Abstract
An internal support part structure for a plastic tank includes a support rod and end surface components disposed at two ends of the support rod. The support rod is made of a first material. An outer surface of the end surface component is covered by a second material. An outer edge of the end surface component has a regular or irregular shape. The structure resolves a problem that a second material wrapping a first material and connected to an inner wall of a plastic tank may be easily pulled off the inner wall. When a fuel tank is impacted, the support rod of the structure breaks first, to protect the surface of the fuel tank from damage.
Claims
1. An internal support part structure for a plastic tank,the structure comprises comprising comprising a support rod and end surface components; wherein the end surface components are disposed at two ends of the support rod, the support rod is made of a first material, an outer surface of each end surface component of the end surface components is covered by a second material, an outer edge of the each end surface component has a regular shape or an irregular shape, and a ratio of a cross-sectional diameter at any uposition of the each end surface component to a cross-sectional diameter at a position of the support rod is less than 1.8 and greater than 1.
2. The internal support part structure according to claim 1, wherein the outer edge of the each end surface component is V-shaped, W-shaped, semicircular, arc-shaped, triangular, zigzag, or polygonal.
3. The internal support part structure according to claim 2, wherein the cross-sectional diameter of the each end surface component is greater than the cross-sectional diameter of the support rod.
4. The internal support part structure according to claim 3, wherein the first material is a reinforced engineering plastic comprising polyphthalamide (PPA), polyphenylene sulfide (PPS), polyoxymethylene (POM), or polyamide (PA), or the first material is a metal material; and the second material is polyethylene (PE) or high-density PE (HDPE).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009] FIG. 1 is a side view of the present invention;
[0010] FIG. 2 is a side view of a support rod;
[0011] FIG. 3 is a schematic diagram of an upper surface of a first material;
[0012] FIG. 4 is a top view of the present invention; and
[0013] FIG. 5 is a schematic structural diagram of an outer edge of an end surface component.
[0014] In the figures: 1. support rod, 2. end surface component, 3. outer edge, 4. first material, and 5. second material.
DETAILED DESCRIPTION OF THE EMBODIMENTS
[0015] To deepen the understanding of the present invention, this embodiment is described in detail below with reference to the accompanying drawings.
[0016] Embodiment 1: Referring to FIG. 1 and FIG. 2, an internal support part structure for a plastic tank is provided. The structure includes a support rod 1 and end surface components 2 disposed at two ends of the support rod. The support rod is made of a first material 4. An outer surface of the end surface component is covered by a second material 5. An outer edge of the end surface component has a regular or irregular shape. Referring to FIG. 5, the outer edge 3 of the end surface component is V-shaped, W-shaped, semicircular, arc-shaped, triangular, zigzag, or polygonal. The end surface of the support rod is covered with the second material, and the second material is the same as the material of a fuel tank. The first material is a reinforced engineering plastic such as PPA, PPS, POM, or PA, or a metal material; and the second material is PE or HDPE. The material of the support rod is the first material or the second material. The first material and the second material are the same or different. The support rod is hollow. A cross-sectional diameter of the end surface of the support rod is greater than a cross-sectional diameter of the support rod. A ratio of a maximum cross-sectional diameter at any position of the support rod to a cross-sectional diameter at any position of the support rod is less than 1.8 and greater than 1. In this solution, the discontinuity of the outer edge of the end surface is to increase a pull-off force between the first material and the second material, so that the support rod cannot be easily pulled off the surface of the fuel tank. A calculation formula of the pull-off force is: F=C*A*P, where C is a circumference of the outer edges of the upper and lower surfaces of the support rod, A is a cross-sectional area of a pull-off surface, and P is a shear strength of the second material. After the outer edges of the upper and lower surfaces of the support rod are designed into a shape such as “V” or “W”, lengths of the outer edges of the upper and lower surfaces of the support rod are increased, so that the pull-off force F′=C′*A*P, and the pull-off force is increased. C′ is the circumference of the outer edges of the upper and lower surfaces of the support rod in this application. Because C′ is greater than C, F′ is greater than F, and the pull-off force between the support rod and the surface of the fuel tank is increased. Before the fuel tank is put into mass production, the performance of the fuel tank needs to be tested. One of the important tests is an impact test of the fuel tank. In the impact test, the fuel tank is dropped from a height to check whether the fuel tank has a rupture or a fuel leakage. After a lot of tests, when a ratio of a maximum cross-sectional diameter of the end surface of the support rod to a minimum cross-sectional diameter of the support rod is 1.25, the fuel tank is protected from damage due to the rigid support rod when the fuel tank is impacted. However, it is not necessarily beneficial to maximize the ratio of the maximum cross-sectional diameter of the end surface of the support rod to the minimum cross-sectional diameter of the support rod. A larger diameter of the end surface of the support rod requires more materials and higher costs. Therefore, in consideration of the production costs and the effect that the support rod first breaks to avoid damage to the surface of the fuel tank when the fuel tank is impacted, a ratio of a cross-sectional diameter at any position of the end surface component to a cross-sectional diameter at any position of the support rod is less than 1.8 and greater than 1, and the support rod has larger diameters at two ends and a small diameter in the middle.
[0017] It should be noted that the above embodiments are not used to limit the protection scope of the present invention, and equivalent changes or substitutions made on the basis of the above technical solutions fall within the protection scope of the claims of the present invention.
