Space frame center upper frame nodal connection

Patent metadata

Field	Value
Publication number	US-11358641-B2
Application number	US-201916663955-A
Country	US
Kind code	B2
Filing date	Oct 25, 2019
Priority date	Oct 25, 2019
Publication date	Jun 14, 2022
Grant date	Jun 14, 2022

Abstract

A center upper frame nodal connection fabrication comprising a top surface, a bottom surface opposite the top surface, two side surfaces, a front surface having a plurality of integral planes oriented at angles relative to each other, and a rear surface opposite the front surface. The top surface, the bottom surface, and the two side surfaces can be weldably attached to each other and the front and rear surfaces to form a structure of the center upper frame nodal connection fabrication. The integral planes of the front surface are configured to weldably attach to respective elongate support members of a space frame. The rear surface is configured to weldably attach to a center upper frame connection casting of the space frame.

First claim

The invention claimed is:

1. A space frame for an off-highway rear haul truck comprising:
a first center upper frame nodal connection fabrication; and
a second center upper frame nodal connection fabrication spaced from the first center upper frame nodal connection fabrication in a width direction of the space frame,
wherein each of the first and second center upper frame nodal connection fabrications includes:
a top surface,
a bottom surface opposite the top surface,
two side surfaces,
a front surface having three integral planes oriented at obtuse angles relative to each other, wherein each of the three integral planes is configured to weldably attach a respective frame tube perpendicular thereto, and
a rear surface opposite the front surface configured to weldably attach a center upper frame connection casting,

wherein the top surface, the bottom surface, and the two side surfaces are weldably attached to each other and the front and rear surfaces to create a box structure.

2. The space frame according to claim 1 , wherein the three integral planes of the first and second center upper frame nodal connection fabrications face upward and the rear surfaces face downward.

3. The space frame according to claim 1 , wherein, in a side view of the space frame, the three integral planes of each of the first and second center upper frame nodal connection fabrications face at a positive acute angle relative to horizontal.

4. The space frame according to claim 1 , wherein the rear surface is parallel to a middle integral plane of the three integral planes of the front surface.

5. The space frame according to claim 1 , wherein the front surface is wider than the rear surface.

6. The space frame according to claim 1 , wherein the side surfaces are recessed from side edges of the top and bottom surfaces.

7. The space frame according to claim 1 , wherein opposite ends of the front surface extend past side edges of the top and bottom surfaces.

8. A center upper frame nodal connection fabrication comprising:
a top surface;
a bottom surface opposite the top surface;
two side surfaces;
a front surface having three integral planes oriented at obtuse angles relative to each other, wherein the three integral planes are configured to weldably attach to respective elongate support members of a space frame; and
a rear surface opposite the front surface configured to weldably attach to a center upper frame connection casting of the space frame,
wherein the top surface, the bottom surface, and the two side surfaces are weldably attached to each other and the front and rear surfaces.

9. The center upper frame nodal connection fabrication according to claim 8 , wherein the three integral planes are configured to face upward when provided in the space frame.

10. The center upper frame nodal connection fabrication according to claim 8 , wherein, in a side view the three integral planes are configured to face at a positive acute angle relative to horizontal when provided in the space frame.

11. The center upper frame nodal connection fabrication according to claim 8 , wherein the rear surface is parallel to a middle integral plane of the three integral planes of the front surface.

12. The center upper frame nodal connection fabrication according to claim 8 , wherein the front surface is wider than the rear surface.

13. The center upper frame nodal connection fabrication according to claim 8 , wherein the side surfaces are recessed from side edges of the top and bottom surfaces.

14. The center upper frame nodal connection fabrication according to claim 8 , wherein opposite ends of the front surface extend past side edges of the top and bottom surfaces.

15. The center upper frame nodal connection fabrication according to claim 8 , wherein each of the three integral planes of the front surface is configured to weldably attach the respective elongate support member thereto such that a longitudinal axis of the respective elongate support member is perpendicular to the corresponding integral plane.

16. A method comprising:
providing a top surface of a center upper frame nodal connection fabrication;
providing a bottom surface of the center upper frame nodal connection fabrication opposite the top surface;
providing two side surfaces of the center upper frame nodal connection fabrication;
providing a front surface of the center upper frame nodal connection fabrication, the front surface having three integral planes oriented at obtuse angles relative to each other, wherein the three integral planes are configured to weldably attach to respective frame tubes of a space frame; and
providing a rear surface of the center upper frame nodal connection fabrication, the rear surface being configured to weldably attach to a center upper frame connection casting of the space frame,
wherein the top surface, the bottom surface, and the two side surfaces are weldably attached to each other and the front and rear surfaces.

17. The method according to claim 16 , further comprising welding the top surface, the bottom surface, and the two side surfaces to each other and the front and rear surfaces to create a box structure, the box structure having a fan shape in a top plan view of the center upper frame nodal connection fabrication.

18. The method according to claim 16 , further comprising welding the frame tubes to the front surface.

19. The method according to claim 18 , wherein said welding is such that respective longitudinal axes of the frame tubes are perpendicular to corresponding ones of the three integral planes of the front face.

20. The method according to claim 16 , further comprising welding the rear surface to the center upper frame connection casting.

Assignees

• Caterpillar Inc

Inventors

• Miller Tad W

Classifications

• B62D27/023 Primary

  Assembly of structural joints · CPC title

• B62D23/005 Primary

  with integrated chassis in the whole shell, e.g. meshwork, tubes, or the like (B62D33/044 takes precedence) · CPC title

• B62D21/12

  assembled from readily detachable parts · CPC title

• B62D21/09 Primary

  Means for mounting load bearing surfaces · CPC title

• B62D21/06

  of X-shaped or fork-shaped construction, i.e. having members which form an X or fork as the frame is seen in plan view · CPC title