Continuously adaptive fastener clip
View Patent ↗A fastener clip includes a base plate and a first and second pair of laterally offset legs extending from the base plate. At least one first wing extends from the first pair of laterally offset legs. The at least one first wing has an engagement region. At least one second wing extending from the second pair of laterally offset legs. The at least one second wing has an engagement region, such that a distance between the engagement regions and the base plate is operative to vary continuously according to a slot thickness. The fastener clip is operative for insertion into the slot defined in a first engagement structure, such as a vehicle chassis.
1. A fastener clip for insertion into a slot of a frame, comprising:
a base plate;
a first pair of laterally offset legs extending from the base plate;
at least one first wing extending from the first pair of laterally offset legs, the at least one first wing having an engagement region, the engagement region is spaced from the base plate by a distance and the distance is capable of varying in response to a slot thickness
a second pair of laterally offset legs extending from the base plate;
at least one second wing extending from the second pair of laterally offset legs,
the at least one second wing having an engagement region, the engagement region is spaced from the base plate by a distance and the distance is capable of varying in response to a slot thickness, and
end brackets at opposite ends of the base plate, wherein the base plate is operative to bend about the end brackets in response to an insertion force applied to the base plate such that the legs cause the wings to increase the distance between the engagement regions and the base plate until at least one of the engagement regions engage the slot.
2. The fastener clip of claim 1 , wherein at least one of the engagement regions further comprises an engagement tab operative to engage at least a portion of the slot.
3. The fastener clip of claim 2 , wherein the engagement tab is a protrusion in a non-planar orientation relative to an end of the wings.
4. The fastener clip of claim 2 , wherein the engagement tab is at least one of: rounded, bulbous, stepped, angled, and depressed.
5. The fastener clip of claim 1 , further comprising at least two threading projections protruding from the base plate, such that the at least two threading projections point to each other to create a frictional opening.
6. The fastener clip of claim 1 , wherein a force on the base plate imparts a torque on the at least one first wing and an opposite torque applied on the at least one second wing.
7. The fastener clip of claim 1 , further comprising a coating on the fastener clip made of at least one of: rubber, plastisol, plastic, acetal, polyacetal, polyoxymethylene, nylon, fiberglass and carbon fiber.
8. The fastener clip of claim 1 , wherein at least one of: the legs and the wings, is tapered.
9. A fastener assembly comprising:
a body panel comprising a mounting member;
a fastener clip for insertion into a slot of a frame, comprising:
a base plate coupled to the mounting member;
a first pair of laterally offset legs extending from the base plate;
at least one first wing extending from the first pair of laterally offset legs,
the at least one first wing having an engagement region, the engagement region is spaced from the base plate by a distance and the distance is capable of varying in response to a slot thickness;
a second pair of laterally offset legs extending from the base plate;
at least one second wing extending from the second pair of laterally offset legs,
the at least one second wing having an engagement region, the engagement region is spaced from the base plate by a distance and the distance is capable of varying in response to a slot thickness,
a first locking tab on the first pair of laterally offset legs at an end opposed the base plate;
a second locking tab on the second pair of laterally offset legs at an end opposed the base plate; and
wherein the base plate is operative to bend about end brackets in response to an insertion force applied to the base plate such that the legs cause the wings to increase the distance between the engagement regions and the base plate until at least one of the engagement regions engage the slot.
10. The fastener assembly of claim 9 , wherein at least one of the engagement regions further comprises an engagement tab operative to engage at least a portion of the slot.
11. The fastener assembly of claim 10 , wherein the engagement tab is a protrusion in a non-planar orientation relative to an end of the wings.
12. The fastener assembly of claim 9 , further comprising at least two threading projections protruding from the base plate, such that the at least two threading projections point to each other to create a frictional opening and to engage a fastener also engaged to the mounting member.
13. The fastener assembly of claim 9 , wherein a force on the base plate imparts a torque on the at least one first wing and an opposite torque applied on the at least one second wing.
14. A vehicle comprising:
a vehicle chassis having a slot;
a body panel including a mounting member;
a fastener clip for insertion into the slot comprising:
a base plate coupled to the mounting member;
a first pair of laterally offset legs extending from the base plate;
at least one first wing extending from the first pair of laterally offset legs,
the at least one first wing having an engagement region, the engagement region is spaced from the base plate by a distance and the distance is capable of varying in response to a slot thickness;
a second pair of laterally offset legs extending from the base plate;
at least one second wing extending from the second pair of laterally offset legs,
the at least one second wing having an engagement region, the engagement region is spaced from the base plate by a distance and the distance is capable of varying in response to a slot thickness, and
end brackets at opposite ends of the base plate, wherein the base plate is operative to bend about the end brackets in response to an insertion force applied to the base plate such that the legs cause the wings to increase the distance between the engagement regions and the base plate until at least one of the engagement regions engage the slot.
15. The vehicle of claim 14 , wherein at least one of the engagement regions further comprises an engagement tab operative to engage at least a portion of the slot.
16. The vehicle of claim 15 , wherein the engagement tab is a protrusion in a non-planar orientation relative to an end of the wings.
17. The vehicle of claim 14 further comprising:
a first locking tabs on the first pair of laterally offset legs at an end opposed the base plate; and
a second locking tabs on the second pair of laterally offset legs at an end opposed the base plate.