X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 05 Nov 2012 11:37:56 -0500 Message-ID: X-Original-Return-Path: Received: from hrndva-omtalb.mail.rr.com ([71.74.56.122] verified) by logan.com (CommuniGate Pro SMTP 6.0c2) with ESMTP id 5854183 for lml@lancaironline.net; Fri, 02 Nov 2012 13:13:44 -0400 Received-SPF: none receiver=logan.com; client-ip=71.74.56.122; envelope-from=Wolfgang@MiCom.net X-Original-Return-Path: X-Authority-Analysis: v=2.0 cv=YP4dOG6x c=1 sm=0 a=MHZY6FYWMEQOp7S43i2QIw==:17 a=3Zlka_XeuxsA:10 a=1Nt-obXqJp8A:10 a=ttCsPuSJ-FAA:10 a=8nJEP1OIZ-IA:10 a=rTjvlri0AAAA:8 a=yfr4iLUR9bAA:10 a=tYZPWW6eAAAA:8 a=Ia-xEzejAAAA:8 a=-QidQ3XyAAAA:8 a=biznXsr5AAAA:8 a=r72B6LDeAAAA:8 a=pGLkceISAAAA:8 a=cd07KHIZkmijxbbh1GoA:9 a=wPNLvfGTeEIA:10 a=MHJMZBy3EKEA:10 a=CVU0O5Kb7MsA:10 a=b1KJu6T2Jp8A:10 a=EzXvWhQp4_cA:10 a=A0LnVcZjDxIA:10 a=amP8cGQ10gkA:10 a=5tig-d09KFAA:10 a=MSl-tDqOz04A:10 a=MHZY6FYWMEQOp7S43i2QIw==:117 X-Cloudmark-Score: 0 X-Originating-IP: 74.218.201.50 Received: from [74.218.201.50] ([74.218.201.50:3356] helo=lobo) by hrndva-oedge01.mail.rr.com (envelope-from ) (ecelerity 2.2.3.46 r()) with ESMTP id 8E/88-12302-52FF3905; Fri, 02 Nov 2012 17:13:09 +0000 X-Original-Message-ID: <0B72068E8E424CF394993E7FB604FBE9@lobo> From: "Wolfgang" X-Original-To: References: Subject: Re: [LML] Re: Performance Data Walter Engine X-Original-Date: Fri, 2 Nov 2012 13:13:21 -0500 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.5512 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5512 A quick and easy way to compare airframes for efficiency is; K = IAS^3 X Weight / HP You can use fuel burn instead of HP if that's more convenient. Wolfgang ----- Original Message ----- From: "RONALD STEVENS" To: Sent: Thursday, November 01, 2012 2:42 PM Subject: Re: [LML] Re: Performance Data Walter Engine > Well, I think I have one of the most heaviest 4p's out there (BRS > (parachute like Cirrus), Amsafe, De-ice, Reversible Prop etc etc), and my > realistic numbers are > > 17500ft, MAP32, 2500RPM, 18.2gph, TIT <1610, CHT<350 cruising 245kts with > FULL FUELL and 2 persons (big ones lol), 250kts with fuel at 1/2 tanks (so > weight does matter a lot). > > Ronald (>200 hours IV-p, 340 Velocity, 1100 Cirrus SR22) > > On 11/1/12 12:20 PM, "Bob Rickard" wrote: > >>John >> >>I flew my IV-P with a BPE overhauled engine yesterday at 210, 31"MAP, >>2500rpm, 17gph, indicating 255 KTAS. And my airplane is slower than >>most I think. So that is realistic. >> >>Bob R >> >>On Nov 1, 2012, at 7:58 AM, "John Barrett" wrote: >> >>> Have I missed something? Have not flown my IVP at FL220 yet, but >>>economy >>> cruise I've heard about could be about 28" MAP burning 16-18 GPH and >>>around >>> 260 kts TAS. Are those numbers realistic? >>> >>> John Barrett >>> N31VP - waiting for BPE engine overhaul completion. >>> >>> -----Original Message----- >>> From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of >>>Dr. >>> Weinsweig >>> Sent: Wednesday, October 31, 2012 5:50 AM >>> To: lml@lancaironline.net >>> Subject: [LML] Re: Performance Data Walter Engine >>> >>> After Ronald asked about pulling back the power on a propjet, I >>>experimented >>> a bit. >>> >>> On a recent flight at fl220, I pulled the power back to burn 23-25 gph >>>and >>> maintained in the 160's kias and 230's ktas in my TKS equipped propjet. >>> >>> Almost piston efficiency. Watta Plane!!!! >>> >>> David Weinsweig >>> N750DW Propjet >>> >>> >>>>>> weinsweigd@tsnci.com 10/23/2012 4:59:28 PM >>> >>> Hi Ronald, >>> >>> Each propjet has somewhat different performance. Mine with tks deicing >>> generally flies between 275-300 ktas in the flight levels. fuel burn is >>> 29-39 gph depending on altitude and power settings. >>> >>> as a baseline I just flew from key west nonstop to huntington, wv at >>> fl210 due to strong headwinds and power pulled back some to conserve >>>fuel >>> and range. I burned 29gph with a true of around 275 ktas in 3;42 nonstop >>> burning through my wing fuel (112 gallons) but still having 34 gallons >>>in >>> the belly tank when i landed. I've done this same flight previously in >>>3:10 >>> but the winds sucked on Sunday. I have found that the turbine engines >>>just >>> burn fuel and 25 gph may be a little low to maintain any speed though I >>>do >>> get that low on descents. They burn close to that at idle. >>> >>> I'd be happy to discuss the good and bad of turbines and the conversion >>> options/shops with you if you'd like as I have had both good and bad >>> experiences. >>> >>> David Weinsweig >>> N750DW Propjet >>> 304-633-5221 >>> weinsweigd@gmail.com >>> >>> >>> >>>>>> ronald@sdc.com 10/22/2012 10:13:17 AM >>> >>> Hello guys >>> >>> Today I flew in a Bonanza with an Allison 250 Turbine, and it was >>>awesome. I >>> was very impressed by performance and the silence and no vibration. >>> >>> So I got curious now about having a Walter Conversion done, but when I >>>was >>> looking for performance data (cruise/fuel flow/ economic or power @ >>> altitudes) I could not find anything on the web?! >>> >>> For example I like flying @ 17500ft, just because I can listen to the >>>radio >>> and do not have to chatter and can avoid bumps when I see one lol >>> >>> So what does a walter engine burn at this altitude? Could it fly with >>>just >>> 25gph and what would be its performance? >>> Things like that... >>> >>> So does anyone have this ? And is there anyone I could fly with (I pay >>>for >>> fuel) who can show me this in his 4p? (I live in Central Florida, but I >>>have >>> a 4p ;) >>> >>> Thanks -- Ronald >>> >>> -- >>> For archives and unsub >>> http://mail.lancaironline.net:81/lists/lml/List.html >>> >>> -- >>> For archives and unsub >>> http://mail.lancaironline.net:81/lists/lml/List.html >>> >>> -- >>> For archives and unsub >>>http://mail.lancaironline.net:81/lists/lml/List.html >>> >>> >>> -- >>> For archives and unsub >>>http://mail.lancaironline.net:81/lists/lml/List.html >> >>-- >>For archives and unsub >>http://mail.lancaironline.net:81/lists/lml/List.html >> > > > >