Side-release buckle
09730495 · 2017-08-15
Assignee
Inventors
Cpc classification
A44B11/266
HUMAN NECESSITIES
International classification
Abstract
A buckle has two identical components relatively shiftable along a central axis into and out of an assembled state, with an interlocking mechanism for releasably coupling the components in their assembled state. The interlocking mechanism includes a wing on each of the components. The wings have opposed mutually spaced resilient panels defining passages therebetween leading to aligned locking surfaces. Each component also has a prong with oppositely protruding posts and first and second cam surfaces. The first cam surfaces are configured and arranged to urge the panels apart and thereby accommodate insertion of the prongs into the passages to locked positions at which the posts are in snap engagement with the locking surfaces. The second cam surfaces are configured and arranged to act in response to flexure of the prongs towards the central axis to urge the panels apart and to thereby accommodate withdrawal of the prong from the passages.
Claims
1. A buckle comprising two components relatively shiftable along a central axis into and out of an assembled state, with one wing on each of said components, said wings having opposed mutually spaced resilient panels defining passages therebetween leading to aligned locking surfaces on said panels, and at least one resilient prong on each of said components, said prongs having oppositely protruding posts and first and second cam surfaces, said first cam surfaces being configured and arranged to urge said panels apart and thereby accommodate insertion of said prongs into said passages to locked positions at which said posts are in snap engagement with said locking surfaces, said second cam surfaces being configured and arranged to act in response to flexure of said prongs towards said central axis to urge said panels apart and to thereby accommodate withdrawal of said prongs from said passages by being pressed inwardly towards the central axis.
2. The buckle of claim 1 wherein a pair of said wings are provided on said one component, and a pair of said prongs are provided on said other component.
3. The buckle of claim 2 wherein said pair of wings are separated by a centrally projecting nose, and wherein said pair of prongs are separated by a U-shaped recess configured and dimensioned to receive said nose.
4. The buckle of claim 1 or 2 wherein said panels are provided with openings for receiving said posts, and wherein said locking surfaces are defined by edges of said openings.
5. The buckle of claim 1 where said locking surfaces are defined by peripheral edges of said panels.
6. The buckle of claim 1 wherein said second cam surfaces are provided on said posts.
7. The buckle of claim 1 wherein said second cam surfaces are provided on said prongs.
8. The buckle of claim 1 wherein said first and second components are identical.
9. A buckle comprising two identical components relatively shiftable along a central axis into and out of an assembled state, with a wing on each of said components, said wings having opposed mutually spaced resilient panels defining passages therebetween leading to aligned locking surfaces on said panels, and a resilient prong on each of said components, said prongs having oppositely protruding posts and first and second cam surfaces, said first cam surfaces being configured and arranged to urge said panels apart and thereby accommodate insertion of said prongs into said passages to locked positions at which said posts are in snap engagement with said locking surfaces, said second cam surfaces being configured and arranged to act in response to flexure of said prongs towards said central axis to urge said panels apart and to thereby accommodate withdrawal of said prongs from said passages by being pressed inwardly towards the central axis.
10. A buckle comprising two identical components relatively shiftable along a central axis into and out of an assembled state, with a wing on each of said components, said wings having opposed mutually spaced resilient panels defining passages therebetween leading to aligned back edges of said panels, and a resilient prong on each of said components, said prongs having oppositely protruding posts and first and second cam surfaces, said first cam surfaces being configured and arranged to urge said panels apart and thereby accommodate insertion of said prongs into said passages to locked positions at which said posts are in snap engagement with the back edges of said panels, said second cam surfaces being configured and arranged to act in response to flexure of said prongs towards said central axis to urge said panels apart and to thereby accommodate withdrawal of said prongs from said passages by being pressed inwardly towards the central axis.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
(12)
(13)
(14)
DETAILED DESCRIPTION
(15) With reference initially to
(16) An interlocking means serves to releasably couple the components 10a, 10b in the assembled state shown in
(17) The interlocking means of the buckle 10 further comprises a resilient prong 18 on each buckle component 10a, 10b. As can be best seen in
(18) In order to disassemble the buckle components 10a, 10b, the resilient prongs 18 are pressed inwardly towards axis A. As depicted in
(19) Laterally spaced longitudinally projecting guide bars 26 with sides configured to provide tongue and groove interfaces 28 (best seen in
(20) With reference to
(21) An interlocking means again serves to releasably couple the two buckle components 30a, 30b in the assembled state. The interlocking means of buckle 30 comprises a pair of laterally projecting wings 32 on component 30a and a pair of forwardly projecting resilient prongs 34 on component 30b.
(22) The wings 32 each have mutually spaced panels 32a, 32b defining passages 36 therebetween. Passages 36 lead to aligned locking surfaces, which in this case are the peripheral edges of apertures 38 in the wing panels 32a, 32b.
(23) The prongs 34 have oppositely projecting posts 40 and first and second cam surfaces 42, 44. With reference to
(24) In order to disassemble the buckle components 30a, 30b, the resilient prongs 34 are pressed inwardly towards axis A. This causes the second cam surfaces 44 to spread the wing panels 32a, 32b apart, which relieves the engagement of the posts 40 in the panel apertures 38, thereby allowing the posts 40 to be withdrawn from the passages 36.
(25) Buckle component 30a may advantageously be provided with a centrally projecting nose 46 configured to be received in a centrally located U-shaped recess 48 defined by laterally spaced guide bars 50 on buckle component 30b. A peripheral groove 52 on nose 46 coacts with a peripheral rib 54 extending around the interior of recess 48 to locate and guide the buckle components during assembly and disassembly.