Thank you agent_smith
However, I am of the view that it may distort under heavy load.
I guess you are refering to BTL profile, but you have to dress it smartly, by gradually cinching all three endings, in order to cease nub distortion and hasten the balance state. I believe the TL profile("tugboat loadings", SPart 1 = > eye, SPart 2 = > eye), barely leave a `tortured` nub.
I think of the harness 1050, as a super basic inline structure, and am trying to build on its core to produce more stable results. However, whatever transformation i subjected to the previously presented inline configuration, i was not able to pick up any correlation with some known knot (some inline knots are harness derivatives), but with a Xarax Samisen bowline.
Link : https://igkt.net/sm/index.php?topic=4883.0I'm afraid, it is not possible to completely diminish the nub distortion of an inline TIB knot structure, because of both links asymmetry.
Xarax had given prominence to this concept by stating that
" there can be no symmetrical TIB midline loop".Link : https://igkt.net/sm/index.php?topic=5440.msg36783#msg36783What we can do, is try to approximate this supposed " pseudo symmetry", in order to keep the distortion to a bare minimum level.
Of great importance, would also be the validity of EEL (either end loadable), CL or RL (cross loadable or ring loadable) qualities, with the feasibility of a solid EL (eye loadable) , BTL (bi-axially through loadable) profiles that correspond to a midline knot accordingly.
Having said that, i only know so far just two knots which somehow come close to such an optimal response when loaded, the 1053 butterfly and the cask knot (EHL).
I also wonder if it is possible to create the ultimate BTL (Bi-axially Through Loadable) mid-line eye knot that is also TIB?
Imagine a structure that is based on a Zeppelin-like core?
Challenge accepted?
This is a tough challenge, but i wouldn't bet against the existence of such a knot structure! Maybe, our minds are not prepared for it yet!!
