X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 09 Sep 2014 13:45:20 -0400 Message-ID: X-Original-Return-Path: Received: from nk11p08mm-asmtp001.mac.com ([17.158.58.246] verified) by logan.com (CommuniGate Pro SMTP 6.0.9e) with ESMTPS id 7136504 for lml@lancaironline.net; Tue, 09 Sep 2014 13:34:20 -0400 Received-SPF: pass receiver=logan.com; client-ip=17.158.58.246; envelope-from=gw5@me.com Received: from [10.20.39.131] (mobile-166-205-064-116.mycingular.net [166.205.64.116]) by nk11p08mm-asmtp001.mac.com (Oracle Communications Messaging Server 7u4-27.10(7.0.4.27.9) 64bit (built Jun 6 2014)) with ESMTPSA id <0NBN0019IA46RC20@nk11p08mm-asmtp001.mac.com> for lml@lancaironline.net; Tue, 09 Sep 2014 17:33:44 +0000 (GMT) X-Proofpoint-Virus-Version: vendor=fsecure engine=2.50.10432:5.12.52,1.0.28,0.0.0000 definitions=2014-09-09_07:2014-09-09,2014-09-09,1970-01-01 signatures=0 X-Proofpoint-Spam-Details: rule=notspam policy=default score=0 spamscore=0 suspectscore=0 phishscore=0 adultscore=0 bulkscore=0 classifier=spam adjust=0 reason=mlx scancount=1 engine=7.0.1-1402240000 definitions=main-1409090143 From: George Wehrung Content-type: multipart/alternative; boundary=Apple-Mail-50EC45D9-1C30-4160-9EC3-F8F80E19567A Content-transfer-encoding: 7bit MIME-version: 1.0 (1.0) Subject: Re: [LML] Re: Cabin Heat Valve Installation X-Original-Message-id: <7C835A03-080A-4B27-B869-2D59DE65EDB7@me.com> X-Original-Date: Tue, 09 Sep 2014 13:33:42 -0400 References: In-reply-to: X-Original-To: Lancair Mailing List X-Mailer: iPad Mail (11D257) --Apple-Mail-50EC45D9-1C30-4160-9EC3-F8F80E19567A Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: quoted-printable Thanks Grayhawk. That is my summation as well. Sent from my iPad > On Sep 9, 2014, at 13:27, Scott Krueger wrote: >=20 > Route the intput hot air from the leg of the T. At max deflection of the v= alve the output is either going out forward (summer) or going rearward into t= he cabin (cold winter). Intermediate settings are up to your needs. >=20 > Grayhawk >=20 >> On Tuesday, September 9, 2014, George Wehrung wrote: >> Can anyone send pics and or installation instructions for the cockpit hea= t valve located on the engine side of the firewall? >>=20 >> I and Lancair have tried to find the install manual but the only ones ava= ilable are for the pressurized ES' and IVs which use a turbo setup. The one w= e have is taking the heat from the exhaust muffler into tube facing the engi= ne compartment and venting through the downward tube of the T shape valve. T= he problem that I see is if the valve is cracked open because it did not ful= ly close is that heat is still coming into the cabin. >>=20 >> If I reroute the heat from the bottom the valve would have to be opened q= uite a bit to allow heat in. >>=20 >> Also, has anyone thought about bringing in outside air through the engine= compartment to behind the instrument panel to help cool the avionics? >>=20 >>=20 >>=20 >> Sent from my iPad >> -- >> For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.ht= ml --Apple-Mail-50EC45D9-1C30-4160-9EC3-F8F80E19567A Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: 7bit

Thanks Grayhawk. That is my summation as well.

Sent from my iPad

On Sep 9, 2014, at 13:27, Scott Krueger <grayhavvk@gmail.com> wrote:

Route the intput hot air from the leg of the T. At max deflection of the valve the output is either going out forward (summer) or going rearward into the cabin (cold winter). Intermediate settings are up to your needs.

Grayhawk

On Tuesday, September 9, 2014, George Wehrung <gw5@me.com> wrote:
Can anyone send pics and or installation instructions for the cockpit heat valve located on the engine side of the firewall?

I and Lancair have tried to find the install manual but the only ones available are for the pressurized ES' and IVs which use a turbo setup. The one we have is taking the heat from the exhaust muffler into tube facing the engine compartment and venting through the downward tube of the T shape valve. The problem that I see is if the valve is cracked open because it did not fully close is that heat is still coming into the cabin.

If I reroute the heat from the bottom the valve would have to be opened quite a bit to allow heat in.

Also, has anyone thought about bringing in outside air through the engine compartment to behind the instrument panel to help cool the avionics?

Sent from my iPad
--
For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html

--Apple-Mail-50EC45D9-1C30-4160-9EC3-F8F80E19567A--