Four end fitting designs of long rod fiberglass
core suspension insulators are studied and the
failure mechanisms are analyzed after UTS and creep
tests. The fracture occurs in the fiberglass rod due
to the stresses induced by the metal part of the endfitting
that hold the insulating components.
The stress distribution in the fiberglass rod
depends strongly on the end fitting design. Generally
stresses are highest near the end fitting edge. Some
designs optimize the axial (a ), radial (a-) and transversal
shear stresses by a jUdicious choi~e of geometrical
parameters.
A 45° fracture starts at the end
interface where stresses are highest,
towards the inside of the rod. Final rod
be explained in terms of each composite's
tics as determined in this work.
%0 Journal Article
%1 miermaza1983failure
%A Mier-Maza, R
%A Lanteigne, J
%A Tourreil, C
%D 1983
%K FAILURE FIBERGLASS INSULATORS
%T FAILURE ANALYSIS OF SYNTHETIC INSULATORS WITH
FIBERGLASS ROD SUBMITTED TO MECHANICAL LOADS
%X Four end fitting designs of long rod fiberglass
core suspension insulators are studied and the
failure mechanisms are analyzed after UTS and creep
tests. The fracture occurs in the fiberglass rod due
to the stresses induced by the metal part of the endfitting
that hold the insulating components.
The stress distribution in the fiberglass rod
depends strongly on the end fitting design. Generally
stresses are highest near the end fitting edge. Some
designs optimize the axial (a ), radial (a-) and transversal
shear stresses by a jUdicious choi~e of geometrical
parameters.
A 45° fracture starts at the end
interface where stresses are highest,
towards the inside of the rod. Final rod
be explained in terms of each composite's
tics as determined in this work.
@article{miermaza1983failure,
abstract = {Four end fitting designs of long rod fiberglass
core suspension insulators are studied and the
failure mechanisms are analyzed after UTS and creep
tests. The fracture occurs in the fiberglass rod due
to the stresses induced by the metal part of the endfitting
that hold the insulating components.
The stress distribution in the fiberglass rod
depends strongly on the end fitting design. Generally
stresses are highest near the end fitting edge. Some
designs optimize the axial (a ), radial (a-) and transversal
shear stresses by a jUdicious choi~e of geometrical
parameters.
A 45° fracture starts at the end
interface where stresses are highest,
towards the inside of the rod. Final rod
be explained in terms of each composite's
tics as determined in this work.},
added-at = {2020-04-04T17:06:58.000+0200},
author = {Mier-Maza, R and Lanteigne, J and Tourreil, C},
biburl = {https://www.bibsonomy.org/bibtex/20bb5aaa703e0704c7a7ab73ec89373db/chkokalis},
interhash = {8b4b124e912c856f83b62bf19f696032},
intrahash = {0bb5aaa703e0704c7a7ab73ec89373db},
keywords = {FAILURE FIBERGLASS INSULATORS},
timestamp = {2020-04-05T16:20:10.000+0200},
title = {FAILURE ANALYSIS OF SYNTHETIC INSULATORS WITH
FIBERGLASS ROD SUBMITTED TO MECHANICAL LOADS},
year = 1983
}