HYBRID METAL POLYMER INTERLOCK

Abstract

A mechanical coupling assembly that includes a primary substrate having at least one aperture formed therein. A secondary substrate includes at least one mechanical interlock monolithically formed with the secondary substrate. The at least one mechanical interlock extends through the aperture. The mechanical interlock includes a main body and a head portion with a transition portion connecting the main body and head portions. The main body includes a bore formed longitudinally therein about a centerline of the aperture. The mechanical interlock joins the primary substrate and secondary substrate mechanically.

Claims

1. A mechanical coupling assembly comprising: a primary substrate having at least one aperture formed therein, the primary substrate including a first surface and opposing second surface separated by a material thickness; a secondary substrate including at least one mechanical interlock monolithically formed with the secondary substrate, the at least one mechanical interlock extending through the aperture and spanning the first and second surfaces, the mechanical interlock including a main body disposed proximate the first surface and a head portion disposed proximate the second surface and a transition portion connecting the main body and head portion; wherein the main body includes a bore formed longitudinally therein about a centerline of the aperture and the primary substrate and secondary substrate are mechanically joined.

2. The mechanical coupling assembly of claim 1 wherein the main body and head portion includes a uniform thickness.

3. The mechanical coupling assembly of claim 1 wherein the main body and head portion extend radially about the aperture the same distance.

4. The mechanical coupling assembly of claim 1 wherein the primary substrate is formed of metal and the secondary substrate is formed of a polymeric material.

5. The mechanical coupling assembly of claim 4 wherein the polymeric material is a fiber reinforced polymeric material.

6. The mechanical coupling assembly of claim 1 wherein the transition portion includes a radial slot formed therein receiving the primary substrate.

7. The mechanical coupling assembly of claim 1 wherein the bore is sized to define a uniform thickness of the head portion and the main body.

8. The mechanical coupling assembly of claim 1 wherein the secondary substrate is over-molded onto the primary substrate.

9. A mechanical coupling assembly comprising: a metal primary substrate having at least one aperture formed therein, the primary substrate including a first surface and opposing second surface separated by a material thickness; a polymeric secondary substrate including at least one mechanical interlock monolithically formed with the secondary substrate, the at least one mechanical interlock extending through the aperture and spanning the first and second surfaces, the mechanical interlock including a main body disposed proximate the first surface and a head portion disposed proximate the second surface and a transition portion connecting the main body and head portion; wherein the main body and head portion have a uniform thickness and the main body and the primary substrate and secondary substrate are mechanically joined.

10. The mechanical coupling assembly of claim 9 wherein the main body and head portion extend radially about the aperture the same distance.

11. The mechanical coupling assembly of claim 9 wherein the polymeric material is a fiber reinforced polymeric material.

12. The mechanical coupling assembly of claim 9 wherein the transition portion includes a radial slot formed therein receiving the primary substrate.

13. The mechanical coupling assembly of claim 9 wherein the secondary substrate is over-molded onto the primary substrate.

14. A method of forming a mechanical coupling assembly comprising the steps of: providing a primary substrate having at least one aperture formed therein; over-molding a secondary substrate onto the primary substrate forming a mechanical interlock, the mechanical interlock including a main body disposed proximate the first surface and a head portion disposed proximate the second surface and a transition portion connecting the main body and head portion; wherein the main body includes a bore formed longitudinally therein about a centerline of the aperture and the primary substrate and secondary substrate are mechanically joined.

15. The method of claim 14 wherein the step of providing a primary substrate includes: determining an outer radius of the primary substrate; determining a size of the aperture; determining a thickness of the primary substrate; selecting a primary substrate material having a tensile modulus.

16. The method of claim 14 wherein the step of over-molding includes: determining a size of the head; determining a thickness of the secondary substrate; selecting a secondary substrate material having a tensile modulus.

17. The method of claim 14 wherein the step of over-molding includes: calculating a polar solution for plate deflection with a point load at various positions.

18. The method of claim 17 wherein the step of over-molding includes: calculating a radial, tangential and shear stress of various positions according to the equation: wherein the various stress components for the radial, tangential and shear stresses are less than a mechanical yield.

19. The method of claim 18 wherein the step of over-molding includes: section the calculated values of values of radial, tangential and shear stress using a yield stress plane and the size of the aperture and the size of the size of the head.

20. The method of claim 19 wherein the step of over-molding includes: performing a parametric analysis for various loads for various thicknesses of the secondary substrate.

21. The method of claim 20 wherein the step of over-molding includes: performing a parametric analysis for primary and secondary using a tensile modulus of the primary and secondary substrates.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0007] FIG. 1 is a sectional view of a mechanical coupling assembly;

[0008] FIG. 2 is a perspective view of a mechanical coupling assembly;

[0009] FIG. 3 is a front view of the mechanical coupling assembly of FIG. 2;

[0010] FIG. 4 is a schematic view detailing dimensions of a mechanical coupling assembly including the primary and secondary substrates;

[0011] FIG. 5 is a schematic representation of a general solution for displacement including the radial, tangential, and shear stresses for different regions of a plate;

[0012] FIG. 6 is a plot of the shoulder width as a function of hole radius for various loads;

[0013] FIG. 7 is a plot of the hole radius, shoulder width, and total stress;

[0014] FIG. 8 is a plot of the hole radius, thickness, and shoulder width for various loads; and

[0015] FIG. 9 is a plot of the hole radius, shoulder width, and total stress.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0016] Referring to FIGS. 1-3, there is shown a mechanical coupling assembly 10 that includes a primary substrate 12 having at least one aperture 14 formed therein. It should be realized that various numbers of apertures may be formed in the primary substrate 12. The primary substrate 12 includes a first surface 16 and an opposing second surface 18 that are separated by a material thickness 20. A secondary substrate 22 includes at least one mechanical interlock 24 monolithically formed with the secondary substrate 22. The at least one mechanical interlock 24 extends through the aperture 14 and spans the first and second surfaces 16, 18. The mechanical interlock 24 includes a main body 26 disposed proximate the first surface 16 and a head portion 28 disposed proximate the second surface 18. A transition portion 30 connects the main body 26 and head portion 28. In one aspect, the main body 26 includes a bore 32 formed longitudinally therein about a centerline of the aperture 14. The mechanical interlock 24 joins the primary and secondary substrates 12, 22 mechanically.

[0017] In one aspect, the bore 32 formed longitudinally about the centerline of the aperture 14 allows the main body 26 and head portion 28 to include a uniform thickness. The uniform thickness allows for specific design characteristics to be met as well as assures even flow and distribution of the secondary substrate 22 in an over-molding process alleviating potential failure modes of the mechanical interlock 24.

[0018] In one aspect, the main body 26 and head portions 28 extend radially about the aperture 14 the same distance. In other words, the shoulder width 34 of the main body 26 and head portion 28 are equal. It should be realized that different shoulder widths may also be utilized. As can be seen in FIG. 1, the head portion 28 extends radially about the aperture 14 a specified shoulder width 34. The same shoulder width 34 is provided on the main body portion 26. As described above, the transition portion 30 connects the head portion 28 and main body 26. In one aspect, the transition portion 30 includes a radial slot 36 defined therein that receives the primary substrate 12.

[0019] The primary substrate 12 may be formed of various materials that are dissimilar relative to the secondary substrate 22. In one aspect, the primary substrate 12 may be formed of a metal material such as, for example, aluminum, magnesium, steel, or other metal materials. The secondary substrate 22 may be formed of a polymeric material that is capable of flowing in an over-molding process. In one aspect, the polymeric material may include a fiber reinforced polymeric material, such as glass reinforced nylons, carbon fiber reinforced polymers and plastics and over-moldable reinforced thermo-plastics.

[0020] As described above, the main body 26 includes a bore 32 formed longitudinally therein about a centerline of the aperture 14. In one aspect, the bore 32 is sized to define the uniform thickness of the head portion 28 and the main body 26. Additionally, when a fiber reinforced polymeric material is utilized as the secondary substrate 22, the uniform thickness assures alignment of the fibers during the over-molding process, again avoiding potential failure modes of the mechanical interlock 24.

[0021] There is also disclosed a method of forming a mechanical coupling assembly 10 that includes the steps of providing a primary substrate 12 having at least one aperture 14 formed therein, over-molding a secondary substrate 22 onto the primary substrate 12 forming a mechanical interlock 24, the mechanical interlock 24 including a main body 26 disposed proximate the first surface 16 and a head portion 28 disposed proximate the second surface 18 with a transition portion 30 connecting the main body 26 and head portion 28. The main body 26 includes a bore 32 formed longitudinally therein about a centerline of the aperture 14. The bore 32 may be defined by a pin in the over molding process. The primary and secondary substrates 12, 22 are mechanically joined by the interlock 24.

[0022] The method of forming a mechanical coupling assembly 10 includes specifying parameters of the primary and secondary substrates 12, 22. As shown in FIG. 4, in one aspect, the step of providing a primary substrate 12 includes determining an outer radius a of the primary substrate 12, determining a size b of the aperture 14, determining a thickness hp of the primary substrate 12, and selecting a primary substrate 12 material having a tensile modulus. The method also includes determining various parameters of the secondary substrate 22 in the step of over-molding. In one aspect, the step of over-molding includes determining a size b+c of the head portion 28, determining a thickness hs of the secondary substrate 22, and selecting a secondary substrate material having a tensile modulus. Referring to FIGS. 4 and 5, there are shown schematic representations of the parameters of the primary and secondary substrates 12, 22.

[0023] In one aspect, the step of over-molding includes calculating a polar solution for plate deflection with a point load at various positions (center of the interlock) using boundary conditions and solution continuity in accordance (with regions of different stiffness as in equation 1)

[00001]$\begin{array}{cc}{k}_1=\frac{E_s.Math.h_s^3}{12.Math.\left(1-v_s^2\right)},k_2=\frac{E_p.Math.h_p^3}{12.Math.\left(1-v_p^2\right)}+\frac{{E_p\left(h_s-h_p\right)}^3}{12.Math.\left(1-v_s^2\right)},.Math.k_3=\frac{E_p.Math.h_p^3}{12.Math.\left(1-v_p^2\right)}& \left(\mathrm{EQ}.Math..Math.1\right)\end{array}$

After calculating the polar solution, a radial, tangential, and shear stress are evaluated according to Equation 2:

.sub.Vonmises={square root over ((.sub.r.sup.2+.sub..sup.2.sub.r.sub.+3.sup.2))}(EQ 2)

The radial, tangential and shear stress component should be lower than the material yield .sub.Y, for each region subject to the constraints:

[00002]$b>0,c>0,\left(b+c\right)<\frac{a}{2}.$

As shown in FIG. 5, the various parameters including the radial, tangential, and shear stresses are graphically depicted. In one aspect, the various stress components for the radial, tangential, and shear stresses are less than a mechanical yield of the secondary substrate.

[0024] Referring to FIG. 6, there is shown a plot of the shoulder width of the secondary substrate 22 as a function of the hole radius of the primary substrate 12. The plot is sectioned for various load conditions. In one aspect, the plot is generated by initially providing variables b and c representative of the hole radius or aperture and shoulder width as shown in FIG. 4. Additionally, parameters are provided for the thickness of the primary substrate 12 which is set as 1 mm in the plot and the secondary substrate 22 which is set as 6 mm in the plot. Additionally, tensile moduli of the primary and secondary substrates 12, 22 are set at 70 and 2 GPa respectively. It should be realized that various sizes and thicknesses as well as tensile modulus may be utilized as determined by the design parameters of the primary and secondary substrates 12, 22. The following plots are utilized to demonstrate the process using one set of parameters for exemplary purposes.

[0025] Referring to FIG. 7, there is shown a plot of the hole radius and shoulder width as a function of the total stress. In one aspect, the plot is generated such that the step of over-molding includes sectioning the calculated values of the radial, tangential, and shear stress using a yield stress plane as well as the size of the aperture and the size of the head. Again, it should be realized that these plots may be generated for various materials for both the primary and secondary substrates 12, 22.

[0026] Referring to FIG. 8, there is shown a plot of the shoulder width, hole radius, and thickness of the secondary substrate 22 for various load parameters. This plot takes into account the design variables of the substrate thickness. The plot is generated utilizing a parametric analysis for various loads and various thicknesses of the secondary substrate 22.

[0027] Referring to FIG. 9, there is shown a plot of the hole radius and shoulder width as a function of the total stress. This plot is generated by performing a parametric analysis for the primary and secondary substrates 12, 22 using a tensile modulus of the primary and secondary substrates 12, 22. This plot takes into account the individual strength characteristics of the primary and secondary substrates 12, 22 to meet a specified load condition.

[0028] The method provides a verifiable process to create mechanical interlocks 24 between dissimilar primary and secondary substrates 12, 22 using an over-molding process. Various over-molding processes such as injection molding and co-molding as well as compression molding may be utilized. The process will allow specific interlocks 24 to be specified for a desired load application.