Method for forming a 3D printed seat support system

1. A method for forming a three-dimensionally (3D) printed flexible support apparatus, the method comprising:

producing arrays of V-spring elements using a 3D printing system, each array including a plurality of V-spring elements attached to one another and arranged in a predefined array shape, and each V-spring element having a predefined firmness or hysteresis characteristic;

arranging the arrays of V-spring elements in at least one two-dimensional (2D) array grid using the 3D printing system, such that at least one V-spring element of each array is attached to a V-spring element of at least one adjacent array; and

shaping the at least one array grid according to a predefined volume to form the support apparatus.

2. The method of claim 1 , further comprising:

forming a plurality of the array grids using the 3D printing system; and

vertically stacking the plurality of array grids using the 3D printing system, such that at least one V-spring element of each array is attached to a V-spring element of at least one array positioned above or below.

3. The method of claim 1 , further comprising:

producing the arrays of V-spring elements using the 3D printing system, such that the plurality of V-spring elements included in each array extend radially from a center axis of the predefined array shape.

4. The method of claim 1 , wherein each V-spring element includes two arms having a first end at which the two arms are attached and an opposite second end, the arms extending angularly with respect to each other from their respective first end toward their respective second end.

5. The method of claim 4 , further comprising:

producing the arrays of V-spring elements using the 3D printing system, such that the plurality of V-spring elements included in each array extend radially from a center axis of the predefined array shape, the respective second ends of each V-spring element in a given array being located on the center axis.

6. The method of claim 5 , wherein, in the given array, a second end of a V-spring element therein is attached to second ends of other V-spring elements therein on the center axis.

7. The method of claim 6 , wherein, in the given array, a second end of a first arm of the V-spring element therein is attached to second ends of first arms of the other V-spring elements therein on the center axis, and a second end of a second arm of the V-spring element therein is attached to second ends of second arms of the other V-spring elements therein on the center axis.

8. The method of claim 5 , wherein, in the given array, a first end of a V-spring element therein is attached to a first end of a V-spring element of at least one adjacent array in the array grid.

9. The method of claim 5 , wherein, in the given array, a first end of a V-spring element therein is attached to a first end of a V-spring element of a plurality of adjacent arrays in the array grid.

10. The method of claim 1 , wherein the predefined array shape is a hexagon.

11. The method of claim 1 , wherein the predefined volume is a 3D model defined using computer-aided design (CAD) techniques.

12. The method of claim 1 , wherein the predefined volume is shaped as a seat pan.

13. The method of claim 1 , further comprising:

defining the firmness or hysteresis characteristic for a given V-spring element; and

producing the V-spring element according to the defined firmness or hysteresis characteristic using the 3D printing system.

14. The method of claim 13 , wherein a firmness or hysteresis characteristic of a first V-spring element in a given array is different from a firmness or hysteresis characteristic of a second V-spring element in the given array.

15. The method of claim 13 , wherein an overall firmness or hysteresis characteristic of a first array is different from an overall firmness or hysteresis characteristic of a second array adjacent to the first array.

16. The method of claim 13 , wherein an overall firmness or hysteresis characteristic of a first section of arrays is different from an overall firmness or hysteresis characteristic of a second section of arrays adjacent to the first section.

17. The method of claim 13 , further comprising:

defining a size, shape, or material of the given V-spring element to achieve a desired firmness or hysteresis characteristic; and

producing the V-spring element according to the defined size, shape, or material using the 3D printing system.

18. The method of claim 13 , further comprising:

defining a width of the given V-spring element or a thickness of the given V-spring element to achieve a desired firmness or hysteresis characteristic; and

producing the V-spring element according to the defined width or thickness using the 3D printing system.

19. The method of claim 18 , wherein the defined width or thickness refers to a center portion of the given V-spring element, and the defined width or thickness at the center portion is different from a width or thickness at an end portion of the given V-spring element, respectively.

20. The method of claim 13 , further comprising:

providing a user interface to allow a user to select the firmness or hysteresis characteristic for the given V-spring element; and

producing the V-spring element according to the selected firmness or hysteresis characteristic using the 3D printing system.

21. The method of claim 1 , further comprising:

shaping the at least one array grid according to dimensions of the predefined volume, such that the at least one array grid fits within the predefined volume.