IP Library Granted Patent US 11,040,833
Granted Patent B2
US 11,040,833 · App. 15/781,629 · Granted Jun 22, 2021

Flight bar-clamp-chain link connection for a chain conveyor

Inventors: Christoph Pietrala (Dortmund, DE); Matthias Köhler (Lünen, DE)
Assignee: Caterpillar Global Mining Europe GmbH
B65G19/24B65G19/08B65G17/38B65G19/20B65G2812/0297B65G2812/0298
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Quick Facts
Patent No.
US 11,040,833
App. No.
15/781,629
Granted
Jun 22, 2021
Kind
B2
Abstract

The present disclosure relates to a flight bar clamp for connecting a flight bar to at least one chain link of at least one conveyor chain of a chain conveyor used in underground mining. The flight bar clamp comprises a clamp main body extending along a clamp longitudinal axis, and at least one chain link engaging portion disposed at the clamp main body configured to engage with one chain link. The at least one chain link engaging portion of the flight bar clamp includes a sacrificial anode reception, and a sacrificial anode body disposed in the sacrificial anode reception. The sacrificial anode body may protect the flight bar clamp, the flight bar and the chains from contact corrosion.

Claims (28)

1. A flight bar clamp for connecting a flight bar to at least one chain link of at least one conveyor chain of a chain conveyor used in underground mining, the flight bar clamp comprising:

a clamp main body extending along a clamp longitudinal axis;

at least one chain link engaging portion disposed at the clamp main body and configured to engage with one chain link of the at least one conveyor chain, the at least one chain link engaging portion of the flight bar clamp including a sacrificial anode reception, wherein the sacrificial anode reception is formed as a recess, a stepped portion, or a groove at an end section of the chain link engaging portion; and

a sacrificial anode body disposed in the sacrificial anode reception, wherein the sacrificial anode reception and the sacrificial anode body are configured so that the sacrificial anode body is substantially accommodated in the sacrificial anode reception.

2. The flight bar clamp of claim 1 , wherein:

the at least one chain link engaging portion of the flight bar clamp is formed as a protrusion extending from the clamp main body; or

the at least one chain link engaging portion of the flight bar clamp is formed as a flattened portion at the clamp main body.

3. The flight bar clamp of claim 1 , further including a plurality of mounting studs extending from the clamp main body.

4. The flight bar clamp of claim 3 , wherein:

the mounting studs are spaced apart from the at least one chain link engaging portion, and/or

the mounting studs are integrally formed with the clamp main body.

5. The flight bar clamp of claim 1 , wherein:

the flight bar clamp has an E-shaped profile with three mounting studs extending from the clamp main body in a direction perpendicular to the clamp longitudinal axis; or

the flight bar clamp has a C-shaped profile with two mounting studs extending from the clamp main body in a direction perpendicular to the longitudinal axis.

6. A flight bar for connecting to at least one chain link of at least one conveyor chain of a chain conveyor used in underground mining via a flight bar clamp, the flight bar comprising:

a flight bar main body extending along a flight bar longitudinal axis and including at least one chain link reception recess for receiving one chain link of the conveyor chain,

a chain link engaging portion disposed in the chain link reception recess and configured to engage with the one chain link of the at least one conveyor chain, the chain link engaging portion of the flight bar including a sacrificial anode reception, wherein the sacrificial anode reception is formed as a recess, a stepped portion, or a groove at an end section of the chain link engaging portion; and

a sacrificial anode body disposed in the sacrificial anode reception, wherein the sacrificial anode reception and the sacrificial anode body are configured so that the sacrificial anode body is substantially accommodated in the sacrificial anode reception.

7. The flight bar of claim 6 , wherein:

the chain link engaging portion of the flight bar is formed as a protrusion extending from a bottom face of the at least one chain link reception; or

the chain link engaging portion of the flight bar is formed as a flattened portion in the at least one chain link reception recess.

8. The flight bar of claim 6 , wherein the flight bar main body further includes a plurality of throughholes for receiving mounting studs of the flight bar clamp.

9. The flight bar of claim 8 , wherein the throughholes are spaced apart from the at least one chain link engaging portion of the flight bar.

10. The flight bar of claim 8 , wherein:

the flight bar has a substantially H-profile cross-section in a plane perpendicular to the flight bar longitudinal axis and at a position of each throughhole, the throughholes extending through the intermediate leg of the H-profile; and/or

the flight bar has a solid cross-section in a plane perpendicular to the flight bar longitudinal axis and at a position of each chain link engaging portion.

11. The flight bar clamp of claim 1 , wherein the sacrificial anode body is disposed in the sacrificial anode reception in a replaceable manner.

12. The flight bar clamp of claim 1 , wherein the sacrificial anode body is formed as a solid body or as an annular body, for example a circular ring body.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 30, 2022
From: CATERPILLAR GLOBAL MINING EUROPE GMBH
To: CATERPILLAR INC.
Reel/Frame 062024/0906 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 5, 2018
From: PIETRALA, CHRISTOPH; KOHLER, MATTHIAS
To: CATERPILLAR GLOBAL MINING EUROPE GMBH
Reel/Frame 045992/0374 →
Priority Claims (1)
EP 151992330 · Dec 10, 2015 · regional
Continuity (1)
Related Publication 20200262653A1 · Aug 20, 2020