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rodgerc

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Posts posted by rodgerc

  1. 39 minutes ago, Blueadventures said:

    Be interested to know how many aircraft have rego allocated to them and how many are in current rego.

    The precise wording on the RA website is:

     

    “There are currently 3232 active aircraft in the RAAus fleet.”

     

    Since registrants are invoiced annually, I’d interpret “active” to mean “currently registered”, but I’ve been wrong before today. 

    • Like 1
  2. If it were me, I’d initially keep life simple by sticking with all 22001 dimensions except the OD. 
     

    Some (very) basic stuff assuming a 70kg engine and prop combo….Call it 700 Newtons for simplicity. 
     

    Original mount net area 790mm^2 x 4off = 3,160mm^2. 
     

    Compressive stress = 790N/3,160mm^2 = 250kPa

     

     

    With a 1-1/2” OD the total bearing area increases to 4,216mm^2 or 33% more. So compressive stress decreases to 790N/4,216mm^2 = 187kPa.
     

    By implication, the compressive strain on the mounts will also be decreased by about 1/3 and along the way, you’ll have increased the surface area to dissipate all that vibration (kinetic energy) heat into the aluminium mounting rails.
     

    Naturally, the back-up washers will also need to be increased in diameter.

     

    It’s pretty easy to cast urethane and there’s a bunch of videos on YouTube showing people doing it at home….Search “casting polyurethane bushings” and pour yourself a drink. 
     

    If you’re still unsure of your ability (it’s easy) then pop over to 33 Holloway Dr Bayswater and talk to Melbourne Polyurethane. 

    • Like 2
  3. IMG_9501.thumb.jpeg.2268c11ad78c57d2dc4bf2ed21ecafd6.jpegWould you be able to crib an extra 1/4” on the diameter of the mount? (I.e. Dimension A)

     

    If yes, then personally I’d try that by having a custom set cast in 80A durometer PUR before switching to a stiffer (higher modulus) compound….It would improve the vibration dampening characteristics of the engine mount.

     

    When comparing the dimensions of the 22001 rubber components with the Lord mounts used on a (albeit considerably heavier) Conti 0-200, it does seem to be rather a big ask. 

  4. I’d be inclined to look at a larger mount rather than a stiffer compound. Simply on the basis of force/area = pressure. (Stress)

     

    For information only, the (during construction) pics below are the RANS bed-mount installation in my Raven. 

    After ~90h flying over 18 months they are standing up very well with no noticeable compression set/sag. 

     

    I suspect they are natural rubber of around 80A durometer. IMG_9497.thumb.jpeg.e7eb0e4b16eafef9591d93e716fb22f8.jpegIMG_9498.thumb.jpeg.dfe798dd31130d6e032559fca5047ee5.jpegIMG_9499.thumb.jpeg.64854c68ff18c150b8011045385a38e8.jpegIMG_9496.thumb.jpeg.a255e6ec416ec781239e1c3771fc9951.jpeg

    • Like 3
  5. For what it’s worth, my AeroVee powered Waiex’s engine mounts were replaced at every annual, because after a year and 25-35h flying they were pretty well shot. 
     

    I suspect they were EPDM of around Shore A, 80 hardness. 
     

    Given thermoset urethane is readily available and easy to cast in a silicone mould, have you considered casting your own larger mounts from polyurethane to spread the load?

  6. Jump forward 7 months and 40+hours of flight time and the 350-400 RPM mag drop issue reappeared a few weeks ago. 
     

    Perhaps it was not the trigger coil gaps but rather the possibility that back in April, the weather had cooled sufficiently for a marginal ignition module to stop misbehaving. 
     

    For the past couple of hot and sweaty weeks in SE Qld my 350-400 RPM mag drop has occurred, but only after ~10 minutes of taxiing. 
     

    Long story short, a set of Mark Kyle’s aftermarket ignition modules has “fixed” the issue.
     

    It’s only a hypothesis, but perhaps when the “faulty” module reached a certain operating temperature, it would revert to the Rotax retarded “soft start” timing and thus, when selecting that module only for a mag check, the engine dropped 350-400 RPM in protest to retarded timing. 
     

    Did somebody just mutter, “correlation does not imply causation”?

    • Like 1
    • Informative 1
    • Who you are insured with? InsuranceHouse. 
    • Are you as happy as can be ? Yes, with the caveat that having insured a number of aircraft for around 12 years I’ve never made a claim. 
    • Would you recommend them? Yes, subject to the above caveat. 
    • Any that you would not recommend? QBE via SAAA. The turf wars between SAAA and RA-Aus meant that despite being a SAAA member for >12 years, being a >500h GA pilot with numerous ratings and endorsements and building via the SAAA’s process of TC inspections using their risk radar, they would not insure my latest build because I chose to register it with RA-Aus. (I’m no longer a SAAA member.)
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