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12-15-2007, 11:34 PM
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Join Date: Jan 2006
Posts: 934
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Lyc Wet Dog Shake
Any idea how much, in inches, a lyc will shake on shutdown at the outboard edges?
Jim
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12-16-2007, 03:08 AM
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Join Date: Jan 2005
Posts: 4,283
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Depends
Sorry there was a thread where someone posted a deflection, could not find it. But it depends on engine, prop and brand/type engine vibration isolators. The deflection depends on where you measure it. I think most of the movement is rotational. If you are looking for gap between baffles and cowl, follow the plans. I think there are some clearances in there.
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George
Raleigh, NC Area
RV-4, RV-7, ATP, CFII, MEI, 737/757/767
2020 Dues Paid
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12-16-2007, 05:58 AM
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Join Date: Apr 2006
Location: south carolina
Posts: 1,111
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looks like
Quote:
Originally Posted by Jim P
Any idea how much, in inches, a lyc will shake on shutdown at the outboard edges?
Jim
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about 2 inches total (1up and 1down) could be more probally less. this is my concern for the fuel pump to flow meter hose.. that hose is suppose to be flexible but its not so flexible as to not wiggle the gascolator/fuel flow assy. remember the baffles are only 3/8 from the cowl so it cant be as much as the video shows..i hope.
http://www.youtube.com/watch?v=yoX4KEXVuFo watch at 6.23
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William Weesner/ still kicking.
Last edited by cytoxin : 12-16-2007 at 06:02 AM.
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12-16-2007, 06:37 AM
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Join Date: Oct 2005
Location: Savannah, GA
Posts: 1,849
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From what I saw in the video it looked like it hardly deflectedz! The whole plane deflected but I think the engine stayed pretty still in regards to the airframe.
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Todd
N110TD
RV-10 Vesta V8 LS2/BMA EFIS/One formerly flying at 3J1 Hobbs stopped at 150 hours
Savannah, GA and Ridgeland, SC
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12-16-2007, 06:41 AM
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Join Date: Apr 2006
Location: south carolina
Posts: 1,111
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look again
Quote:
Originally Posted by TSwezey
From what I saw in the video it looked like it hardly deflectedz! The whole plane deflected but I think the engine stayed pretty still in regards to the airframe.
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full screen the video if you did not and you will see the more than obvious relative motion. it moves, and a good bit at that.just as you hear the implulse coupling click. however i dont know what type of mounts he's using. vip v/s lords ??
edit : the best ground run video ive seen yet and perfect timing BTW for my concerns...like he read my mind.
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William Weesner/ still kicking.
Last edited by cytoxin : 12-16-2007 at 06:44 AM.
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12-16-2007, 06:47 AM
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Join Date: Mar 2005
Location: Dallas area
Posts: 10,762
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Depends on a lot of things.
The heavier the prop, the softer the mounts, the higher the compression, the more the shake.
__________________
Mel Asberry, DAR since the last century.
EAA Flight Advisor/Tech Counselor, Friend of the RV-1
Recipient of Tony Bingelis Award and Wright Brothers Master Pilot Award
USAF Vet, High School E-LSA Project Mentor.
RV-6 Flying since 1993 (sold)
<rvmel(at)icloud.com>
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12-16-2007, 07:08 AM
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Join Date: Sep 2005
Location: Maple Grove, MN
Posts: 2,331
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The majority of motion on my engine seems to be rotational during startup or shutdown. I have an O360 C/S prop, with non-aerobatic mounts. I would estimate that the valve covers, during this rotational motion, move up and down maybe 1/4 to 3/8" from their rest position. Certainly no more. My baffles have 1/2" clearance, and there is no sign that they've hit the cowl. The center of the engine, just behind the prop, moves up and down perhaps 1/8".
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Alex Peterson
RV6A N66AP 1700+ hours
KADC, Wadena, MN
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12-16-2007, 08:29 AM
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Join Date: Sep 2006
Location: Sedalia,KY
Posts: 252
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Quote:
Originally Posted by cytoxin
about 2 inches total (1up and 1down) could be more probally less. this is my concern for the fuel pump to flow meter hose.. that hose is suppose to be flexible but its not so flexible as to not wiggle the gascolator/fuel flow assy. remember the baffles are only 3/8 from the cowl so it cant be as much as the video shows..i hope.
http://www.youtube.com/watch?v=yoX4KEXVuFo watch at 6.23
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Seriously off topic guys, and I apoligize, but can anyone identify the pickup truck in that video? I can't tell what it is. PM me if you know so the thread does not get hijacked.
Thanks
Josh
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"Shake the hand that shook the world" - Walter O'Dim
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12-16-2007, 09:33 AM
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Join Date: Apr 2005
Location: KSLC
Posts: 4,021
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Quote:
Originally Posted by AlexPeterson
The majority of motion on my engine seems to be rotational during startup or shutdown. I have an O360 C/S prop, with non-aerobatic mounts. I would estimate that the valve covers, during this rotational motion, move up and down maybe 1/4 to 3/8" from their rest position. Certainly no more. My baffles have 1/2" clearance, and there is no sign that they've hit the cowl. The center of the engine, just behind the prop, moves up and down perhaps 1/8".
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Initially, I, along with another builder, was concerned about the clearance between the two horizontal fiberglass baffles attached to the bottom side of the top cowling & the vertical aluminum baffle pieces that are on each side of the starter gear ring. We wanted to know if we needed a larger gap, along with the rubber seal.
Numerous aircraft that we looked at, only had an 1/8" gap or slightly more/less, and little signs of wear on the fiberglass, which proves it is much more rotational; and almost nothing with side to side motion, considering it's far forward of the mounts.
L.Adamson -- RV6A
Last edited by L.Adamson : 12-16-2007 at 09:35 AM.
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12-16-2007, 09:38 AM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Rotational
Quote:
Originally Posted by AlexPeterson
The majority of motion on my engine seems to be rotational during startup or shutdown. I have an O360 C/S prop, with non-aerobatic mounts. I would estimate that the valve covers, during this rotational motion, move up and down maybe 1/4 to 3/8" from their rest position. Certainly no more. My baffles have 1/2" clearance, and there is no sign that they've hit the cowl. The center of the engine, just behind the prop, moves up and down perhaps 1/8".
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On my Tiger (O-360 engine, similar mounts...) I installed an indicator on the bottom right engine mount bolt - well, not quite, but the aftermarket PowerFlow exhaust system has a rod that passes through the cowling about 10-12 inches below the mount. This rod is fixed to the engine mount bolt and the exhaust - it moves with the engine.
The cowling hole had to be opened up to allow for the "wet dog shake", and is about 3 inches wide (rotational shake) and less than 1 inch fore and aft (up/down shake).
The rod can be seen in this picture....
Based on this, I would say the biggest movement is rotational, and the biggest physical movement would be an up/down movement at the cylinder heads.
gil A
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Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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