IP Library › Granted Patent US 11,358,641
Granted Patent B2
US 11,358,641 · App. 16/663,955 · Granted Jun 14, 2022

Space frame center upper frame nodal connection

Inventor: Tad W. Miller (Bonney Lake, WA)
Assignee: Caterpillar Inc.
B62D21/09B62D21/06B62D23/005B62D27/023B23K2101/006
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,358,641
App. No.
16/663,955
Granted
Jun 14, 2022
Kind
B2
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.

Claims (41)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 25, 2019
From: MILLER, TAD W
To: CATERPILLAR INC.
Reel/Frame 050827/0489 →
Continuity (1)
Related Publication 20210122421A1 · Apr 29, 2021
Cited By (1)
US 12,691,942