Stress-based method for optimization of joint members within a complex structure

Patent metadata

Field	Value
Publication number	US-10960468-B2
Application number	US-201715809528-A
Country	US
Kind code	B2
Filing date	Nov 10, 2017
Priority date	Jul 2, 2014
Publication date	Mar 30, 2021
Grant date	Mar 30, 2021

Abstract

A method for fabricating a joint designed to connect tubes for a space frame, where a space frame may be a vehicle chassis, is provided. The method may generate joints with variable geometry and fine features which may reduce production costs, reduce production time, and generate joints configured for highly specific applications. The joint may include centering features which may create a space between a surface of the tube and a surface of the joint through which adhesive may flow.

First claim

What is claimed is:

1. A method of fabricating a joint member for connection of a plurality of connecting tubes forming a space frame,
the method comprising: determining a relative tube angle,
tube size, and tube shape for each of the plurality of connecting tubes to be connected by the joint member;
determining a stress direction and magnitude to be exerted by the plurality of connecting tubes at the joint member; and
3-D printing the joint member having a configuration that accommodates the relative tube angle,
tube size, and tube shape at each joint member, and
supports the stress direction and magnitude exerted by the plurality of connecting tubes; and
wherein the joint member comprises a joint protrusion on sidewalls of connecting tubes configured to be inserted into a connecting tube, and
one or more nipples configured to allow introduction of adhesive in a space between the joint protrusion on the sidewalls of nipples and at least on one of the connecting tube side walls.

2. The method of claim 1 , wherein the space frame is configured to at least partially enclose a three-dimensional volume.

3. The method of claim 1 , wherein each connecting tube of the plurality of connecting tubes has a longitudinal axis along a different plane.

4. The method of claim 1 , wherein the space frame is a vehicle chassis frame.

5. The method of claim 1 , further comprising 3-D printing centering features on at least a portion of the joint member, wherein the centering features comprise a regular or irregular pattern of raised bumps.

6. The method of claim 5 , wherein the centering features are printed on the joint protrusion of the joint member configured to be inserted into a connecting tube.

7. The method of claim 5 , wherein the characteristics of the centering features are determined based on the stress direction and magnitude to be exerted by the plurality of connecting tubes at the joint member.

8. The method of claim 1 , wherein the stress direction and magnitude to be exerted by the plurality of connecting tubes at the joint member is determined empirically or computationally.

9. The method of claim 1 , wherein the nipples are 3-D printed on the joint member at the time that the joint member is printed and are carved from the same bulk material.

10. The method of claim 1 , wherein the nipples are positioned on opposite sides of the joint member.

11. A method of fabricating a joint member for connection of a plurality of connecting tubes forming a space frame, the method comprising:
receiving, by a computer,
a design describing the space frame;
determining specifications, by the computer, of the plurality of connecting tubes,
wherein the specifications comprise a relative tube angle, tube size, and tube shape for each of the plurality of connecting tubes to be connected by the joint member;
determining structural requirements, by the computer,
wherein the structural requirements comprise a stress direction and magnitude to be exerted by the plurality of connecting tubes at the joint member; and
3-D printing the joint member, wherein the joint member has a configuration that accommodates the relative tube angle, tube size, and tube shape at each joint member, and
supports the stress direction and magnitude exerted by the plurality of connecting tubes wherein the joint member comprises a joint protrusion on sidewalls of connecting tubes configured to be inserted into a connecting tube, and one more nipple configured to allow introduction of adhesive in a space between the joint protrusion on the sidewalls of nipples and at least one of the connecting tubes side walls.

12. The method of claim 11 , wherein the space frame is configured to at least partially enclose a three-dimensional volume.

13. The method of claim 11 , wherein each connecting tube of the plurality of connecting tubes has a longitudinal axis along a different plane.

14. The method of claim 11 , wherein the space frame is a vehicle chassis frame.

15. The method of claim 11 , wherein the computer is a server.

16. The method of claim 11 , wherein the received design comprises a 3D model describing a framework of a vehicle chassis.

Assignees

• Divergent Tech Inc

Inventors

• Czinger Kevin Robert
• Balzer William Bradley
• Penmetsa Praveen Varma
• Omohundro Zachary Meyer
• O'Brien Matthew M

Classifications

• B22F10/10

  Formation of a green body · CPC title

• B22F5/10 Primary

  of articles with cavities or holes, not otherwise provided for in the preceding subgroups · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• B22F2998/10

  Processes characterised by the sequence of their steps · CPC title

• G06F30/15

  Vehicle, aircraft or watercraft design · CPC title