The present disclosure relates to a pressure-resistant shell, and especially to a pyram-shaped deep-sea pressure-resistant shell and a design method thereof.
The pressure-resistant shell is a thin shell structure that is subjected to a hydrostatic pressure, which requires good mechanical properties, space utilization in the shell, fluid dynamics characteristics and occupant comfort, and the performances of the submersible such as safety, carrying capacity, maneuverability and diving time need to be improved.
Spherical, cylindrical or annular shell structures are mainly adopted by the pressure-resistant shell of submersibles in services. Among them, the spherical structure shell has strong pressure resistance, but its internal space utilization is low. Although the cylindrical structure shell has the advantage of high space utilization rate, its mechanical properties are poor, and the internal stiffener needs to be increased, which sacrifices a certain space inside the shell. The annular shell structure has strong pressure resistance, but its space is not easy to expand, resulting in low space utilization. It can be seen that these properties cannot be effectively coordinated by the existing pressure-resistant shells, which are technical problems in the development of submersibles.
Many shell structures with good pressure resistance characteristics have been created in nature, among them, the pyram is a long-term underwater living organism, and the shell has the advantages such as good weight strength ratio, streamline and aesthetic characteristics, and the structure has enough strength and stability without strengthening the support, which is an excellent pressure resistant structure. However, how to implement bionic application is an extremely difficult problem.
The objectives of the present disclosure are that: in view of the above problems, the objectives of the present disclosure are to provide a pyram-shaped deep-sea pressure-resistant shell with good mechanical characteristics, space utilization rate inside the shell, occupant comfort, safety and carrying capacity, as well as a design method thereof.
Technical solutions are as follows. The pyram-shaped deep-sea pressure-resistant shell comprises a conical shell, an annular combined shell, a cylindrical shell, a flange bolt and a perforated thick plate; a bottom end of the conical shell is connected with a top end of the annular combined shell, the conical shell is in communication with an interior part of the annular combined shell; the perforated thick plate blocks the bottom end of the annular combined shell, the perforated thick plate and the annular combined shell are connected by means of multiple flange bolts; the cylindrical shell is disposed inside the annular combined shell, a lower end of the cylindrical shell is inserted in a gap between the annular combined shell and the perforated thick plate, and an upper end and the lower end of the cylindrical shell are respectively connected to an inner peripheral surface of the annular combined shell.
Further, the annular combined shell includes a first annular shell, a second annular shell and a third annular shell connected from an upper end to a lower end in sequence, and the first annular shell, the second annular shell and the third annular shell are internally connected, an upper end of the first annular shell is connected to the conical shell, a bottom end of the third annular shell is connected to the perforated thick plate, the cylindrical shell is arranged inside the third annular shell.
Further, an outside peripheral surface of the cylindrical shell is provided with at least two channels, such that the first annular shell, the second annular shell and the third annular shell are interconnected with each other.
Further, outer shell surfaces of the first annular shell, the second annular shell and the third annular shell are all circular arc surfaces, with outer diameters of the first annular shell, the second annular shell and the third annular shell increasing in sequence, and centers of circular cross-sections of the circular arc surfaces of the first annular shell, the second annular shell and the third annular shell are all located on an extension line of an outer profile of the conical shell.
Optimally, the conical shell, the first annular shell, the second annular shell and the third annular shell are sequentially welded and fixed into a whole.
Further, the flange bolt includes a bolt, a first flange, a sealing ring, a second flange, a washer, and a nut. The first flange is fixed to a bottom surface of the annular combined shell, the second flange is fixed to a bottom surface of the perforated thick plate, the bolt is threaded and arranged in the first flange and the second flange in sequence, such that the first flange and the second flange are in securely threaded-connection with each other through the nut, the sealing ring is arranged between a connection surface of the first flange and the second flange, and the washer is arranged between a contact surface of the nut and the second flange.
Provided is a method of designing the pyram-shaped deep-sea pressure-resistant shell. The method comprises the following steps.
Given that a height of an isosceles triangle inside the pyram-shaped deep-sea pressure-resistant shell is H, then:
H=(L+2r2+2r3+2r4)cos α;
where L represents a length of a generatrix of the conical shell, r2 represents a circumference radius of the first annular shell, r3 represents a circumference radius of the second annular shell, r4 represents a circumference radius of the second annular shell, and a represents a half-cone angle; and
rotation radii of the conical shell, the first annular shell, the second annular shell, the third annular shell and the cylindrical shell are obtained through the design values for circular radii of the shells by calculation.
Given that a thickness of the conical shell is t1:
where p represents a calculated pressure, [σ] represents an allowable stress, α represents the half-cone angle, R1 represents a radius of a large end of the conical shell, r represents a radius of a small end of the conical shell, and K1 represents a parameter related to reinforcing ribs;
a meridional thin film stress σφ, a circumferential thin film stress σθ and an equivalent stress σe of the conical shell are respectively according to a theory of thin shell:
the meridional thin film stress σφ and the circumferential thin film stress σθ are substituted into the equivalent stress σe to determined a thickness of a conical shell with equal thickness t1e based on a criterion of a maximum equivalent stress [σe]max being less than or equal to the allowable stress [σ] of materials, in consideration of the maximum equivalent stress [σe]max being equal to the allowable stress [σ] of the materials during design;
according to a calculation formula of a buckling load for the conical shell:
a thickness of the conical shell with equal thickness t1b is determined by calculation;
the thickness of the shell derived from a principle of thin films and the formula of the buckling load above is calculated respectively, and a maximum thickness of the two is determined as an ultimate thickness of the conical shell.
Given that a thickness of annular shells of the first annular shell, the second annular shell and the third annular shell ti is:
where i takes 2, 3, 4, p represents the calculated pressure, [σ] represents the allowable stress, Ri represents a rotating pitch diameter of the annular shell, ri represents a circumference radius of the annular shell, α represents the half-cone angle, E represents an elastic modulus, μ represents Poisson's ratio;
the maximum meridional thin film stress σφ, the maximum circumferential thin film stress σθ and the maximum equivalent stress σe of the annular shell are respectively according to the theory of thin shell:
the maximum meridional thin film stress σφ and the maximum circumferential thin film stress σθ are substituted into the maximum equivalent stress σe to determine a thickness of an annular shell with equal thickness tie, based on a criterion of the maximum equivalent stress [σe]max being less than or equal to the allowable stress [σ] of materials, in consideration of the maximum equivalent stress [σe]max being equal to the allowable stress [σ] of the materials during design;
According to Jordan Formula, a critical buckling load for the annular shell is expressed as:
a thickness of the annular shell with equal thickness tib is determined by calculation according to the above formula;
The thickness of the shell derived from the principle of thin film and the formula of the load above is respectively calculated, and a maximum thickness of the two is determined as an ultimate thickness of the first annular shell, the second annular shell and the third annular shell.
Given that a thickness of the cylindrical shell t5 is:
where p represents the calculated pressure, [σ] represents the allowable stress, R represents a rotating radius of the cylindrical shell, l represents a height of the cylindrical shell and E represents the elastic modulus;
a meridional thin film stress σφ, a circumferential thin film stress σθ and an equivalent stress σe of the cylindrical shell are respectively according to the theory of thin shell:
the meridional thin film stress σφ and the circumferential thin film stress σθ are substituted into the equivalent stress σe to determine a thickness of a cylindrical shell with equal thickness t5e, based on a criterion of the maximum equivalent stress [σe]max being less than or equal to the allowable stress [σ] of materials, in consideration of the maximum equivalent stress [σe]max being equal to the allowable stress [σ] of the materials during design;
a calculation formula of a buckling load for the cylindrical shell is:
a thickness of the cylindrical shell with equal thickness t5b is determined by calculation; and
the thickness of the shell derived from the principle of thin films and the formula of the load above is respectively calculated, and a maximum thickness of the two is determined as an ultimate thickness of the cylindrical shell.
Optimally, in Step 1, it is taken that K1=1.
Beneficial effects are that: compared with the prior art, the advantages of the present disclosure are as follows.
The present disclosure is further elucidated below in conjunction with the drawings and specific embodiments, it should be understood that these embodiments are merely intended to illustrate the present disclosure and not to limit the scope of the present disclosure.
The pyram-shaped deep-sea pressure-resistant shell, as illustrated in
The upper end of the first annular shell 2 is connected to the conical shell 1 and the two are interconnected with each other. The perforated thick plate 7 blocks the bottom end of the third annular shell 4 and the two are connected with each other by a plurality of flange bolts 6. The flange bolt 6 includes a bolt 61, a first flange 62, a sealing ring 63, a second flange 64, a washer 65 and a nut 66. The first flange 62 is fixed to a bottom surface of the annular combined shell, the second flange 64 is fixed to a bottom surface of the perforated thick plate 7, the bolt 61 is threaded and arranged in the first flange 62 and the second flange 64 in sequence, such that the first flange 62 and the second flange 64 are in securely threaded-connection with each other through the nut 66, the sealing ring 63 is arranged between a connection surface of the first flange 62 and the second flange 64, and the washer 65 is arranged between a contact surface of the nut 66 and the second flange 64.
The cylindrical shell 5 is disposed inside the third annular shell 4 and the lower end of the cylindrical shell 5 is inserted in a gap between the annular combined shell and the perforated thick plate 7, and an upper end and the lower end of the cylindrical shell 5 are respectively connected to an inner peripheral surface of the annular combined shell. The outer peripheral surface of the cylindrical shell 5 is provided with at least two channels, so that the first annular shell 2, the second annular shell 3 and the third annular shell 4 are interconnected with each other.
Outer shell surfaces of the first annular shell 2, the second annular shell 3 and the third annular shell 4 are all circular arc surfaces, with outer diameters of the first annular shell 2, the second annular shell 3 and the third annular shell 4 increasing in sequence. The centers of the circular cross-sections of the circular arc surfaces of the first annular shell 2, the second annular shell 3 and the third annular shell 4 are all located on an extension line of the outer profile of the conical shell 1. The conical shell 1, the first annular shell 2, the second annular shell 3 and the third annular shell 4 are sequentially welded and fixed into a whole.
The above method of designing the pyram-shaped deep-sea pressure-resistant shell, comprises the following steps.
The height of the isosceles triangle inside the pyram-shaped deep-sea pressure-resistant shell is as shown in Formula (1),
H=(L+2r2+2r3+2r4)cos α; (1)
where L represents a length of a generatrix for the conical shell, r2 represents a circumference radius of the first annular shell, r3 represents a circumference radius of the second annular shell, r4 represents a circumference radius of the second annular shell, and α represents a half-cone angle, and
rotation radii of the conical shell, the first annular shell, the second annular shell, the third annular shell and the cylindrical shell are obtained through the design values for circular radii of the shells by calculation.
Given that a thickness of the conical shell in the pyram-shaped deep-sea pressure-resistant shell is t1:
where p represents a calculated pressure, [σ] represents an allowable stress, α represents the half-cone angle, R1 represents a radius of a large end of the conical shell, r represents a radius of a small end of the conical shell, and K1 represents a parameter related to reinforcing ribs, and it is taken that K1=1,
the derivation processes of Formulas (3) and (4) are as follows:
according to a theory of thin shell, a meridional thin film stress σφ, a circumferential thin film stress σθ and an equivalent stress σe of the conical shell are as shown by Formulas (5) to (7):
the formula (5) and the formula (6) are substituted into the formula (7) to obtain the equivalent stress of the shell; a thickness of a conical shell with equal thickness t1e in Formula (3) is determined, based on a criterion of a maximum equivalent stress [σe]max is less than or equal to the allowable stress [σ] of materials, in consideration of the maximum equivalent stress [σe]max being equal to the allowable stress [σ] of the materials during design.
The calculation formula of a buckling load for the conical shell is:
the thickness of the conical shell with equal thickness t1b in Formula (4) is determined by calculation through the above Formula (8), and
the thickness of the shell derived from the principle of thin films and the formula of the buckling load above is respectively calculated, and a maximum thickness of the two is determined as an ultimate thickness of the conical shell.
The thickness of annular shells of the pyram-shaped deep-sea pressure-resistant shell ti is:
where i takes 2, 3, 4, p represents the calculated pressure, [σ] represents the allowable stress, Ri represents a rotating pitch diameter of the annular shell, ri represents a circumference radius of the annular shell, α represents the half-cone angle, E represents an elastic modulus, μ represents Poisson's ratio,
the derivation processes of Formulas (10) and (11) are as follows:
according to the theory of thin shells, the maximum meridional thin film stress σφ, the maximum circumferential thin film stress σθ and the maximum equivalent stress σe of the annular shell are as shown by Formulas (12) to (14):
the formula (12) and the formula (13) are substituted into the formula (13) to obtain the maximum equivalent stress of the shell; a thickness of an annular shell with equal thickness tie in Formula (10) is determined based on a criterion of the maximum equivalent stress [σe]max being less than or equal to the allowable stress [σ] of materials, in consideration of the maximum equivalent stress [σe]max being equal to the allowable stress [σ] of the materials during design,
according to Jordan Formula, a critical buckling load for the annular shell is expressed as:
according to the above formula (15), a thickness of the annular shell with equal thickness tib in (11) is determined by calculation,
the thickness of the shell derived from the principle of thin film and the load formula above are respectively calculated, and a maximum thickness from two of them is determined as an ultimate thickness of the annular shell.
When a thickness of the cylindrical shell t5 in the pyram-shaped deep-sea pressure-resistant shell is:
where p represents the calculated pressure, [σ] represents the allowable stress, R represents a rotating radius of the cylindrical shell, l represents a height of the cylindrical shell and E represents the elastic modulus,
the derivation processes of Formulas (17) and (18) are as follows:
according to the theory of thin shells, a meridional thin film stress σφ, a circumferential thin film stress σθ and an equivalent stress σe of the cylindrical shell are as shown by Formulas (19) to (21):
Formula (19) and Formula (20) are substituted into Formula (21) to obtain the equivalent stress of the shell; a thickness of a cylindrical shell with equal thickness t5e in Formula (17) is determined, based on a criterion of the maximum equivalent stress [σe]max being less than or equal to the allowable stress [σ] of materials, in consideration of the maximum equivalent stress [σe]max being equal to the allowable stress [σ] of the materials during design,
the calculation formula of a buckling load for the cylindrical shell is:
the thickness of the cylindrical shell with equal thickness t5b in Formula (18) is determined by calculation through the above formula (22),
the thickness of the shell derived from the principle of thin films and the formula of the load above is respectively calculated, and a maximum thickness of the two is determined as an ultimate thickness of the cylindrical shell,
A calculation example of the above design method is as follows.
The pyram-shaped deep-sea pressure-resistant shell and the perforated thick plate under the shell are made of high strength steel 0Cr17Ni4Cu4Nb, the allowable stress [σ] is 865 MPa, the elastic modulus of the materials is 213 GPa, the Poisson's ratio is 0.27, the density is 7.78 g/cm3, according to the above formulas, the structure design of the pyram-shaped deep-sea pressure-resistant shell under water depth 2 Km is carried out.
The half-cone angle of the conical shell α is designed to be 30°, and the proportion of each segment on the waist of the isosceles triangle on the pressure-resistant shell is L:2r2:2r3:2r4=1:1:2:4, the length of L is designed to be 1 m, then r2 is 0.5 m, r3 is 1 m, r4 is 2 m, the rotation radii of the conical shell, the first annular shell, the second annular shell, the third annular shell and the cylindrical shell are obtained by calculation, so that R1 is 0.5 m, R2 is 0.75 m, R3 is 1.5 m, R4 is 3 m, R5 is 2 m.
The height H of is the whole pyram-shaped deep-sea pressure-resistant shell is obtained by calculating according to Formula (1):
The calculated pressure p which is 32.67 MPa under water depth 2 Km is obtained according to Formula (16):
p=Kρ
0
gh/0.9; (16)
where K represents a safety factor, which is taken to be 1.5; ρ0 represents the density of sea water, which is taken to be take 1000 kg/m3; g represents the acceleration of gravity, which is taken to be 9.8 m/s2; h represents the water depth, which is taken to be 2 Km.
The thickness of the conical shell:
the thickness of the conical shell is obtained by calculation according to Formula (3):
the thickness of the conical shell is obtained by calculation according to Formula (4):
the thickness of the conical shell t1 is obtained according to Formula (2):
t
1=Max{t1e, t1b}=Max{0.005,0.019}=0.019 m.
The thickness of the first annular shell:
the thickness of the first annular shell is obtained by calculation according to Formula (10):
the thickness of the first annular shell is obtained by calculation according to Formula (11):
the thickness of the first annular shell t2 is obtained according to Formula (9):
t
2=Max{t2e, t2b}=Max{0.014,0.076}=0.076 m.
The thickness of the second annular shell:
the thickness of the second annular shell is obtained by calculation according to Formula (10):
the thickness of the second annular shell is obtained by calculation according to Formula (11):
the thickness of the second annular shell t3 is obtained according to Formula (9):
t
2=Max{t2e, t2b}=Max{0.043,0.056}=0.056 m.
The thickness of the third annular shell:
the thickness of the third annular shell is obtained by calculation according to the formula (10):
the thickness of the third annular shell is obtained by calculation according to Formula (11):
the thickness of the third annular shell t4 is obtained according to Formula (9):
t
2=Max{t2e, t2b}=Max{0.057,0.042}=0.057 m.
The thickness of the cylindrical shell:
the height of the cylindrical shell is design to be the height of the intermediate part of the third annular shell, and the height l is taken to be 3.4 m.
the thickness of the cylindrical shell is obtained by calculating according to Formula (17):
the thickness of the cylindrical shell is obtained by calculating according to Formula (18):
the thickness of the cylindrical shell t5 is obtained according to Formula (16):
t
5=Max{t5e, t5b}=Max{0.065,0.076}=0.076 m.
The specific design parameters of the pressure-resistant shell in this embodiment are as shown in Table 1.
indicates data missing or illegible when filed
Number | Date | Country | Kind |
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202111384175.3 | Nov 2021 | CN | national |
Filing Document | Filing Date | Country | Kind |
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PCT/CN2022/081712 | 3/18/2022 | WO |