Collapsible retainer

• US 8,936,420 B2
• Filed: 12/29/2011
• Issued: 01/20/2015
• Est. Priority Date: 12/31/2010
• Status: Active Grant

• Current Assignee: Illinois Tool Works Inc.
• Original Assignee: Illinois Tool Works Inc.
• Inventors: Scroggie, Derek, Osterland, Robert, Murawski, Robert A., Bozinovski, Michelle E.
• Primary Examiner(s): DELISLE, ROBERTA S
• Application Number:
  US13/997,678
• Publication Number:
  US 20130287518A1
• Time in Patent Office: 1,118 Days
• Field of Search: 411/32, 411/45, 411/78, 411/80, 411/80.1, 411/80.2
• US Class Current: 411/45
• CPC Class Codes: B23P 19/08 Machines for placing washers, circlips, or the like on bolts or other members
• CPC Class Codes: F16B 5/0607 joining sheets or plates to each other F16B5/0692, F16B21/082 take precedence
• CPC Class Codes: F16B 5/065 the plates being one on top of the other and distanced from each other, e.g. by using protrusions to keep contact and distance
• CPC Class Codes: Y10T 29/49954 Fastener deformed after application

Abstract

A press-in fastener adapted to join a first component to a second component. The fastener includes a proximal head and a distal base clip portion below the head. The base clip portion includes an axially displaceable post structure and a pair of opposing wings extending in upwardly angled relation away from the travel path defined by the post structure. Collapsible legs engage the wings in operative connection to the post structure. As the fastener is pressed inwardly, upon encountering resistance from the second component, the legs collapse in folded relation as the post structure travels axially between the wings.

Claims

1. A press-in fastener for joining a first component to a second component, said fastener comprising:

a head adapted to engage the first component; and

a base clip portion disposed below the head and adapted for insertion into an acceptance opening in the second component, the base clip portion including a pair of flexible wing elements and a post structure of substantially incompressible construction disposed along an axial travel path between the wing elements, the wing elements extending upwardly at acute angles relative to the post structure travel path, the post structure being operatively connected to the head such that linear movement of the head is translated to the post structure, at least one collapsible leg operatively connecting each of the wing elements to the post structure such that said at least one collapsible leg collapses into a folded condition upon application of axial compression as the head is pressed towards the second component and the post structure moves axially between the wing elements following insertion of the base clip portion into the acceptance opening.

2. The press-in fastener as recited in claim 1, wherein the fastener is of unitary molded polymer construction.

3. The press-in fastener as recited in claim 1, wherein each of the wing elements includes an outboard projecting shoulder stop adapted to blockingly engage an upper surface of the second component.

4. The press-in fastener as recited in claim 3, wherein each of the wing elements includes an undercut disposed below the shoulder stop adapted to engage a perimeter edge of the acceptance opening.

5. The press-in fastener as recited in claim 1, wherein each of the wing elements includes an inboard ledge or hooking arm adapted to engage an opposing projection extending away from the post structure as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

6. The press-in fastener as recited in claim 1, wherein a pair of ribs of dogleg configuration extends between the post structure and an overlying support platform disposed below the head, at least one of the ribs including an outwardly projecting nose having an outwardly angled lower surface adapted to slidingly engage an inboard surface of an opposing wing element as the head and support platform are pressed towards the second component following insertion of the base clip portion into the acceptance opening.

7. The press-in fastener as recited in claim 6, wherein the outwardly projecting nose includes an inwardly angled upper surface adapted to engage an inboard ledge of an opposing wing element as the head and support platform are pressed towards the second component following insertion of the base clip portion into the acceptance opening.

8. The press-in fastener as recited in claim 1, wherein a hook structure of dogleg configuration including a downwardly angled inboard hooking arm is disposed at a free end of each of the wing elements.

9. The press-in fastener as recited in claim 8, wherein the post structure includes a pair of opposing, outwardly projecting ears, and wherein each of the inboard hooking arms is adapted to latch over an opposing one of the outwardly projecting ears as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

10. The press-in fastener as recited in claim 1, wherein an overlying support platform is disposed below the head in overlying relation to the post structure, and wherein a pair of upwardly angled flexible arm elements extend away from opposing sides of the post structure, and wherein each of the wing elements includes an inboard ledge adapted to engage an opposing one of the flexible arm elements as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

11. The press-in fastener as recited in claim 10, wherein at least one collapsible leg extends between an upper portion of each wing element and the support platform.

12. The press-in fastener as recited in claim 11, wherein at least one collapsible leg includes a plurality of living hinges arranged in alternating in-board and out-board orientation along the collapsible leg such that the collapsible leg collapses upon application of axial compression as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

13. The press-in fastener as recited in claim 12, wherein the wing elements cooperatively form a distal cusp disposed below a molded-in bridge connection between the wing elements, and wherein a pair of spaced-apart detents projects upwardly away from the bridge connection, the post structure including a downwardly projecting distal tab portion sized and shaped for receipt between the detents when the post structure has moved axially between the wing elements following insertion of the base clip portion into the acceptance opening.

14. The press-in fastener as recited in claim 1, wherein each of the collapsible legs includes a plurality of living hinges arranged in alternating in-board and out-board orientation such that the leg collapses into an accordion folded condition upon application of axial compression as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

15. The press-in fastener as recited in claim 1, wherein at least one of the collapsible legs is free of living hinges.

16. A press-in fastener as recited in claim 1, wherein a collapsible leg extends between a lower portion of each wing element and a distal end of the post structure, the legs being separated by a longitudinal gap, each of the legs including a plurality of living hinges disposed along the length, the living hinges being arranged in alternating in-board and out-board orientations along the legs, wherein the legs have an axial compressive strength less than the post structure such that the legs collapse into an accordion folded condition preferentially to the post structure upon application of axial compression as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

17. The press-in fastener as recited in claim 1, wherein the collapsible legs include a first leg section that is articulable relative to a second leg section, wherein collapsation of the legs results in distal locations of the leg sections being located closer to one another than that which was the case prior to collapsation of the legs.

18. The press-in fastener as recited in claim 1, wherein the wings have a free end located at an end of the upwardly extension thereof.

19. A press-in fastener for joining a first component to a second component, said fastener comprising a unitary molded polymer structure including:

a head adapted to engage the first component;

a neck extending downwardly from the head, the neck having an effective diameter less than the head;

a support platform disposed below the neck, the support platform projecting outwardly away from the neck in transverse orientation to the head; and

a base clip portion disposed below the head and adapted for insertion into an acceptance opening in the second component, the base clip portion including a pair of flexible wing elements and a post structure disposed along an axial travel path between the wing elements, the wing elements extending upwardly at acute angles relative to the post structure travel path, the post structure extending downwardly from the support platform in operative connection to the head such that linear movement of the head is translated to the post structure, at least one collapsible leg extending between an upper portion of each wing element and the support platform to operatively connect each of the wing elements to the post structure such that said at least one collapsible leg collapses into a folded condition upon application of axial compression as the head is pressed towards the second component and the post structure moves axially between the wing elements following insertion of the base clip portion into the acceptance opening, wherein a pair of upwardly angled flexible arm elements extend away from opposing sides of the post structure, and wherein each of the wing elements includes an inboard ledge adapted to engage an opposing one of the flexible arm elements as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening and wherein the wing elements cooperatively form a distal cusp disposed below a molded-in bridge connection between the wing elements with a pair of spaced-apart detents projects upwardly away from the bridge connection, the post structure including a downwardly projecting distal tab portion sized and shaped for receipt between the detents when the post structure has moved axially between the wing elements.

20. A press-in fastener as recited in claim 19, wherein each collapsible leg includes a plurality of living hinges arranged in alternating in-board and out-board orientation along the collapsible leg such that the collapsible leg collapses upon application of axial compression as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

21. A press-in fastener as recited in claim 19, wherein each of the wing elements includes an outwardly projecting nose disposed below an intersection with the corresponding collapsible leg.

22. The press-in fastener as recited in claim 19, wherein the collapsible legs include a first leg section that is articulable relative to a second leg section, wherein collapsation of the legs results in distal locations of the leg sections being located closer to one another than that which was the case prior to collapsation of the legs.

23. The press-in fastener as recited in claim 19, wherein the wings have a free end located at an end of the upwardly extension thereof.

24. A method of joining a first component to a second component, the method comprising the steps of:

providing a press-in fastener, said fastener comprising a head adapted to engage the first component and a base clip portion disposed below the head and adapted for insertion into an acceptance opening in the second component, the base clip portion including a pair of flexible wing elements and a post structure of substantially incompressible construction disposed along an axial travel path between the wing elements, the wing elements extending upwardly at acute angles relative to the post structure travel path, the post structure being operatively connected to the head such that linear movement of the head is translated to the post structure, at least one collapsible leg operatively connecting each of the wing elements to the post structure such that said at least one collapsible leg collapses into a folded condition upon application of axial compression as the head is pressed towards the second component and the post structure moves axially between the wing elements following insertion of the base clip portion into the acceptance opening; and

pressing the base clip portion into an acceptance opening in the second component, such that the collapsible legs collapse into a folded condition preferentially to the post structure upon application of axial compression as the head is pressed towards the second component following insertion of the base clip portion into the acceptance opening.

25. The method of claim 24, wherein the collapsible legs include a first leg section that is articulable relative to a second leg section, wherein collapsation of the legs results in distal locations of the leg sections being located closer to one another than that which was the case prior to collapsation of the legs.

26. The method of claim 24, wherein the wings have a free end located at an end of the upwardly extension thereof.