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  • Randomly OT, Helicopter Weight and Balance question.
  • chopperT
    Free Member

    OK, I sat CAA(NZ) exam for Rotorcraft today, 94% (yay!), but one question bothers me. Lateral Centre of Gravity calculation had me guessing.
    So, arms left of centreline are negative, arms right are positive. I have loads and arms for left and right fwd scales, rear scale is on the centreline.
    The way I figure, lateral CoG arm is
    left weight x left arm(-)=left moment
    right weight x right arm(+)=right moment

    LW+RW=WT, LM+RM+MT, CoG(lat)=WT/MT.

    But it isn't. For some reason I need to use the aft scale reading aswell,even though that lies on the centreline (ie; 0 arm=0 moment),to give a total weight, and divide that by the total L/R moment to get the lateral CoG position. Why?

    MrNutt
    Free Member

    ladened or unladened? is it an african helicopter?

    TheFunkyMonkey
    Free Member

    Depends on your favourite colour

    chopperT
    Free Member

    Random question = random answer?

    thisisnotaspoon
    Free Member

    The fore/aft ballance only applies if you are attempting takeoff/landing from a treadmill.

    elliptic
    Free Member

    So basically you've been given these weights and distances:

    |————–|————–|
    Wl…………Wa…………Wr

    You need the position of the CoG ie. the position that the total weight Wl + Wa + Wr acts through.

    So yes, you need all three weights to compute that.

    (Note that if Wa is much larger than the other two, the CoG must necessarily be close to that position regardless of any imbalance between Wl and Wr. If not, the CoG can be further out.)

    chopperT
    Free Member

    So Wa influences the arm of the lateral CoG, because the L/R weights are taken ahead of the longitudinal CoG?

    elliptic
    Free Member

    Nothing to do with longitudinal balance, it's purely a 2-d problem.

    CoG is where the total weight of the helicopter acts through, and Wa is part of that total weight.

    What you're looking for is the point where the combined (lateral) moment of *all three* components is zero.

    Of course Wa has a moment of zero about the centreline. But if the CoG is not on the centreline…

    chopperT
    Free Member

    Bing! The light goes on "Of course Wa has a moment of zero about the centreline. But if the CoG is not on the centreline… "

    Thanks. I'll sleep better tonight!

    BTW, I did get the question right, but I couldn't figure out why.

    elliptic
    Free Member

    No probs!

    So do you get to fly them now..?

    Pook
    Full Member

    Bagsy first on the uplift day.

    chopperT
    Free Member

    Ain't allowed to fly them – just get to fix them!

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