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HybridZ

RTz

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Posts posted by RTz

  1. Seems to me that as the suspension compresses the longitudinal link will cause the suspension to swing in an arc.

     

    Could be used as anti-squat?

     

    That would very quickly cause bind in the lateral links, if everything were solid bearings.

     

    Got it, and I agree. I had assumed your were referring to spherical bearing's. I don't believe there would be any binding with spherical's.

     

    EDIT--Actually, maybe that would just cause toe change. Still not what I'd be looking for.

     

    Subtle use of toe changes are often desirable. I probably would'nt go far out of my way to have dynamic toe, but I'm not opposed to it if 'comes with the package' and the curve is reasonable.

     

    The RCVD book discusses this suspension on p642 as well. Binding is not mentioned as an issue with this setup, although toe change is and it's suggested as a good suspension design for compliance and ride comfort.

     

    It does say something to that effect, but its related to bushing orientation/durometer, which wouldn't be applicable here.

     

    I'm 'arguing' simply becuase I see it as a reasonable alternative and based on similar packaging. Unfortunately, I'm not conviced of the strut side load's being a factor that can be reasoanbly reduced with control arm design, but its outside my ability to either argue or prove.

     

    Am I bugging you yet? :-)

  2. Engine mass loads, when mounted to the crossmember, pass directly to the suspension. The same would be essentially true if the engine mounts were on the frame rail directly above where the crossmember mounts to the frame rail. Moving the engine mounting back on the frame rail makes the frame rail more of a beam connecting the front suspension with the engine mounts.

     

     

    Perfect! That's exactly it. I need to learn how to write.

  3. where does the engine move place the transmission shifter?

     

    Here's a picture of my LT1 powered Z, also with a T56, mounted in the standard JTR position...

     

    Dash.jpg

     

     

    Its a modified Datsun shift lever, oriented so the offset positions the knob rearward. While its not etched in stone, its looking like the trans will be another 3" farther back. Flipping the shift lever around, I should end up with a knob an inch or two father back than the above picture, which I would welcome.

  4. I'm not being argumentative, I'm just confused.

     

    That makes two of us, my friend. I read your arguments as constructive and I'm hoping that you're doing the same with mine. I think there's value in understanding loads and load paths so this discussion interests me. If I prove to be wrong, so be it. I will walk away with a better understanding.

     

     

    1. That a more direct connection between the contact patch and the engine has an effect on handling?

     

     

    Nope, sorry to give that impression.

     

     

    2. That a more direction connection between the contact patch and the engine has a greater or lesser effect on framerail loading?

     

     

    Getting closer.

     

    I thought presenting the case from a lateral perspective would have been easier, but thats not proving true. Allow me to start over from a vertical perspective, from the point of severe bottoming out.

     

    To exaggerate, put 20,000 lbs of weight on top of the engine (stock mounted). The suspension will be on its stops and the four vertical bolts through the crossmember will try to tear out (vertically). The lower rail is seeing a lot of focused stress (in tension), but its being held to great degree by the upper rail due to the strut tower. A fairly robust load path.

     

    On the other hand, assume the engine is mounted to the lower rail, roughly in the middle. Again, putting the same 20K lbs of weight on the engine. The suspension is still bottomed, but now the lower rail is bowed downward because the only thing attaching it to the upper rail is the inner fender and its not efficiently built for that load. Also, there is no longer ANY stress on the 4 crossmember bolts. In fact, you could remove them and move the crossmember up and down by hand. The load path changed.

     

    In both cases the amount of stress is the same, but its re oriented. The loads on the rail changed from tension to compressive and the loads on the crossmember are removed entirely.

     

    In retrospect, laterally speaking, its more complex, but still has the same 'issue'... a re-arranged load path.

     

    If any of that makes sense, and you agree, I'll take another stab at the lateral scenario.

  5. Hi John,

     

    I'm not trying to say the loads disappear... just trying to say they get re-arranged.

     

    With a crossmember mounted engine, in a lateral load, the load goes from the contact patch, through the spindle, strut housing, BJ, LCA, and into the crossmember, which is directly connected to the engine. The lower frame rail sees no direct lateral loading. Yes, a 'small' amount is feed into the TC bucket via the TC rod, and a smaller amount yet throughout he trans mount. Its dispersed. Obviously, there is a direct load going through the upper spring perch and into the upper rail which shares the load with lower frame rail via the strut tower itself and the inner apron. Again, I see the loads being dispersed, and having no direct impact to the lower rail, except that of being pulled down.

     

     

    FrontLoadPaths.jpg

     

    Edit: My only point is that frame mounting will produce highly focused loads on the rail (instead of the crossmeber), whereas crossmember mounting disperses the loads over a broad area of the unibody

  6. Why? The front frame rails are strongest at the TC rod buckets, which handle greater loads then the torque an engine can produce.

     

    When the engine is mounted to the frame rails, the frame now sees a localized load point in every direction (lateral, vertical, longitudinal). When crossmember mounted, there are no lateral loads (from the engine) and the remaining loads are dispersed broadly through the upper and lower frame rails and inner fender liners.

     

    Additionally, moving the mount 'pedestal's' back 5.5" isn't close enough to the TC bucket area to have any relevance, or so it seems to me.

     

    Of lesser importance, an unnamed member has done some compliance testing of the bucket area, and has found, with 'normal' lateral chassis loading, there is quite a bit of flex in the TC bucket. While it may be the strongest part of the front frame rails, it still flex's more than I'd like to see.

     

    I'm aware that a number of our members have done 'frame mounts'. Its simply my preference to avoid it if its reasonable.

  7. Ok your NEVER going to bend a 3/8" thick boxed or even correctly multi-gusseted & tig welded, steel motor mount simply because anything on the cars frame you bolt it or weld it TOO will bend first if enought stress is applied, you might also consider the potential stress and weight of the drive train are FAR below the tensile and sheer and torsional strength a correctly designed 3/8" steel mount less than 8" long will have

     

    I hear ya Grumpy... makes sense. Here is part of my concern... If the brackets are completely ridgid, there should not be any rotational forces on the crossmember. But, if the offset brackets were allowed to flex, that would putting a twisting load on the crossmeber, yes?

  8. Summary...

    If I wanted to offset the standard JTR mounts an additional 2" rearward, what is the necessary material thickness to achieve equivalent rigidity?

     

    Why...

    Today's EMS's commonly allow us to delete the distributor, which is the principal physical limiting factor with respect to engine location. Deletion allows a more reward location of the drive-train.

     

    Nitty Gritty...

    The JTR brackets offset the drivetrain rearward 3.5". If I wanted to increase that to 5.5", 57% increase center-center, I would need to increase the bracket thickness from .3125" to ???

     

    Knowing that any material, doubled in thickness, results in 8x rigidity (increases with the cube, correct?), increasing the thickness to .375" should more than cover it with a 73% gain in stiffness... 20% greater thickness = 1.2^3 = 1.728.

     

    Am I looking at this right? Considering lateral and vertical loads, does it matter that they are mounted on a 45 degree, or is that 'no factor' in this scenario?

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