Thrust bearing assembly for hinge structure

• US 4,996,739 A
• Filed: 11/06/1989
• Issued: 03/05/1991
• Est. Priority Date: 11/06/1989
• Status: Expired due to Term

• Current Assignee: Austin R. Baer
• Original Assignee: Austin R. Baer
• Inventors: Baer, Austin R.
• Primary Examiner(s): Seidel, Richard K.
• Assistant Examiner(s): Cuda, Carmine
• Application Number:
  US07/432,573
• Time in Patent Office: 484 Days
• Field of Search: 16/354, 16/273, 16/380, 16/DIG. 27, 384/420, 384/906
• US Class Current: 16/354
• CPC Class Codes: E05D 1/04 with guide members shaped as circular arcs
• CPC Class Codes: E05D 3/122 Gear hinges
• CPC Class Codes: E05Y 2201/71 Toothed gearing
• CPC Class Codes: Y10S 384/906 Antirotation key

Abstract

A thrust bearing assembly for a hinge structure having two geared hinge members and a clamp member. The geared hinge members are maintained in rotatable, intermeshing relation along their adjacent longitudinally extending edges by the clamp members to permit smooth and uniform movement of the hinge structure. The thrust bearing assembly of the present invention includes a pair of non-metallic interconnected inserts arranged in side-by-side order to extend laterally across and inhibit relative longitudinal movements between the hinge members. The interconnected inserts are configured to facilitate their insertion in and removal from the hinge structure while maintaining the hinge members in mesh.

Claims

1. A thrust bearing assembly for a hinge structure including two geared hinge members and a clamp member, the geared hinged members being in intermeshing relation when the hinge structure is assembled and are longitudinally movable relative to each other with the clamp member maintaining the geared hinge members in mesh as they rotate, said thrust bearing assembly comprising:

a pair of interengaging inserts removably disposed in adjacent longitudinal co-extensive recesses defined along adjacent longitudinal edges of each hinge member and extending laterally across the hinge members to inhibit their longitudinal movement relative to each other, said inserts being configured to inhibit longitudinal movements relative to each other when disposed in the recesses of the hinge members while permitting said inserts to be rotationally moved relative to each other to facilitate removal of the thrust bearing assembly without requiring disassembly of the hinge members of the hinge structure.

2. The thrust bearing assembly according to claim 1 wherein said inserts slidably interengage with each other along adjacent longitudinal edges, with said longitudinal edges of said inserts having complementary profiles which allow the inserts to rotationally move relative to each other.

3. The thrust bearing assembly according to claim 1 wherein said inserts have a tongue-and-groove configuration defined along adjacent longitudinal edges to permit slidable interengagement and inhibit longitudinal movements of the inserts relative to each other.

4. The thrust bearing assembly according to claim 1 wherein each of said inserts are configured to define a longitudinally extending open-sided channel which accommodates an inwardly turned end of said clamp member, the open side of the channel permitting removal of the insert from the longitudinally extending recess defined by the hinge members upon manipulation of the inserts relative to each other.

5. The thrust bearing assembly according to claim 1 wherein said pair of inserts define co-extensive upper and lower bearing surfaces which slidably contact upper and lower surfaces of the recesses defined by each hinge member.

6. The thrust bearing assembly according to claim 1 wherein said thrust bearing assembly further includes means for inhibiting inadvertent movement of the inserts relative to each other.

7. The thrust bearing assembly according to claim 6 wherein said means for inhibiting inadvertent movement of the inserts includes a lateral projection provided on one insert to extend across and be received in releasable locking relation with a laterally extending groove defined on an adjacent insert to readily allow operator access thereto.

8. The thrust bearing assembly according to claim 1 wherein said pair of inserts are formed from a non-metallic material to enhance slidability between the inserts and the hinge members.

9. A thrust bearing assembly for a pinless hinge structure including two rotatable hinge members and a clamp member, said hinge members being longitudinally movable relative to each other and are rotatably joined along adjacent longitudinal edges by intermeshing gear segments forming part of and which allow said hinge members to longitudinally move relative to each other with said clamp member maintaining the gear segments in mesh, said thrust bearing assembly comprising:

at least two inserts disposed in side-by-side relation in adjacent longitudinally co-extensive recesses defined along adjacent longitudinal edges of each hinge member and extending laterally across the hinge members to inhibit relative longitudinal movements therebetween, said inserts being joined to each other by a tongue-and-groove configuration defined along adjacent longitudinal edges of the inserts and which inhibits longitudinal movement therebetween and permits the inserts to be rotationally moved relative to each other to facilitate insertion and removal of the thrust bearing assembly into and from the hinge structure while maintaining the hinge members in mesh with each other.

10. The thrust bearing assembly according to claim 9 wherein an adjacent longitudinal edge of one insert has a convex-shaped profile while an adjacent longitudinal edge of the other insert has a concave-shaped profile, said profiles permitting the inserts to be rotationally displaced relative to each other.

11. The thrust bearing assembly according to claim 9 wherein each of said inserts defines a longitudinally extending generally C-shaped channel which rotatably accommodates an inwardly turned end of said clamp member, the shape of said channel permitting removal of each insert from the recesses defined by the hinge members upon rotation of the inserts relative to each other.

12. The thrust bearing assembly according to claim 9 wherein each of said inserts have non-metallic upper and lower bearing surfaces which slidably engage upper and lower surfaces of the recesses defined by the hinge members.

13. The thrust bearing assembly according to claim 9 further including a detent mechanism disposed along the adjacent longitudinal edges of the inserts to inhibit inadvertent rotational movements of the inserts relative to each other.