Structural joint with multi-axis load carrying capability

Patent metadata

Field	Value
Publication number	US-9546678-B2
Application number	US-201314105757-A
Country	US
Kind code	B2
Filing date	Dec 13, 2013
Priority date	Dec 14, 2012
Publication date	Jan 17, 2017
Grant date	Jan 17, 2017

Abstract

A structural joint is formed of a mandrel having a plurality of bumps and dimples formed thereon which is fitted into a sleeve. The bumps and dimples form a non-circular geometry at all points along the length of the mandrel. The bumps are defined by surfaces which have 1 st and 2 nd derivatives which are continuous.

First claim

The invention claimed is:

1. A structural joint comprising:
an elongate mandrel having opposite ends and a length defined therebetween, and an exterior surface with a plurality of bumps and dimples formed thereon, wherein the plurality of bumps and dimples alternate along the length and around a circumference of the mandrel to form non-circular transverse cross-sectional geometries at all points along the length of the mandrel, wherein each of the plurality of bumps is defined by a surface which has 1 st and 2 nd derivatives which are continuous; and
a sleeve surrounding the mandrel and having an interior surface conforming to the plurality of bumps and dimples on the mandrel such that the mandrel prevents torsional rotation of the mandrel relative to the sleeve and prevents axial translation of the mandrel relative to the sleeve.

2. The structural joint of claim 1 , wherein the mandrel is formed of one or more metallic materials.

3. The structural joint of claim 1 , wherein the mandrel is formed of one or more composite materials.

4. The structural joint of claim 1 , wherein the mandrel and the sleeve are formed of metallic or composite materials.

5. The structural joint of claim 1 , wherein the interior surface of the sleeve surrounding the mandrel includes bumps and dimples that closely conform to the plurality of bumps and dimples of the exterior surface of the mandrel.

6. The structural joint of claim 5 , wherein the mandrel and the sleeve are formed of metallic or composite materials.

7. The structural joint of claim 1 , wherein each of the plurality of bumps defines a crest having a radius which is equal to the radii of the crests of the other of the plurality of bumps.

8. The structural joint of claim 1 , wherein the elongate mandrel includes an axial bore having internal threads over at least a part of the length of the mandrel.

9. The structural joint of claim 1 , wherein the axial bore is attached to a component.

10. The structural joint of claim 1 , wherein each of the plurality of dimples defines a trough having a radius that is equal to the radii of the troughs of the other of the plurality of dimples.

11. The structural joint of claim 1 , wherein outer peripheries of a plurality of the non-circular transverse cross-sectional geometries are defined by a closed primary primitive curve with the 1 st derivative defining local slope and the 2 nd derivative defining local curvature.

12. A structural joint comprising:
an elongate mandrel having opposite ends and a length defined therebetween, and an exterior surface with a plurality of concave bumps and convex dimples formed thereon, wherein each of the plurality of concave bumps is adjacent to a first plurality of the plurality of convex dimples along the length of the mandrel and a second plurality of the plurality of convex dimples around a circumference of the mandrel and smoothly transitions into the adjacent dimples to form non-circular transverse cross-sectional geometries at all points along the length of the mandrel; and
a sleeve surrounding the mandrel and having an interior surface conforming to the plurality of concave and convex dimples on the mandrel such that the mandrel prevents torsional rotation of the mandrel relative to the sleeve and prevents axial translation of the mandrel relative to the sleeve.

13. The structural joint of claim 12 , wherein the mandrel is formed of one or more metallic materials.

14. The structural joint of claim 12 , wherein the mandrel is formed of one or more composite materials.

15. The structural joint of claim 12 , wherein the mandrel and the sleeve are formed of metallic or composite materials.

16. The structural joint of claim 12 , wherein the interior surface of the sleeve surrounding the mandrel includes bumps and dimples that closely conform to the plurality of concave bumps and convex dimples of the exterior surface of the mandrel.

17. The structural joint of claim 16 , wherein the mandrel and the sleeve are formed of metallic or composite materials.

18. The structural joint of claim 12 , wherein each of the plurality of concave bumps defines a crest having a radius which is equal to the radii of the crests of the other of the plurality of concave bumps.

19. The structural joint of claim 12 , wherein the elongate mandrel includes an axial bore having internal threads over at least a part of the length of the mandrel.

20. The structural joint of claim 19 , wherein the axial bore is attached to a component.

Assignees

• The Us Administrator Of The Nat Aeronautics And Space Adminstration
• Nasa

Inventors

• Wu K Chauncey
• Martin Robert A
• Stewart Brian K

Classifications

• F16D2001/102

  the torque is transmitted via polygon shaped connections · CPC title

• Y10T403/7073

  Cross-Sectional Technologies · mapped topic

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16C3/023

  made of several parts, e.g. by welding · CPC title

• F16C3/02

  Shafts; Axles · CPC title