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09-20-2016, 05:34 AM
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Join Date: Feb 2005
Location: Shawnee, Kansas
Posts: 804
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Dear Mr. Lycoming, why is the cam so high up in the engine?!
What is the trade-off? Why did Lycoming put the cam on top and every other flat engine manufacturer (Continental, Franklin, Jabiru, VW & GM/Corvair) put it on the bottom where it stays nice and happy bathed in oil when we neglect them?
This seems like a pretty big flaw. I've always wondered this.
__________________
Bruce Meacham
Building RV-4A 18ZM
Built/Own RV-4 254MM
First RV RV-3 3456B
VAF annual donation on autopay
Last edited by BruceMe : 09-20-2016 at 05:38 AM.
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09-20-2016, 05:58 AM
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Join Date: Jan 2005
Location: Louisville, Ga
Posts: 7,840
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Nope
They're not 'bathed' in oil. The oil level is way below the cams on Continentals...they're all splash oiled, except for the bearings which are pressure lubed.
Best,
__________________
Pierre Smith
RV-10, 510 TT
RV6A (Sojourner) 180 HP, Catto 3 Bl (502Hrs), gone...and already missed
Air Tractor AT 502B PT 6-15 Sold
Air Tractor 402 PT-6-20 Sold
EAA Flight Advisor/CFI/Tech Counselor
Louisville, Ga
It's never skill or craftsmanship that completes airplanes, it's the will to do so,
Patrick Kenny, EAA 275132
Dues gladly paid!
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09-20-2016, 06:02 AM
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Join Date: Aug 2015
Location: Cape Coral, FL
Posts: 349
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Maybe we're putting the engines in upside down???  
__________________
Thanks,
Anthony
RV6-A "Aluminum Mistress"
Too many hobbies- not enough time.
2016, 2017, 2018, 2019 donor and happy to do it.
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09-20-2016, 06:57 AM
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Join Date: Jan 2005
Location: Clarion, Pennsylvania
Posts: 549
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Don't know the answer, but the O-145, Lycoming's first boxer, had the cam down low:
https://en.m.wikipedia.org/wiki/Lyco...g_O-145_B2.jpg
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-Andy Turner
RV-10 N784JC
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09-20-2016, 07:07 AM
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Forum Peruser
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Join Date: Jan 2005
Location: Austinville, Alabama
Posts: 2,455
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Maybe Mahlon will give his valued opinion.
P.S. Mahlon Russell, where are you?
__________________
Don Hull
RV-7 Wings
KDCU Pryor Field
Pilots'n Paws Pilot
N79599/ADS-B In and Out...and I like it!
?Certainly, travel is more than the seeing of sights;
it is a change that goes on, deep and permanent, in the ideas of living." Miriam Beard
Last edited by rv7boy : 09-20-2016 at 11:50 AM.
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09-20-2016, 07:08 AM
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Join Date: Jun 2005
Posts: 846
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cam
Just overhauld a Perkins diesel that was 32 years old and all its life has been in a boat on the ocean in a damp hole in the bottom and not a spec of rust on the cam.Maybe the Lycoming cam is made from wrong type of metal also the valve train in the Perkins is set up with more pressure than Lyco turns same RPM @ 2700 and no cam spauling.Go figure.
Bob
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09-20-2016, 08:20 AM
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Join Date: Sep 2007
Location: Central IL
Posts: 5,515
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Musings
An engine design is a tangled mass of tradeoffs and contractions. Very few are a clean sheet design, and even they have compromises for fitting manufacturing machinery on hand and other influences for commonalities of volume production for lowest cost.
A loop flow combustion chamber (both intake and exhaust on the same side) means pushrods are better located on the opposite side. Aero engine designs always want to have holes in the bottom to prevent a cylinder from completely filling with liquids, oil or fuel.
So - there is no magic reason for the cam to be located high as far as I have ever been able to determine. Lubrication is not an issue either way. Lycoming has done other odd things design wise, I honestly think that if it were not for a better parent company, they would not have ended up the prime supplier of engines today.
If our engines had positive crankcase ventilation the cams would probably not have corrosion problems. PCV is very problematic for the operational profile and its failure modes, so there are some other strong reasons it is not incorporated. It is not water that is the real issue, it is sulfur in the fuel. Sulfur has been removed from nearly all world fuels worldwide as it interferes with catalytic reactions and would make sulfates . . . . . . not good. Regardless, we have methods of preventing corrosion.
Litigation and certification is tangled in there too as they drive some very odd decisions and are in many ways an impediment to improvements. " Mr Lycoming, I see you improved your connecting rod. That means the previous design was inferior and you were hiding it. Ladies and gents of the jury . . . "
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Bill
RV-7
Lord Kelvin:
“I often say that when you can measure what you are speaking about,
and express it in numbers, you know something about it; but when you
cannot measure it, when you cannot express it in numbers, your knowledge
is of a meager and unsatisfactory kind.”
Last edited by BillL : 09-20-2016 at 08:24 AM.
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09-20-2016, 10:59 AM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Quote:
Originally Posted by Planecrazy232
Maybe we're putting the engines in upside down???  
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If you storing it as a core for a long time, then upside down is best with the case full of oil. 
__________________
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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09-20-2016, 11:49 AM
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Forum Peruser
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Join Date: Jan 2005
Location: Austinville, Alabama
Posts: 2,455
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In addition to the location of the camshaft, which is the original topic, I am also intrigued by the decision to support the camshaft in a journal machined in the casting(s). When I saw my O-320 apart during an overhaul a few years ago, I was surprised at this. Is this common practice for all aircraft engines?
__________________
Don Hull
RV-7 Wings
KDCU Pryor Field
Pilots'n Paws Pilot
N79599/ADS-B In and Out...and I like it!
?Certainly, travel is more than the seeing of sights;
it is a change that goes on, deep and permanent, in the ideas of living." Miriam Beard
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09-20-2016, 11:57 AM
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Join Date: Mar 2005
Location: Dallas area
Posts: 10,762
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Quote:
Originally Posted by rv7boy
In addition to the location of the camshaft, which is the original topic, I am also intrigued by the decision to support the camshaft in a journal machined in the casting(s). When I saw my O-320 apart during an overhaul a few years ago, I was surprised at this. Is this common practice for all aircraft engines?
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If you are referring to the fact that the cam does not ride in bearings, since all loads on the cam are from the lifters and their force is from opposing directions, there are practically no loads on the bearing surfaces. Therefore bearings are not needed.
__________________
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>
Last edited by Mel : 09-20-2016 at 01:10 PM.
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