X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=G+5i7Os5 c=1 sm=1 tr=0 a=JFLq0Zg074/TNoPlXaVJig==:117 a=x7bEGLp0ZPQA:10 a=DDNF8ybvv5wA:10 a=xqWC_Br6kY4A:10 a=J70Eh1EUuV4A:10 a=_EeEMxcBAAAA:8 a=Ia-xEzejAAAA:8 a=o1OHuDzbAAAA:8 a=pGLkceISAAAA:8 a=7g1VtSJxAAAA:8 a=vXYAmHiu0tKokZ0umMsA:9 a=CjuIK1q_8ugA:10 a=Qa1je4BO31QA:10 a=5UeK9suJl1gA:10 a=gvSQh4r-fQ0A:10 a=LZQimvQx6xhWh2wU:21 a=_W_S_7VecoQA:10 a=frz4AuCg-hUA:10 a=ya5i7YzpaYYA:10 a=syqr5EOPB93U0NEwqYpB:22 a=Urk15JJjZg1Xo0ryW_k8:22 a=5YQ6H4ZxyGn-KoBYtt8s:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Le Roux Breytenbach breytenbachleroux@gmail.com" Received: from mail-ed1-f42.google.com ([209.85.208.42] verified) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 12967039 for flyrotary@lancaironline.net; Tue, 17 Sep 2019 15:51:19 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.208.42; envelope-from=breytenbachleroux@gmail.com Received: by mail-ed1-f42.google.com with SMTP id f20so2011278edv.8 for ; Tue, 17 Sep 2019 12:51:20 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=from:to:subject:thread-topic:thread-index:date:message-id :accept-language:content-language:mime-version; bh=+XN1Hbmd9Ki89AwsK9SQ6e4SErYTB2hLmEhsD44yLbg=; b=LODShLPuJKZmdUdAMMqL3rannlKPwMnZ9Ym7IQx92co6q4gZCZyNeB5xey6Wh1DbB3 Ad9Nzg+Q85bv/c1j2tNSNQ+9u70DO0mD1G3HntYyryVVD2nEREriQ9InKxHrOL36S/vb 5pfMB393VMV8mnfJEkO4WG2MpW5M8Sdhm2Lyhsn64yBaRlWVMj/3WoHw2HK0Cb9SKvZf A6dXRZoG6Uf4vAiEZh3Q2bQhJm0GHl0Rpm5fmxQlS/YMWTIY4sZdmfIQflxBdsR3WonO /TWR8/zTW5tw73u4zXXYtGUJ6VqCiK85X0lC+nq6gXZV6IRAyzTdTZbaa3KQp5V28dbJ /Tpg== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:from:to:subject:thread-topic:thread-index:date :message-id:accept-language:content-language:mime-version; bh=+XN1Hbmd9Ki89AwsK9SQ6e4SErYTB2hLmEhsD44yLbg=; b=ctCGXxrRz7bOxV6eY8Dyge3zrgklAQ8BdtCpsiymKv9e8V47Ads9uWBnUnWyVq4Kem e0/4s+GLQYlZqNtFMhYudxvKyllc1TlwSzbu2siQXro5syQY3BnU0K1Upc70IgVdrpIa oMSpF1m0FrySitaEJZo/GPnnR8OyOjBtZltbBkKzYuzAD1IS3blWXnTpDCTs/xUoEc+t Om4EUkBDfeqg+hbxxn1wzoS3cCEcVYeCKlQ3nf4sawGGna1HB246xuRWppAbLeVzC1xC S5MPVfryw2QWvOuJ7BEfGkxbHYINQ577X0bAs0tT/QUYR1XWytU2XLdb/1YMEMy9N6iF cVYg== X-Gm-Message-State: APjAAAUv1d2U8dGIKVsnHRllN8wdVH18Uulm2p/4xg14Y+ZbZ+Tqzp0F v8RgMuFVAUoUeIoLb2tvt9TxW3LO X-Google-Smtp-Source: APXvYqxRopvWKIJd3Vnuw7020OI0gXBKn8uQkVTjhF/XnnRwpBNIBmDIzuIRSQbWuuzVyq/9fsNUcA== X-Received: by 2002:a50:f19c:: with SMTP id x28mr6488070edl.42.1568749861778; Tue, 17 Sep 2019 12:51:01 -0700 (PDT) Return-Path: Received: from SN1PR12MB2398.namprd12.prod.outlook.com ([2603:1036:802:6::5]) by smtp.gmail.com with ESMTPSA id f8sm384131ejk.30.2019.09.17.12.51.00 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Tue, 17 Sep 2019 12:51:00 -0700 (PDT) To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Renesis intake parts Thread-Topic: [FlyRotary] Re: Renesis intake parts Thread-Index: AQHVbY5QfBpZndmBpkCX4j2JCJx8uw== X-MS-Exchange-MessageSentRepresentingType: 1 Date: Tue, 17 Sep 2019 19:50:58 +0000 Message-ID: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-Exchange-Organization-SCL: -1 X-MS-TNEF-Correlator: X-MS-Exchange-Organization-RecordReviewCfmType: 0 Content-Type: multipart/alternative; boundary="_000_SN1PR12MB239858E9D270D9826BB68CC3FD8F0SN1PR12MB2398namp_" MIME-Version: 1.0 --_000_SN1PR12MB239858E9D270D9826BB68CC3FD8F0SN1PR12MB2398namp_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Yes Finn : Planned to use rtv with bolts and nuts all around the flange. Just want to oppened it periodically for inspections when needed. Yes the flange is also on top as i planned to turn the 13B - 90 degrees ( = plugs up) so the intakes stand upright.Then the TB (Throttlebody ) face the= inlet duct.Want to make use of the "ram effect " of the incoming air to th= e TB and filter. This makes the hot exhaust easier to exit without complexity in turnes and = bends underneath the engine. Side radiator with "gills" on the side for hot air to exit on the side of t= he cowl.Think that the "suction effect" of the laminar flo of air over the = vents will help with the pressure drop inside the cowl. Well this is what i planned and want to do.. The proof is in the pudding and must be tested first. There is always a compromise, if i want to do one thing then must give up o= n another. Le Roux Get Outlook for iOS ________________________________ From: Rotary motors in aircraft on behalf of = Finn Lassen finn.lassen@verizon.net Sent: Tuesday, September 17, 2019 9:19 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Renesis intake parts Don't see why it shouldn't last: 1) It's round (assuming end opposite throttle body is a hemisphere) 2) Fiberglass doesn't fatigue like alum, right? Weak point would be at the flange. Are you planning on using RTV or some ot= her adhesive? I'm at the point where I need to construct the plenum. However the flange m= oves it closer to the engine. Maybe I can I can put the removable cover on = top? Finn On 9/17/2019 12:48 PM, Le Roux Breytenbach breytenbachleroux@gmail.com wrote: This is my custom intake plenum must still do the 2 intakes from the plenum= . What is your predictions will it last on the rotary pulses ? 8 layers of bidirectional cloth the "pipe" On Fri, Sep 13, 2019 at 10:49 PM Steven W. Boese SBoese@uwyo.edu wrote: The images show the intake parts used for the tests in the previous message= . Steve Boese -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.= html -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.= html --_000_SN1PR12MB239858E9D270D9826BB68CC3FD8F0SN1PR12MB2398namp_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable
Yes Finn : Planned to use rtv with bolts and n= uts all around the flange.
Just want to oppened it periodically for inspe= ctions when needed.
Yes the flange is also on top as i planned to = turn the 13B  - 90 degrees ( plugs up) so the intakes stand upright.Th= en the TB (Throttlebody ) face the inlet duct.Want to make use of the "= ;ram effect " of the incoming air to the TB and filter.
This makes the hot exhaust easier to exit with= out complexity in turnes and bends underneath the engine.
Side radiator with "gills" on the si= de for hot air to exit on the side of the cowl.Think that the "suction= effect" of the laminar flo of air over the vents will help with the p= ressure drop inside the cowl.
Well this is what i planned and want to do..
The proof is in the pudding and must be tested= first.
There is always a compromise, if i want to do = one thing then must give up on another.

Le Roux




Get Outlook for iOS
 
From: Rotary motors in airc= raft <flyrotary@lancaironline.net> on behalf of Finn Lassen finn.lass= en@verizon.net <flyrotary@lancaironline.net>
Sent: Tuesday, September 17, 2019 9:19 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Renesis intake parts
 
Don't see why it shouldn't last:
1) It's round (assuming end opposite throttle body is a hemisphere)
2) Fiberglass doesn't fatigue like alum, right?
Weak point would be at the flange. Are you planning on using RTV or some ot= her adhesive?

I'm at the point where I need to construct the plenum. However the flange m= oves it closer to the engine. Maybe I can I can put the removable cover on = top?

Finn

On 9/17/2019 12:48 PM, Le Roux Breytenbach breytenbachleroux@gmail.com wrote:
This is my custom intake plenum must still do the 2 intakes from the p=
lenum.=0A=
What is your predictions will it last on the rotary pulses ?=0A=
8 layers of bidirectional cloth the "pipe"=0A=
=0A=
On Fri, Sep 13, 2019 at 10:49 PM Steven W. Boese SBoese@uwyo.edu=0A=
<flyrotary@lancaironline.net> wrote:=0A=

The images show the intake parts used for the tests in the previous me=
ssage.=0A=
=0A=
Steve Boese=0A=
--=0A=
Homepage:  http://www.flyrotary.com/=0A=
Archive and UnSub:   http://mail.lancaironline.=
net:81/lists/flyrotary/List.html=0A=



--=0A=
Homepage:  http://www.flyrotary.com/=0A=
Archive and UnSub:   http://mail.lancaironline.=
net:81/lists/flyrotary/List.html=0A=


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