Backplane for receiving electrical components

• US 9,823,712 B2
• Filed: 03/18/2014
• Issued: 11/21/2017
• Est. Priority Date: 03/18/2014
• Status: Active Grant

• Current Assignee: JP Morgan Chase Bank, N.A. (JP Morgan Chase & Co)
• Original Assignee: Western Digital Technologies Incorporated (Western Digital Corporation)
• Inventors: Huang, Lidu, Hirano, Toshiki, Wilke, Jeffrey, Ou-Yang, Jin Hui, Bell, Michael
• Primary Examiner(s): Nguyen, Hoa C
• Assistant Examiner(s): Tso, Stanley
• Application Number:
  US14/218,117
• Publication Number:
  US 20150268701A1
• Time in Patent Office: 1,344 Days
• Field of Search: 36167901, 36167902, 361683, 439 55, 439 77, 439384
• CPC Class Codes: G06F 1/187 Mounting of fixed and removable disk drives

Abstract

A backplane configured to receive electrical components is provided. The backplane in one example includes a substrate comprising an at least partially flexible material, a plurality of backplane traces formed as part of the substrate, at least one connector island formed in the substrate, with the at least one connector island located in an opening in the substrate and configured to receive at least one mating electrical component, and one or more spring elements bridging between the at least one connector island and the substrate, with traces of the plurality of backplane traces extending over the one or more spring elements to the at least one connector island and with the one or more spring elements allowing the at least one connector island to flex with respect to the substrate and absorb vibrations.

Claims

1. An apparatus comprising a backplane configured to receive electrical components, the backplane comprising:

a substrate comprising an at least partially flexible material;

a plurality of backplane traces formed as part of the substrate;

a first plurality of connector islands aligned along a first axis and configured to receive a respective mating electrical component;

a second plurality of connector islands aligned along a second axis parallel with the first axis and configured to receive a respective mating electrical component;

a first plurality of spring elements extending across the second axis to connect the first plurality of connector islands to the substrate, wherein;

traces of the plurality of backplane traces extend over the first plurality of spring elements to the first plurality of connector islands; and

the first plurality of spring elements allows the first plurality of connector islands to flex with respect to the substrate and absorb vibrations; and

a second plurality of spring elements extending across the first axis to connect the second plurality of connector islands to the substrate, wherein;

traces of the plurality of backplane traces extend over the second plurality of spring elements to the second plurality of connector islands; and

with the second plurality of spring elements allows the second plurality of connector islands to flex with respect to the substrate and absorb vibrations.

2. The apparatus of claim 1, wherein each connector island is configured to move independently of other connector islands.

3. The apparatus of claim 1, wherein the backplane is configured to receive multiple rows and columns of electrical components.

4. The apparatus of claim 1, further comprising a retainer post formed of an at least partially flexible material, wherein the retainer post comprises:

a neck portion configured to fit to a connector bore of at least one of the connector islands of the first and second pluralities of connector islands; and

a shaft portion configured to;

receive a corresponding bore of an electrical component connector; and

hold the electrical component connector at a predetermined position.

5. The apparatus of claim 1, wherein each connector island of the first plurality of connector islands is offset from each connector island of the second plurality of connector islands along a direction parallel with the first axis.

6. The apparatus of claim 1, wherein:

each spring element of the first plurality of spring elements comprises two spring elements;

the two spring elements form a substantially flat hourglass shape including two centrally-extending loop portions; and

the two centrally-extending loop portions have a substantially common loop axis.

7. The apparatus of claim 1, wherein:

each spring element of the first plurality of spring elements comprises two spring elements;

the two spring elements form a substantially flat hourglass shape including two centrally-extending loop portions; and

the two centrally-extending loop portions have different loop axes.

8. The apparatus of claim 1, wherein the backplane further comprises a cut-out slot located at a junction of a spring element of the first plurality of spring elements and the substrate.

9. The apparatus of claim 1, further comprising one or more damper elements positioned underneath the backplane and configured to absorb deflections of the backplane with respect to a surface underneath the backplane associated with a shell into which the backplane is mounted.

10. The apparatus of claim 1, further comprising one or more limiter elements positioned underneath the backplane and configured to:

limit deflection amplitudes of spring elements of the first plurality of spring elements to prevent displacement of the spring elements of the first plurality of spring elements beyond a predetermined displacement; and

limit deflection amplitudes of the backplane.

11. An apparatus comprising a backplane configured to receive electrical components, the backplane comprising:

a substrate comprising an at least partially flexible material;

a plurality of backplane traces formed as part of the substrate;

a series of alternating connector islands formed along two substantially parallel axes extending substantially lengthwise on the substrate, wherein;

each connector island is able to move independently of other connector islands;

pairs of connector islands of the series of connector islands located in openings in the substrate and configured to receive one or more mating electrical components; and

a first connector island of a first axis is laterally spaced from an adjacent second connector island of a second axis along the first axis;

a plurality of spring elements, each spring element extending across one of the two substantially parallel axes to connect a respective connector island formed along the other of the two substantially parallel axes to the substrate, wherein;

traces of the plurality of backplane traces extend over the plurality of spring elements to the particular connector island; and

the plurality of spring elements allows the particular connector island to flex with respect to the substrate and absorb vibrations; and

one or more limiter elements positioned underneath the backplane and configured to limit deflection amplitudes of the connector islands to prevent displacement of the plurality of spring elements beyond a predetermined displacement.

12. The apparatus of claim 11, further comprising a retainer post formed of an at least partially flexible material, wherein the retainer post comprises:

a neck portion configured to fit to a connector bore of at least one of the connector islands of the series of alternating connector islands; and

a shaft portion configured to;

receive a corresponding bore of an electrical component connector; and

hold the electrical component connector at a predetermined position.

13. The apparatus of claim 11, wherein:

each spring element of the plurality of spring elements comprises two spring elements;

the two spring elements form a substantially flat hourglass shape including two centrally-extending loop portions; and

the two centrally-extending loop portions have a substantially common loop axis.

14. The apparatus of claim 11, wherein:

each spring element of the plurality of spring elements comprises two spring elements;

the two spring elements form a substantially flat hourglass shape including two centrally-extending loop portions; and

the two centrally-extending loop portions have different loop axes.

15. The apparatus of claim 11, wherein the backplane further comprises a cut-out slot located at a junction of one of the spring elements of the plurality of spring elements and the substrate.

16. The apparatus of claim 11, further comprising one or more damper elements positioned underneath the backplane and configured to absorb deflections of the backplane with respect to a surface underneath the backplane associated with a shell into which the backplane is mounted.

17. The apparatus of claim 11, wherein the one or more limiter elements are further configured to limit deflection amplitudes of the backplane.

18. A method of absorbing vibrations in one or more electrical components installed to a backplane, comprising:

in the backplane, receiving two or more electrical components on two or more connector components affixed to two or more corresponding connector islands formed in a substrate of the backplane;

in the backplane, allowing a first connector island coupled to a first electrical component to;

independently deflect with respect to the substrate; and

absorb vibrations generated by the first electrical component;

in the backplane, allowing a second connector island coupled to a second electrical component to;

independently deflect with respect to the substrate; and

not receive vibrations present in the substrate;

allowing one or more limiter projections to limit deflection amplitudes of the connector islands to prevent displacement of the connector islands beyond a predetermined displacement; and

allowing one or more fasteners to;

allow displacement of the connector islands toward the one or more limiter projections; and

prevent displacement of the connector islands beyond a predetermined displacement away from the one or more limiter projections.

19. The method of claim 18, further comprising allowing one or more damper elements located below the substrate to absorb deflections of the backplane with respect to a surface underneath the backplane associated with a shell into which the backplane is mounted.

20. The method of claim 18, further comprising allowing the one or more limiter projections to limit deflection amplitudes of the backplane.