Return-Path: Sender: (Marvin Kaye) To: lml Date: Mon, 30 Jun 2003 08:31:34 -0400 Message-ID: X-Original-Return-Path: Received: from mta9.srv.hcvlny.cv.net ([167.206.5.42] verified) by logan.com (CommuniGate Pro SMTP 4.1b8) with ESMTP id 2449321 for lml@lancaironline.net; Mon, 30 Jun 2003 01:07:15 -0400 Received: from asv2.srv.hcvlny.cv.net (asv2.srv.hcvlny.cv.net [167.206.5.51]) by mta9.srv.hcvlny.cv.net (iPlanet Messaging Server 5.2 HotFix 1.16 (built May 14 2003)) with ESMTP id <0HHA00EMW3JKST@mta9.srv.hcvlny.cv.net> for lml@lancaironline.net; Mon, 30 Jun 2003 01:06:56 -0400 (EDT) Received: from ValidationPartners.com (ool-18bb9fce.dyn.optonline.net [24.187.159.206]) by asv2.srv.hcvlny.cv.net (8.12.9/8.12.9) with ESMTP id h5U56ooY024455; Mon, 30 Jun 2003 01:06:51 -0400 (EDT) X-Original-Date: Mon, 30 Jun 2003 01:08:55 -0400 From: Adam Molny Subject: Re: [LML] Legacy sequenced gear doors X-Original-To: "Jeffrey W. Skiba" X-Original-Cc: Lancair X-Original-Message-id: <3EFFC5E7.2B4C8553@ValidationPartners.com> MIME-version: 1.0 X-Mailer: Mozilla 4.7 [en-gb] (Win98; U) Content-type: text/plain; charset=us-ascii Content-transfer-encoding: 7BIT X-Accept-Language: en References: <519194EBBDF7D2118C6000A0CC412E330FEEFB@EXCHANGE> Hi Jeff - Disclaimer - I am an idiot, I know nothing, and I have never built a plane before. No, you're not smoking anything -- these are legitimate concerns. I figured someone would catch the leakage thing. The rate you mention is measured at 5000psi. We operate at 1000psi or less. Does that mean the leakage rate would be proportionately lower? Did the manufacturer spec a worst case scenario with worn O-ring seals? I don't know. I will have to do more research to see if other brands have similar leakage. For our systems, you really want the leakage rate to be nil. An internal leak (either at the valve or in one of the cylinders) causes pressure to bleed from the high side to the low side. When the pressure drops enough, the pump kicks in for a few seconds to restore it. This should happen before the pressure drops enough to let the gear or doors sag down. People have complained about the pump kicking in every few minutes for the duration of the flight. This is probably not acceptable. >From the gear test videos I have seen, the doors open MUCH faster than the gear. Of course, this is with the plane on jacks. Things may behave differently in flight when aerodynamic loads are applied. In any case, this is not a safety-critical issue. If the gear hits the door, it would cause cosmetic damage only, and the gear should still extend when needed. I looked at using a sequence valve to block the gear from coming up, but the parts count, plumbing, and complexity start to skyrocket! In order to block the gear from coming up, you have to know when the doors are fully down. This means you must either add another pair of microswitches, or somehow actuate the sequence valve's plunger when the door reachs the full open position. If you use microswitches, you will need an electrically controlled blocking valve. If the valve sticks in the blocked position, the emergency gear extension won't work. So now, you need a blocking valve that is fail-safe. I'm sure there is a way to do it. North American did it on the P51 Mustang 60 years ago! BTW, I purchased the Mustang maintenance manual on CD-ROM as part of my research. They also use a single valve to control both gear doors. The valve's directional control plunger is operated by mechanical linkages connecting it to the main gear legs. The main gear have spring-loaded down lock pins. The pins retract when hydraulic pressure rises enough to overcome the springs. That pressure spike happens when the doors hit their stops at the fully open position. During the first phase of gear extension, my system works the same as a normal Legacy. Therefore, I will be vulnerable to the same rubbing problem. Overall, this is a complex problem, and I'm sure there are lots of subtle gotcha's out there. I'll keep plugging away at it. -Adam "Jeffrey W. Skiba" wrote: > > I have been thinking about doing this on my legacy for some time, I have my > gear working (mains). > > Some things I first noticed that I ran into while trying to do this.... > Your spool valve has 82cc/minute internal leakage (5cu in./minute) Do you > think that's okay ?? I am no engineer but if it leaks within the valve will > it not want to start to pressurize the side you do NOT want pressurized?? > Maybe you can stop that with another valve that opens the side that should > not have pressure to the return line ??? > > Next, > I upgraded my Hydraulic pump to the high capacity pump, which now by the way > comes standard on the Legacy kit, it takes gear cycle time from 10-12 > seconds to like 6-8 !!! And sometimes even faster, so I would be very > careful about the door closed gear out and then go to retract. Maybe you > might want to stop pressure to the gear UP until the inner door is fully > opened??? > > Next side note, The Regular Stock gear system on the Legacy during normal > powered gear extension has a tendency to rub the inner gear doors by the > main wheels. ( I have been told this by Mark Manke that it's one of those > "things") > > I really hope you can tell me the issues I bring up, you already thought > about and I am smoking something because I would love to have a system like > this.... Need any help testing ??? I would be happy to help... > > I will pull out my old diagrams from when I was kicking it around and see if > I can think of anything else.... > > Jeff Skiba > Legacy #191