IP Library › Granted Patent US 11,271,344
Granted Patent B2
US 11,271,344 · App. 16/789,769 · Granted Mar 8, 2022

Strain relief apparatus for wire harness assembly

Inventor: Michael Furlong (Sharpsburg, GA)
Assignee: Delta Air Lines, Inc.
H01R13/5825H01R13/5804H01R13/6271
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Quick Facts
Patent No.
US 11,271,344
App. No.
16/789,769
Granted
Mar 8, 2022
Kind
B2
Abstract

A wire connector strain relief apparatus is provided herein. The wire connector strain relief apparatus includes a body having a generally U-shaped cross-section, a first end, and a second end. The first end of the body is configured to receive a wire harness that includes one or more wires to be, or already, connected to an electrical connector. The second end of the body includes one or more structural features configured to engage with one or more structural features of an external surface of the electrical connector to attach to the electrical connector and minimize relative movement between the wire harness and the electrical connector.

Claims (32)

1. A wire connector strain relief apparatus comprising:

a body having a generally U-shaped cross-section, a first end, and a second end, wherein:

the first end of the body is configured to receive a wire harness that includes one or more wires to be, or already, connected to an electrical connector; and

the second end of the body includes one or more structural features configured to engage with one or more structural features of an external surface of the electrical connector to attach to the electrical connector and minimize relative movement between the wire harness and the electrical connector, wherein the one or more structural features of the second end of the body include a locating groove that extends along a substantially horizontal bottom of the body from a first substantially vertical side of the body to a second substantially vertical side of the body, and wherein the one or more structural features of the second end of the body further include a first depressed portion of an inner surface of the first substantially vertical side of the body, wherein the first depressed portion defines a first hole on the substantially horizontal bottom of the body that is complementary to, and configured to mate with, a first surface feature of the electrical connector.

2. The wire connector strain relief apparatus of claim 1 , wherein the one or more structural features of the second end of the body further include an inclined surface and a ledge, and the one or more structural features of the external surface of the electrical connector include a surface feature of the electrical connector that slides over the inclined surface and becomes lodged beneath the ledge, and wherein the inclined surface and the ledge are configured to snap fit to the one or more structural features of the external surface of the electrical connector.

3. The wire connector strain relief apparatus of claim 1 , wherein the one or more structural features of the second end of the body further include a locating rib that is sized and positioned in the second end of the body so as to engage with a surface feature of the electrical connector.

4. The wire connector strain relief apparatus of claim 1 , wherein the first end of the body includes a slot configured to accommodate a securing element to secure to the wire harness.

5. The wire connector strain relief apparatus of claim 1 , wherein the body is made of an aircraft-approved material.

6. The wire connector strain relief apparatus of claim 1 , wherein the one or more structural features of the second end of the body further include a second depressed portion of an inner surface of a second substantially vertical side of the body.

7. The wire connector strain relief apparatus of claim 6 , wherein the second depressed portion defines a second hole on the substantially horizontal bottom of the body that is complementary to, and configured to mate with, a second surface feature of the electrical connector.

8. A wire connector strain relief system comprising:

an electrical connector;

a wire harness that includes one or more wires to be, or already, connected to the electrical connector; and

a wire connector strain relief apparatus including a body having a generally U-shaped cross-section, a first end, and a second end, wherein the first end of the body is configured to receive the wire harness, and wherein the second end of the body includes one or more structural features configured to engage with one or more structural features of an external surface of the electrical connector to attach to the electrical connector and minimize relative movement between the wire harness and the electrical connector, wherein the one or more structural features of the second end of the body include a locating groove that extends along a substantially horizontal bottom of the body from a first substantially vertical side of the body to a second substantially vertical side of the body, and wherein the one or more structural features of the second end of the body further include a first depressed portion of an inner surface of the first substantially vertical side of the body, wherein the first depressed portion defines a first hole on the substantially horizontal bottom of the body that is complementary to, and configured to mate with, a first surface feature of the electrical connector.

9. The wire connector strain relief system of claim 8 , wherein the one or more structural features of the second end of the body further include an inclined surface and a ledge, and the one or more structural features of the external surface of the electrical connector include a surface feature of the electrical connector that slides over the inclined surface and becomes lodged beneath the ledge, and wherein the inclined surface and the ledge are configured to snap fit to the one or more structural features of the external surface of the electrical connector.

10. The wire connector strain relief system of claim 8 , wherein the one or more structural features of the second end of the body further include a locating rib that is sized and positioned in the second end of the body so as to engage with a surface feature of the electrical connector.

11. The wire connector strain relief system of claim 8 , wherein the first end of the body includes a slot configured to accommodate a securing element to secure to the wire harness.

12. The wire connector strain relief system of claim 8 , wherein the body is made of an aircraft-approved material.

13. The wire connector strain relief system of claim 8 , wherein the one or more structural features of the second end of the body further include a second depressed portion of an inner surface of the second substantially vertical side of the body.

14. The wire connector strain relief system of claim 13 , wherein the second depressed portion defines a second hole on the substantially horizontal bottom of the body that is complementary to, and configured to mate with, a second surface feature of the electrical connector.

15. A method for wire connector strain relief comprising:

receiving, at a first end of a body having a generally U-shaped cross-section, a wire harness that includes one or more wires to be, or already, connected to an electrical connector; and

engaging, by one or more structural features of a second end of the body, with one or more structural features of an external surface of the electrical connector to attach to the electrical connector and minimize relative movement between the wire harness and the electrical connector, wherein the one or more structural features of the second end of the body include a locating groove that extends along a substantially horizontal bottom of the body from a first substantially vertical side of the body to a second substantially vertical side of the body, wherein the engaging includes mating, to a first surface feature of the electrical connector, a first hole on the substantially horizontal bottom of the body that is complementary to a first surface feature of the electrical connector, wherein the first hole is defined by a first depressed portion of an inner surface of the first substantially vertical side of the body.

16. The method for wire connector strain relief of claim 15 , wherein engaging includes:

snap fitting an inclined surface and a ledge of the second end of the body to a surface feature of the electrical connector that slides over the inclined surface and becomes lodged beneath the ledge of the electrical connector.

17. The method for wire connector strain relief of claim 15 , wherein engaging includes:

engaging a locating rib of the second end of the body with a surface feature of the electrical connector.

18. The method for wire connector strain relief of claim 15 , wherein receiving the wire harness includes:

using a securing element, securing the wire harness to a slot of the first end of the body.

19. The method for wire connector strain relief of claim 15 , wherein engaging further includes:

mating, to a second surface feature of the electrical connector, a second hole on the substantially horizontal bottom of the body that is complementary to a second surface feature of the electrical connector.

20. The method for wire connector strain relief of claim 19 , wherein the second hole is defined by a second depressed portion of an inner surface of the second substantially vertical side of the body.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 13, 2020
From: FURLONG, MICHAEL
To: DELTA AIR LINES, INC.
Reel/Frame 051811/0289 →
Continuity (2)
Provisional Application 62947771 · Dec 13, 2019
Related Publication 20210184395A1 · Jun 17, 2021