X-CGP-ClamAV-Result: CLEAN X-VirusScanner: Niversoft's CGPClamav Helper v1.23.0 (ClamAV engine v0.103.0) X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=XpSExmN9 c=1 sm=1 tr=0 a=wgWIERYvTl7iGN6jnMCulQ==:117 a=55z/sxGcUIPVrBMYBb4HRw==:17 a=IkcTkHD0fZMA:10 a=3YhXtTcJ-WEA:10 a=x7bEGLp0ZPQA:10 a=_Z_nqdSeG58A:10 a=Ia-xEzejAAAA:8 a=_6GpL_ENAAAA:8 a=7g1VtSJxAAAA:8 a=TCIWbTgpjsP3Ni8PkKUA:9 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=grOzbf7U_OpcSX4AJOnl:22 From: " 12348ung@gmail.com" Received: from mail-pl1-f181.google.com ([209.85.214.181] verified) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 1461392 for flyrotary@lancaironline.net; Wed, 28 Apr 2021 17:50:54 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.214.181; envelope-from=12348ung@gmail.com Received: by mail-pl1-f181.google.com with SMTP id e2so29312318plh.8 for ; Wed, 28 Apr 2021 14:50:55 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=from:to:references:in-reply-to:subject:date:message-id:mime-version :content-transfer-encoding:content-language:thread-index; bh=raAWuQjJr8Q91aFCZR1nIPsgSYLii5Q74fWrY+c8Lbo=; b=LMuMGRcW/ON3T3dYR8fIcFcSnxcKeOT6ZVL37qrGoIhdWJr4dRzgTWCZKNzw1/H7US ep5iqu9P1DzT/XmUO+NR9wE9ryzVi/phFP6Lr3xvxJr4PWUSjRquqYvrOuWC/tcJ03WT 6SdpMm1M3j6LP8AwCrc3RtioBi4dDPhOGC1p1Wqge4QMTvzRZGq38u7vTYwzdfRVwND3 d0bUc2SEBLw/4WZcA7w6EKQAQ9YrFNFo01V+4cUX8caxiTaYqSDrsmbr0jYOj4TSSGRV JHQZin85rRcixtBhCQZ1Tw30eDvDAZkcZnaEC2Fpv/u6SWo/lIEJZ3OG8TtZrIfNP8te HVSQ== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:from:to:references:in-reply-to:subject:date :message-id:mime-version:content-transfer-encoding:content-language :thread-index; bh=raAWuQjJr8Q91aFCZR1nIPsgSYLii5Q74fWrY+c8Lbo=; b=j+NMmWN3UEQTy7wqaPn3+fhu10ovhXIcDvLqmiHLaqVbvIlDhAa+NCD7sFEunYMT7g bUsnbJLU6U26FkM3pZeH9Gh7b4BGf6NXejv0mrWREbx65bhVwoVssR7kRooSUPZx9/zf hw1iGDmc2H8IN255PlUCWdWPnrnl8BGdUjOGV5fxESS/qmHmLowc1bxWoWxOMbYkht7h QwzyV1Xqv+05C0eCNe9IOqZnkSvXCFe4t0cc6CnQS1MYJDBJppNq23v85cQ39px/72i4 lAFRoEfM9A7Cl0fYTV5UkB1zx204y+SYAaVDro29Cp+GO4jb6mnmj2/QXAiIG9cXotiW qGYQ== X-Gm-Message-State: AOAM530VnpOvt+YINCTZAMWet2b+OLMhAUi1/7OItn2u2nBVgOIynvFM elcgHx89Q20wkBf0bVqy5byvVX5tufOUVg== X-Google-Smtp-Source: ABdhPJwZ5zK+S94v6Yh/uSQTO5CkDVjKt4Nc/tIvwiOuDTGqUDADoMbolik7TipSTKByDcpn0H6zpQ== X-Received: by 2002:a17:902:ee11:b029:ed:7108:623e with SMTP id z17-20020a170902ee11b02900ed7108623emr5130626plb.38.1619646637033; Wed, 28 Apr 2021 14:50:37 -0700 (PDT) Return-Path: <12348ung@gmail.com> Received: from UserPC ([103.198.24.78]) by smtp.gmail.com with ESMTPSA id d12sm399068pjj.50.2021.04.28.14.49.54 for (version=TLS1_2 cipher=ECDHE-ECDSA-AES128-GCM-SHA256 bits=128/128); Wed, 28 Apr 2021 14:50:04 -0700 (PDT) To: "'Rotary motors in aircraft'" References: In-Reply-To: Subject: RE: [FlyRotary] EGT probes location Date: Thu, 29 Apr 2021 07:49:46 +1000 Message-ID: <004901d73c78$726717e0$573547a0$@gmail.com> MIME-Version: 1.0 Content-Type: text/plain; charset="UTF-8" Content-Transfer-Encoding: quoted-printable X-Mailer: Microsoft Outlook 16.0 Content-Language: en-us Thread-Index: AQHm2pSYmOJt51PHNBonl02BwzuQmKqrOY7g Finn, I spent too much time with EGT's. I kept worrying myself = to death as the temps got to 1800 degrees. Was told they should not get = over 1600. Kept in touch with another bloke who had no EGT's and when = he finally pulled his engine apart --- no damage whatever. Whether he = managed to run cooler ??? Now fitting turbo and the EGT probe will be after the turbo. That way = I will feel much better?? If cooler readings Regards, =20 Neil. -----Original Message----- From: Rotary motors in aircraft =20 Sent: Thursday, April 29, 2021 7:30 AM To: Rotary motors in aircraft Subject: [FlyRotary] EGT probes location So, I'm using the Renesis stock exhaust manifold. Tried to mount the EGT probes as close as possible and same distance = from the ports. However, at high power I'm seeing as much as 120F higher on rotor 2. Exhaust gas from rotor 1 passes by rotor 2 exhaust port so I'm wondering = if that somehow increases rotor 2 EGT readings. Caught my attention today when EGT2 got above 1,800F at 6,200 RPM and 161 mph TAS @ 3,300' density altitude. Any of you that's using the stock exhaust manifold run into this? Finn --- This email has been checked for viruses by Avast antivirus software. https://www.avast.com/antivirus -- Homepage: http://www.flyrotary.com/ Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html