This paper presents a fatigue design method for plug and ring type gas welded joints, which incorporates welding residual
stress effects. A non-linear finite element analysis (FEA) was first performed to simulate the gas welding process. The numerically
predicted residual stresses of the gas welds were then compared to experimental results measured using a hole drilling method.
In order to evaluate the fatigue strength of the plug and ring type gas welded joints, a stress amplitude (σa)R taling the welding residual stress of the gas weld into account was introduced and is based on a modified Goodman equation
incorporating the effect of the residual stress. Using the stress amplitude (σa)R, the ΔP-Nf relations obtained from fatigue tests for plug and ring type gas welded joints having various dimensions and shapes were
systematically rearranged into (σa)R-Nf relations. It was found that the proposed stress amplitude (σa)R could provide a systematic and reasonable fatigue design criterion for the plug and ring type gas welded joints. 相似文献
Pitting corrosion is typical corrosion observed on coated hold frames of bulk carriers which exclusively carry coal and iron ore. In order to secure the safety of these types of bulk carriers, it is important to understand the effect of pitting corrosion on local strength of hold frames.
In order to investigate this effect, a series of 4- and 3-point bend tests on structural models which consist of web, shell and face plates has been carried out. Artificial pitting was created on the web plate to simulate pitting. In the 4-point bend tests, two equal concentrated loads have been applied vertically at the one-third points of simply supported models so that compression load due to bending would act on the face plate. In this testing condition, lateral-distortional buckling occurred before reaching the ultimate strength and local buckling of the face plate was observed after reaching the ultimate strength. The effect of web plate pitting on the lateral-distortional buckling strength was found to be small but the ultimate strength decreases with increase in the degree of pitting intensity. In the 3-point bend tests, concentrated load has been applied vertically at the center of simply supported models so that compression load due to bending would act on the face plate. In this testing condition, local face buckling occurred just after reaching the ultimate strength. The ultimate strength is found to be decreasing with increase in the degree of pitting intensity.
A series of non-linear FE analyses has been performed to simulate the deformation behavior observed in the tests. It has been revealed that even in the case of randomly distributed pitting corrosion the ultimate strength of the structural models was almost the same as that of the structural models with uniform corrosion corresponding to the average thickness loss. 相似文献
The aim of this study is to derive a simple analytical formula for predicting the ultimate collapse strength of a single- and double-hull ship under a vertical bending moment, and also to characterize the accuracy and applicability for earlier approximate formulations. It is known that a ship hull will reach the overall collapse state if both collapse of the compression flange and yielding of the tension flange occur. Side shells in the vicinity of the compression and the tension flanges will often fail also, but the material around the final neutral axis will remain in the elastic state. Based on this observation, a credible distribution of longitudinal stresses around the hull section at the overall collapse state is assumed, and an explicit analytical equation for calculating the hull ultimate strength is obtained. A comparison between the derived formula and existing expressions is made for largescale box girder models, a one-third-scale frigate hull model, and full-scale ship hulls.List of symbols
AB
total sectional area of outer bottom
-
AB
total sectional area of inner bottom
-
AD
total sectional area of deck
-
AS
half-sectional area of all sides (including longitudinal bulkheads and inner sides)
-
as
sectional area of a longitudinal stiffener with effective plating
-
b
breadth of plate between longitudinal stiffeners
-
D
hull depth
-
DB
height of double bottom
-
E
Young's modulus
-
g
neutral axis position above the base line in the sagging condition or below the deck in the hogging condition
-
H
depth of hull section in linear elastic state
-
Is
moment of inertia of a longitudinal stiffener with effective plating
-
l
length of a longitudinal stiffener between transverse beams
-
ME
elastic bending moment
-
Mp
fully plastic bending moment of hull section
-
Mu
ultimate bending moment capacity of hull section
-
Muh,Mus
ultimate bending moment in hogging or sagging conditions
-
r
radius of gyration of a longitudinal stiffener with effective plating [=(Is/as)1/2]
-
t
plate thickness
-
Z
elastic section modulus at the compression flange
-
ZB,ZD
elastic section modulus at bottom or deck
-
slenderness ratio of plate between stiffeners [= (b/t)(y/E)1/2]
-
slenderness ratio of a longitudinal stiffener with effective plating [=(l/r)(y/E)1/2]
-
y
yield strength of the material
-
yB,
yB,
yD
yield strength of outer bottom, inner bottom
-
yS
deck, or side
-
u
ultimate buckling strength of the compression flange
-
uB,
uB,
uD
ultimate buckling strength of outer bottom
-
uS
inner bottom, deck, or side 相似文献