Mailing List flyrotary@lancaironline.net Message #39166
From: Rob <rob@mum.edu>
Subject: Re: [FlyRotary] Re: engine mounts
Date: Thu, 23 Aug 2007 21:47:44 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Bill or anyone,
I guess I need to change my question to more specifics. For example, what do you think of the single point attachment on the rear of the s-beam verses the more substantial attachment of the flat plate mount. I personally don't know if I feel comfortable with a single point of attachment in the rear. For example, there may be times when the engine gets torqued around due to sudden changes of flight direction.
Robert
----- Original Message -----
Sent: Thursday, August 23, 2007 12:56 PM
Subject: [FlyRotary] Re: engine mounts

Robert,
I understood the question. The fact is that either mount is attached to the firewall with the same type of 4130 tubes. There is little difference between the two unless you change the tube design. The response time of the pilot, is probably the most important factor, (reducing power or shutting the engine off), to the survival of the engine mount. The best situation here is to do careful inspection of the prop, be it a C/S, wood, metal, or composite. Obviously the constant speed prop is the most likely to give this kind of problem. If you have a C/S you should be checking it carefully at each annual. this is the ounce of prevention to prevent your pound of panic when the blade flies off!
Bill Jepson


-----Original Message-----
From: Rob <rob@mum.edu>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Sent: Thu, 23 Aug 2007 8:41 am
Subject: [FlyRotary] Re: engine mounts

If I may clarify my question a bit. My question was not how to prevent the engine from departing but rather which mount would survive longer because of how it is designed.
Robert
----- Original Message -----
Sent: Thursday, August 23, 2007 9:34 AM
Subject: [FlyRotary] Re: engine mounts

Jerry,
First of all, nice looking work! Second I don't think that there is anything wrong with either mount. The thread here started with a question about a mount that would stay together when the prop shed a blade. This is a problem I really think the will just leave you SOL. If you design the mount strong enough to handle that one senario it will be overweight for everything else!
Bill Jepson


-----Original Message-----
From: Jerry Hey <jerryhey@earthlink.net>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Sent: Thu, 23 Aug 2007 5:42 am
Subject: [FlyRotary] Re: engine mounts


On Aug 23, 2007, at 2:26 AM, WRJJRS@aol.com wrote:

In a message dated 8/22/2007 7:57:15 PM Pacific Standard Time, Lehanover@aol.com writes:
I would (will) go with the flat plate. All of the pan bolts are involved. Four Lord style mounts involved.
Compact and uses the engine block for added stiffness. I will include the nose gear in my mount to reduce fire wall complexity. Possible oil control benefit.
 
Lynn E. Hanover 

Lynn,
Well reasoned, but it you use a slightly changed version of the Shertz mount like Jerry Hey is now making the mount uses the bellhousing bolts and fits between the Psru plate and the engine. Using two large lord mounts and that system I believe it's a toss up. I really don't think you can really plan for this though unless you always fly high and carry a 'chute!
Bill Jepson

I have not used that design in a long time.  The S-beam now is bolted to the pan flange using eight  pan bolts at the flywheel end. It is easier to install and does not involve the PSRU at all.   I don't think there is a strength issue with either type of engine mount.  Here are two pics just shot this morning of a RV7A engine mount under construction.  At this stage the pan flange (less the pan) is bolted to the S-beam. The same bolts are later used to attach the S-beam to the engine. This engine mount is asymmetrical, it is extended on the exhaust side to provide clearance for exhaust and is shortened on the cool side to provide room for a cool side rad.  Jerry


   
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