Energy absorbing link

Patent metadata

Field	Value
Publication number	US-9500249-B2
Application number	US-201514641586-A
Country	US
Kind code	B2
Filing date	Mar 9, 2015
Priority date	Mar 9, 2015
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

An apparatus and method for a composite structural aircraft transmission support link having an integral energy-absorbing feature is disclosed. The link is a two-force member that can carry structural loads up an ultimate load. When loaded beyond ultimate load the design allows sections of the link to fail in a controlled and progressive manner, so that energy is absorbed over a defined stroking distance.

First claim

What is claimed is:

1. A two-force member energy-absorbing link structure comprising:
an elongated structural member having first and second opposing ends and a lengthwise extending central axis, wherein at least the first and second opposing ends of the elongated structural member are constructed of a primary material having a strength characteristic sufficient to link together two structures;
a thru-hole extending substantially orthogonally with respect to the central axis and through the first opposing end; and
a section of the elongated structural member constructed of secondary material having a lesser strength characteristic than the strength characteristic of the primary material, said section extending a lengthwise distance substantially along a direction that the lengthwise extending central axis extends, and said section extending from a location proximate and adjacent the thru-hole,
wherein the section is configured to deform when exposed to a predetermined axial compression load, and wherein a length of the elongated structural member remains substantially the same before and after the section deforms.

2. The two-force member energy-absorbing link structure as recited in claim 1 , wherein the elongated structural member is a tubular elongated member.

3. The two-force member energy-absorbing link structure as recited in claim 1 , wherein the first opposing end has a u-shaped clevis structure with opposing first and second prong members forming the u-shaped clevis structure.

4. The two-force member energy-absorbing link structure as recited in claim 3 , wherein the thru-hole extends through the first prong member.

5. The two-force member energy-absorbing link structure as recited in claim 1 , wherein the section of the elongated structural member constructed of a secondary material is an elongated slot extending a lengthwise distance.

6. The two-force member energy-absorbing link structure as recited in claim 5 , wherein the section of the elongated structural member is a weakened region to allow the section to deform when the predetermined axial compression load is applied to the elongated structural member in the direction that the lengthwise extending central axis extends.

7. The two-force member energy-absorbing link structure as recited in claim 6 , wherein the section includes ply-drops proximate the thru-hole to initiate crushing of the secondary material to reduce an initial load spike.

8. The two-force member energy-absorbing link structure as recited in claim 6 , wherein the secondary material is recessed with respect to the primary material, and wherein the secondary material includes lengthwise slits extending at least partially in the direction that the lengthwise extending central axis extends.

9. The two-force member energy-absorbing link structure as recited in claim 1 , wherein the thru-hole is configured to have a fastening member positioned therein, and wherein the fastening member is configured to slide into and deform the section in response to the axial compression load.

10. A two-force member energy-absorbing link structure comprising:
an elongated tubular member having first and second opposing ends and a lengthwise extending central axis, wherein the elongated tubular member is constructed of a primary material having a primary material thickness and has a strength characteristic sufficient to link together two structures;
a thru-hole extending substantially orthogonally with respect to the central axis and through the first opposing end; and
a section of the elongated structural member constructed of secondary material having a secondary material thickness with a thickness less than the primary material thickness, and having a lesser strength characteristic than the strength characteristic of the primary material, and said section extending a lengthwise distance substantially along a direction that the lengthwise extending central axis extends and said section extends from a point of the material proximate and adjacent the through hole,
wherein the section is configured to deform when exposed to a predetermined axial compression load, and wherein a length of the elongated structural member remains substantially the same before and after the section deforms.

11. The two-force member energy-absorbing link structure as recited in claim 10 , wherein one or more of the first and second opposing distal ends have a u-shaped clevis structure with opposing first and second prong members forming the u-shaped clevis structure.

12. The two-force member energy-absorbing link structure as recited in claim 11 , wherein the thru-hole extends through one or more of the first and second prong members.

13. The two-force member energy-absorbing link structure as recited in claim 10 , wherein the section of the elongated structural member constructed of a secondary material is an elongated slot extending a lengthwise distance.

14. The two-force member energy-absorbing link structure as recited in claim 13 , wherein the section of the elongated tubular member is formed in the primary material as a weakened region of the elongated tubular member to allow the section to deform when the predetermined axial compression load is applied to the elongated tubular member in the direction that the lengthwise extending central axis extends.

15. The two-force member energy-absorbing link structure as recited in claim 14 , wherein the section is formed with ply-drops proximate the thru-hole to act as a trigger to initiate crushing of the secondary material to reduce an initial load spike.

16. The two-force member energy-absorbing link structure as recited in claim 14 , wherein the section is formed having lengthwise slits extending at least partially in the direction that the lengthwise extending central axis extends.

17. A two-force member energy-absorbing link structure comprising:
an elongated structural member having first and second opposing ends and a lengthwise extending central axis, wherein at least the first and second opposing ends of the elongated structural member are constructed having a primary material thickness and having a strength characteristic sufficient to link together two structures;
a thru-hole extending substantially orthogonally with respect to the central axis and through the first opposing end; and
a recessed cutaway slot section of the elongated structural member having a lesser thickness and lesser strength characteristic than the strength characteristic of the primary material, said section extending a lengthwise distance substantially along a direction that the lengthwise extending central axis extends, and said section extending from a location of the material proximate and adjacent the thru-hole,
wherein the recessed cutaway slot section is configured to deform when exposed to a predetermined axial load, and wherein a length of the elongated structural member remains substantially the same before and after the recessed cutaway slot section deforms.

18. The two-force member energy-absorbing link structure as recited in claim 17 , wherein the first opposing distal end has a u-shaped clevis structure with opposing first and second prong members forming the u-shaped clevis structure.

19. The two-force member energy-absorbing link structure as recited in claim 17 , wherein the recessed cutaway slot section of the elongated structural member is formed as a weakened region of the elongated structural member to allow the recessed cutaway slot section of the elongated structural member to deform when the predeter

Assignees

• Boeing Co

Inventors

• Ludin Douglas R
• Stauffer Matthew S
• Bolukbasi Akif O
• Birchette Terrence S

Classifications

• F16F7/12 Primary

  using plastic deformation of members {(F16F9/30 takes precedence; yieldable means for mounting bumpers on vehicles B60R19/26; yieldable or collapsible steering columns B62D1/192)} · CPC title