The present disclosure relates to a parameter design method of ship ice resistance model experiment, in which the non-refrigerated model ice is used to simulate broken ice without bending failure, belonging to the field of ship engineering.
Much attention has been paid to the development of the Arctic region, and the broken ice field is the most common ice condition. However, there are few researches on the subject of ship navigation in broken ice field, which is mainly due to the lack of basic measured data or experimental data of ship resistance in the broken ice field. Therefore, it is necessary and important to carry out ship ice resistance experiment.
Model experiment is one of the research means to establish the relationship between various physical factors, including ship model experiment method. The ship model experiment method includes refrigerated model ice experiment in ice basin and non-refrigerated model ice experiment of conventional towing tank. Although the refrigerated model ice experiment can more truly simulate the ship navigating state in the broken ice, the time period of ice field preparation is long, and it is necessary to adjust repeatedly to prepare an ice field meeting the strength requirements, and the prepared ice field can only be used in one set of experiments. As a result, it takes a lot of manpower and material resources to conduct a ship ice resistance model experiment, and the resulting ice floe are not easy to manipulate. In non-refrigerated model ice experiment, the arrangement of the ice field is relatively convenient and time-saving, considering that the bending failure of broken ice is not the main component of resistance in ship navigation, the non-deformation material can be used as non-refrigerated model ice, so that the model ice can be used repeatedly to save the material cost. Therefore, the research and develop of a method for ship ice resistance model experiment based on non-refrigerated model ice is necessary.
According to the technical problems such as the scarcity of ice basin, the technique difficulty, long period and high cost of the preparation of ice field, the present disclosure provides a method of ship ice resistance model experiment based on non-refrigerated model ice. The non-refrigerated model ice experiment has obvious advantages in satisfying the experimental conditions. The present disclosure simulates the non-refrigerated model ice without bending failure by using H-type PP material, and provides a set of parameter design method of non-refrigerated ice ship model experiment. Under the assumption of no bending failure, the present disclosure calculates the size and the shape distribution of the model ice according to the actually observed statistical law; in addition provides a simple and practical method to build a small basin with a fence, which can more accurately simulate the real state of the broken ice field. Based on the above reasons, the present disclosure can be popularized and applied to the ship ice resistance model experiment of non-refrigerated ice in the ship engineering field.
A method of ship ice resistance model experiment based on non-refrigerated model ice, including the following steps:
S1. Determining the overall length L1, breadth B, and scale ratio λ of a selected ship model
A size A1 of an experimental area for placing broken ice in the ship ice resistance model experiment is determined. If the pool is full of broken ice, the total number of model ice required is too large, resulting in unnecessary waste. Therefore, according to the purpose of saving and accurate measurement, an experiment is carried out in a smaller area circled in the centre of the pool. In the direction of width, the boundary has a certain influence on the experiment, it is generally believed that when the width of the experimental area W is greater than 3 times the breadth of the ship model, the boundary influence can be neglected; in the direction of length, in order to simulate the ergodic steady sailing process of the ship in the broken ice field, it is necessary to ensure that the length L2 of the experimental area is at least 5 times that of the overall length of the ship model.
According to the overall length L1 and the breadth B of the selected ship model, determining the minimum size of the experimental area, further determining the size of the experimental area:
L2≥5L1,
W≥3B,
A1=WL2,
wherein, L2 represents a length of the experimental area, and the W represents a width of the experimental area;
The location of the experimental area in the pool: in the direction of width, the spacing between the left/right edge of the experimental area and the lateral wall of the pool should be the same; in the direction of length, when the bow enters the experimental area, it is necessary to ensure that the ship has been sailing at a constant speed for a period of time, that is, the flow around the ship model has been stable; the trailer should stop when the bow is close to but not reach the terminus of the experimental area, the terminus of the experimental area should be a certain distance from the basin wall to ensure that the boundary influence is within the acceptable range.
S2. Determining a characteristic length of model ice
S21. Determining a target coverage ratio c of the model ice
S22. According to the experimental area size A1 obtained in step S1 and the target ice coverage ratio c obtained in step S21, determining a total area A2 of the model ice:
A2=cA1.
The present disclosure has an assumption that the broken ice have no bending failure, which requires the length and thickness of the actual model ice satisfy a certain conditions, so as to ensure that the breaking and bending of the broken ice are secondary in the experimental process (which can be neglected), and the broken ice moves like a rigid body.
S23. According to the bending theory of thin plate sitting on elastic foundation, determining a critical characteristic length Lc of the broken ice without bending failure:
wherein, D represents a flexural rigidity of ice, satisfying the following equation:
E represents an elastic modulus of ice, with the unit of Pa; and t represents an actual thickness of the broken ice, with the unit of m; ν is Poisson's ratio; and k represents an elastic stiffness of the base, satisfying the following equation:
k=ρwg,
ρw is the density of water, with the unit of kg/m3; and g is the acceleration of gravity, with the unit of kg/m2.
S24. Determining the critical characteristic length l of the model ice:
wherein, L represents a characteristic length of the broken ice, satisfying the following condition:
L≤Lc.
As long as the characteristic length L of the broken ice is less than the critical characteristic length Lc of the broken ice, it is considered to satisfy the assumption of no bending failure of the broken ice.
S25. According to the critical characteristic length l of the model ice, determining a characteristic length ln of each size of the model ice in the ship ice resistance model experiment.
S3. Determining a quantitative proportion of the model ice for each size under the target coverage ratio c of the model ice:
wherein, N(ln) represents a number of the model ice with the size ln, α1, α2, β1 and β2 are coefficients, α1=1.15, α=1.87; when the characteristic length ln of the model ice is in a range of [l1,l2], the total area of the model ice satisfies the following equation:
Solving the following equation set to obtain β1 and β2:
S4. According to the quantitative proportion of the model ice of each size under the target coverage ratio c obtained in step S3, and the total area A2 of the model ice to obtain the number of the model ice for each size under the target coverage ratio c.
S5. Determining a geometrical shape and parameters of the model ice for each size under the target coverage ratio c:
A roundness R of the model ice satisfies the following equation:
wherein, dp represents a perimeter-equivalent diameter, d represents a area-equivalent diameter, and d is equal to ln, P represents a perimeter of geometrical shape of the model ice.
From the above equation, it can be seen that the larger R is, the more square the model ice shape is, when dp=ln, the shape of the model ice is a circle with R=1.
An area S of the geometrical shape of the model ice satisfies the following equation:
A caliper diameter is a distance between a pair of external parallel lines of a shape, which can be vividly understood as the distance of the shape measured by a caliper. If the pair of the parallel lines rotates a circle around the shape, there will be a maximum distance and a minimum distance, which are respectively defined as the maximum caliper diameter Dmax and the minimum caliper diameter Dmin.
A caliper diameter ratio Ra of the model ice satisfies the following equation:
Ra=Dmax/Dmin.
P is determined according to the value of R.
The geometrical shape of the model ice is determined according to P, S, and Ra.
The actual construction method of the experimental area is to build a fence with PVC pipes connected by tee pipes; in order to make the PVC pipes float on the water surface to perform a good effect for blocking the model ice, the outer wall of the PVC pipe located under the water is pasted with pearl cotton board.
The Model ice is made of H-type PP material, which is stable in mechanical properties, strong enough and insoluble in water. Therefore, it is an ideal non-refrigerated model ice material.
Non-refrigerated model ice is made of H-type PP material, the full name of the material is Homopolymer polypropylene, which is polymerized by propylene monomer; the molecular chain of the H-type PP material has a very high regularity, so that the material has good mechanical properties, good strength and high crystallinity, and its disadvantage is poor shock resistance. The main material properties of H-type PP material and sea ice are shown in the table below:
Comparing the properties in the above table, it can be seen that the density and friction coefficient of H-type PP material are very close to those of sea ice, which can more accurately reproduces the motion state of sea ice during the ship movement, so as to estimate the ship ice resistance in broken ice field. Moreover, PP-H material has stable mechanical properties, sufficient strength, insoluble in water, highly maneuverable during experimental, and can be used repeatedly, so as to save the experimental cost.
The present disclosure overcomes the problems of poor economy and poor operability of the freezing model ice experiment of ice basin, and provides a method for carrying out a ship ice resistance model experiment in the towing tank.
In order to more clearly illustrate the embodiments of the present disclosure or the technical solutions in the prior art, the drawings required in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings in the following descriptions are some embodiments of the present disclosure. For those of ordinary skilled in the art, other drawings can be obtained based on these drawings without inventive effort.
To make the objectives, technical solutions and advantages of the present disclosure clearer, a clear and complete description in the embodiments of the present disclosure may be given herein after in combination with the accompany drawings in the embodiment of the present disclosure. Obviously, the described embodiments are parts of the embodiments of the present disclosure, but not all of them. Based on the embodiments in the present disclosure, all other embodiments obtained by those of ordinary skilled in the art without inventive effort are within the scope of the present disclosure.
As shown in
S1. The overall length L1, breadth B and scale ratio λ of the selected ship model were determined.
A FPSO ship model was used in this embodiment, with a scale ratio λ=50 and the main size of the ship model is shown in the table below.
L1=4.36 m, B=0.656 m.
The size A1 of the experimental area for placing broken ice in the ship ice resistance model experiment was determined:
According to the overall length L1 and the breadth B of the selected ship model, the minimum size of the experimental area was determined, and the size of the experimental area was further determined:
L2≥5L1=21.8m,
W≥3B=1.968m,
A1=WL2,
wherein, L2 represents the length of the experimental area, and W represents the breadth of the experimental area.
According to the minimum size of the experimental area and the actual size of the towing tank (170 m×7.0 m×4.0 m), the size of the experimental area of 29 m×3.0 m×4.0 m was finally selected.
S2. The characteristic length of the model ice was determined
S21. The target coverage ratio c was determined
The ratio c was set to 90%, 80%, and 60% respectively.
S22. According to the experimental area size A1 obtained in step S1 and the target ice coverage ratio c obtained in step S21, a total area A2 of the model ice was determined:
A2=cA1,
When c was equal to 90%, 80%, and 60%, the corresponding A2 was 67.5 m2, 60 m2 and 45 m2.
S23. According to the bending theory of thin plate sitting on elastic foundation, the critical characteristic length Lc of the broken ice without bending failure was determined:
wherein, D represents a flexural rigidity of the ice, which satisfies the following equation:
E represents an elastic modulus of the ice, E=5 GPa; and t represents an actual thickness of the broken ice, t=1 m; ν represents Poisson's ratio, ν=0.3; k represents an elastic stiffness of the base, which satisfies the following equation:
k=ρwg,
ρw is the density of water, ρw=1025 kg/m3; and g is the acceleration of gravity, g=9.81 kg/m2.
S24. The critical characteristic length l was determined:
wherein, L represents the characteristic length of the broken ice, which satisfies the following equation:
L≤Lc.
So,
S25. According to the critical characteristic length l of the model ice, the characteristic length ln of each size of the model ice in the ship ice resistance model experiment was determined to be 10 cm, 15 cm, 20 cm, 25 cm, and 30 cm respectively.
S3. the quantitative proportion of the model ice for each size under the target coverage ratio c of the model ice was determined:
wherein, this equation is the size distribution law function of the broken ice.
Wherein, N(ln) represents a number of the model ice with the size ln, α1, α2, β1 and ρ2 are coefficients, α1=1.15, α2=1.87, when the characteristic length l of the model ice is in the range of [l1,l2], the total area of the model ice satisfies the following equation:
The following equation set was solved to find β1 and β2.
The ratio c was equal to 90%, 80% and 60%, and the corresponding β3 and β2 values were respectively solved, as shown in the table below:
β1 and β2 were plugged into the size distribution law function of the broken ice to obtain a cumulative distribution function of the corresponding target coverage. According to the obtained cumulative distribution function and the scale ratio λ, the quantitative proportion of the model ice with different sizes under the target coverage c of the model ice was calculated (In order to get a quantity of 30 cm by interpolation, calculating the cumulative quantity of 35 cm).
S4. According to the quantitative proportion of the model ice of each size under the target coverage ratio c obtained in step S3, and the total area A2 of the model ice, the number of the model ice of each size under the target coverage ratio c was obtained, as shown in the table below:
The cumulative quantity distribution with target coverage ratio of 0.6 is shown in
S5. The geometrical shape and parameters of the model ice for each size under target coverage ratio c were determined:
The roundness R of the model ice satisfies the following formula:
wherein, dp represents a perimeter-equivalent diameter, d represents a area-equivalent diameter, and d is equal to ln, P represents a perimeter of geometrical shape of the model ice.
An area S of the geometrical shape of the model ice satisfies the following equation:
A caliper diameter ratio Ra of the model ice satisfies the following equation:
Ra=Dmax/Dmin
The statistic data showed that the R of the broken ice behaves as a linear function, which was about 1.145±0.002, meanwhile, the smaller the characteristic length L of the ice floe was, the smaller the fluctuation was. The caliper diameter ratio Ra was about 1.78±0.4, and the smaller the maximum caliper diameter Dmax, the smaller the fluctuation of Ra was. Thus, took R=1.145, Ra=1.78.
P was determined according to the value of R;
The geometrical shape of the model ice was determined according to P, S, and Ra.
The geometric shape of the model ice was selected as polygon to satisfy the relationship of perimeter, area and side length of the shape in the table above, so as to determine the detailed geometric shape parameters of the regular polygon. Each polygon calculation method is different, and there are non-unique geometric parameters according to the above conditions, so there is no detailed calculation here. Only a set of diagrams of long trapezoid, flat trapezoid, rectangle, pentagon, hexagon, and ellipses (30 cm) with assumption of symmetry are listed here, as shown in
After the experimental area was selected, a fence with a size of 29 m×3.0 m should be installed in the towing tank to fence the broken ice field for ship navigation. The fence was made of standard PVC pipe with a length of 4 m and a external diameter of 75 mm. The PVC pipes were connected with tee pipes. In order to strengthen the connection between the pipe fittings and the tee pipes, two holes were drilled in the overlap part of PVC pipe and the tee pipe, and the iron wire was tightened through the two holes. The whole installation effect of the fence is shown in
Finally, according to the above calculation results, the picture of the experimental area with a target coverage ratio of 0.6 is shown in
At last, it should be stated that the above embodiments are only used to illustrate the technical solutions of the present disclosure without limitation; and despite reference to the aforementioned embodiments to make a detailed description of the present disclosure, those of ordinary skilled in the art should understand: the described technical solutions in above various embodiments may be modified or the part of or all technical features may be equivalently substituted; while these modifications or substitutions do not make the essence of their corresponding technical solutions deviate from the scope of the technical solutions of the embodiments of the present disclosure.
Number | Date | Country | Kind |
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201910009613.4 | Jan 2019 | CN | national |
Filing Document | Filing Date | Country | Kind |
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PCT/CN2019/099884 | 8/9/2019 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2020/140435 | 7/9/2020 | WO | A |
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106394806 | Feb 2017 | CN |
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Number | Date | Country | |
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20210108986 A1 | Apr 2021 | US |