine were unscathed. >>=20 >> Cheers >>=20 >> Steve Izett >>=20 >>=20 >>=20 >>=20 >>=20 >>=20 >>=20 >>=20 >>> On 8 Jan 2020, at 11:58 pm, Finn Lassen finn.lassen@verizon.net = wrote: >>>=20 >>> I thought about 3D printing a pressure multiplexer to be driven by a = stepper motor. >>>=20 >>> Imagine an 8 point ignition distributor. >>>=20 >>> You wouldn't have 8 real time pressure sensors, but I guess 1 second = on each input should be enough for pressure to stabilize enough for = measurement. So sampling all 8 inputs would take 8 seconds. >>>=20 >>> Commercially available but much more expensive than buying 7 extra = sensors. >>>=20 >>> Should be a fun Arduino project. >>>=20 >>> Finn >>>=20 >>> On 1/8/2020 10:17 AM, Matt Boiteau mattboiteau@gmail.com wrote: >>>> Temp sensors are cheap, but pressure sensors are $15-20??each. >>>=20 >>=20 >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html >=20 >=20 > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html