Patent classifications
B65G39/06
Belt conveyor roller wear liner, belt conveyor roller and conveyor including same and corresponding method
The present disclosure concerns a belt conveyor roller wear liner superposable against an outer peripheral surface of a roller cylindrical body, the roller wear liner comprising: a shock-absorbing matrix; and a plurality of inserts, spaced-apart from one another and embedded in the shock-absorbing matrix with external surfaces of the inserts and the shock-absorbing matrix, extending between the inserts, being exposed outwardly, the roller wear liner being substantially ring-shaped. It also concerns a corresponding belt conveyor roller assembly, a corresponding belt conveyor and a corresponding method.
Belt conveyor roller wear liner, belt conveyor roller and conveyor including same and corresponding method
The present disclosure concerns a belt conveyor roller wear liner superposable against an outer peripheral surface of a roller cylindrical body, the roller wear liner comprising: a shock-absorbing matrix; and a plurality of inserts, spaced-apart from one another and embedded in the shock-absorbing matrix with external surfaces of the inserts and the shock-absorbing matrix, extending between the inserts, being exposed outwardly, the roller wear liner being substantially ring-shaped. It also concerns a corresponding belt conveyor roller assembly, a corresponding belt conveyor and a corresponding method.
AIRCRAFT LANDING GEAR ASSEMBLY
An aircraft landing gear assembly including structural members coupled via a coupling including a bearing. The bearing has a body defining a first bearing surface arranged to contact a first counter-face of the coupling. The first bearing surface is defined by a first tubular layer of fibre reinforced polymer of a first type having an axis and containing synthetic fibres of a first type wound around and along the axis of the bearing. The bearing body further has a second tubular layer of fibre reinforced polymer of a second type containing synthetic fibres of a second type wound around and along the axis of the bearing.
AIRCRAFT LANDING GEAR ASSEMBLY
An aircraft landing gear assembly including structural members coupled via a coupling including a bearing. The bearing has a body defining a first bearing surface arranged to contact a first counter-face of the coupling. The first bearing surface is defined by a first tubular layer of fibre reinforced polymer of a first type having an axis and containing synthetic fibres of a first type wound around and along the axis of the bearing. The bearing body further has a second tubular layer of fibre reinforced polymer of a second type containing synthetic fibres of a second type wound around and along the axis of the bearing.
BELT CONVEYOR ROLLER WEAR LINER, BELT CONVEYOR ROLLER AND CONVEYOR INCLUDING SAME AND CORRESPONDING METHOD
The present disclosure concerns a belt conveyor roller wear liner superposable against an outer peripheral surface of a roller cylindrical body, the roller wear liner comprising: a shock-absorbing matrix; and a plurality of inserts, spaced-apart from one another and embedded in the shock-absorbing matrix with external surfaces of the inserts and the shock-absorbing matrix, extending between the inserts, being exposed outwardly, the roller wear liner being substantially ring-shaped. It also concerns a corresponding belt conveyor roller assembly, a corresponding belt conveyor and a corresponding method.
BELT CONVEYOR ROLLER WEAR LINER, BELT CONVEYOR ROLLER AND CONVEYOR INCLUDING SAME AND CORRESPONDING METHOD
The present disclosure concerns a belt conveyor roller wear liner superposable against an outer peripheral surface of a roller cylindrical body, the roller wear liner comprising: a shock-absorbing matrix; and a plurality of inserts, spaced-apart from one another and embedded in the shock-absorbing matrix with external surfaces of the inserts and the shock-absorbing matrix, extending between the inserts, being exposed outwardly, the roller wear liner being substantially ring-shaped. It also concerns a corresponding belt conveyor roller assembly, a corresponding belt conveyor and a corresponding method.
Return Roller Assemblies for Conveyor Systems
A return roller assembly for a belted conveyor assembly is formed from an elongated circular roller assembly having ends adapted to affix to a frame assembly and at least one groove around the outside thereof, and at least one circular annular return roller assembly containing a rib about the inside circumference thereof. The elongated circular roller assembly groove is adapted to receive the circular annular return roller rib to retaining the circular annular return roller assembly during rotation of the elongated circular roller assembly.
Return Roller Assemblies for Conveyor Systems
A return roller assembly for a belted conveyor assembly is formed from an elongated circular roller assembly having ends adapted to affix to a frame assembly and at least one groove around the outside thereof, and at least one circular annular return roller assembly containing a rib about the inside circumference thereof. The elongated circular roller assembly groove is adapted to receive the circular annular return roller rib to retaining the circular annular return roller assembly during rotation of the elongated circular roller assembly.
Roller and locking method thereof
The present disclosure provides a roller and a locking method thereof. The roller includes a main body, a first groove provided on an inner surface of the main body, and a first elastic component fitted with the first groove; wherein a through hole for receiving and fixing a shaft is provided on the first elastic component. The present disclosure can be used to lock shafts.
Roller and locking method thereof
The present disclosure provides a roller and a locking method thereof. The roller includes a main body, a first groove provided on an inner surface of the main body, and a first elastic component fitted with the first groove; wherein a through hole for receiving and fixing a shaft is provided on the first elastic component. The present disclosure can be used to lock shafts.