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Metal chip briquetting machine main structure and function
add time：2015-12-08
body:
The fuselage is welded and processed by the left and right side frames, the front frame, the base, the side cylinder support, and the cover cylinder support, respectively, and then welded together into a box type. The cover plate is hinged to the left and right side walls through the two axle shafts from the support hole on the left and right side walls. The door slides in the support groove on the side wall. All the inner walls of the material box are equipped with guard plates to facilitate repair and replacement after wear.
main tank:
The master cylinder is a double-acting, single-piston rod type cylinder that is bolted to the right side frame of the fuselage. The cylinder is equipped with a piston and a YX-shaped sealing ring is mounted on the piston to form two oil chambers in the cylinder. When the high-pressure liquid acts on the sealing ring, the two wings of the sealing ring are tightly attached to the piston and the cylinder wall to ensure that the two oil chambers are not collateral. Both ends of the cylinder are also equipped with sealing rings. The cylinder ports are also equipped with guide sleeves for supporting and guiding the piston rod. The piston rod and the indenter are fastened with a screw flange.
Side cylinder:
The side cylinder is mounted on the lower part of the door beam, and is hinged to the support hole in the rear part of the right side frame with two half pins. The piston rod and the pressure head are connected by a screw flange, which is used for the secondary compression and the compression type. The material inside is initially formed.
Cover cylinder:
The cover cylinder is a double-acting, single-piston rod type cylinder. The two axle shafts are hinged to the body cap cylinder support seat. The piston rod and the body cover are hinged with a pin to drive the cover for rotational movement.
Gate cylinder:
The gate cylinder is a double acting single rod type cylinder. One end of the cylinder block is supported on the bearing support at the rear part of the left frame of the fuselage by a pin. A rectangular flange is screwed on the outer end of the piston rod, and the flange is connected to the door with screws, so that the gate cylinder reciprocates.
Locking mechanism
The locking mechanism consists of a spring-return cylinder (one-way action of the piston, resetting the piston by a spring) and parts connected to the front frame. Two sets of locking mechanisms are installed side by side in the upper hole of the front frame. The locking pin, the piston rod and the guide rod (into the oil) are integrated to ensure that the cover-locking-opening and other actions are repeated.
The fuselage is welded and processed by the left and right side frames, the front frame, the base, the side cylinder support, and the cover cylinder support, respectively, and then welded together into a box type. The cover plate is hinged to the left and right side walls through the two axle shafts from the support hole on the left and right side walls. The door slides in the support groove on the side wall. All the inner walls of the material box are equipped with guard plates to facilitate repair and replacement after wear.
main tank:
The master cylinder is a double-acting, single-piston rod type cylinder that is bolted to the right side frame of the fuselage. The cylinder is equipped with a piston and a YX-shaped sealing ring is mounted on the piston to form two oil chambers in the cylinder. When the high-pressure liquid acts on the sealing ring, the two wings of the sealing ring are tightly attached to the piston and the cylinder wall to ensure that the two oil chambers are not collateral. Both ends of the cylinder are also equipped with sealing rings. The cylinder ports are also equipped with guide sleeves for supporting and guiding the piston rod. The piston rod and the indenter are fastened with a screw flange.
Side cylinder:
The side cylinder is mounted on the lower part of the door beam, and is hinged to the support hole in the rear part of the right side frame with two half pins. The piston rod and the pressure head are connected by a screw flange, which is used for the secondary compression and the compression type. The material inside is initially formed.
Cover cylinder:
The cover cylinder is a double-acting, single-piston rod type cylinder. The two axle shafts are hinged to the body cap cylinder support seat. The piston rod and the body cover are hinged with a pin to drive the cover for rotational movement.
Gate cylinder:
The gate cylinder is a double acting single rod type cylinder. One end of the cylinder block is supported on the bearing support at the rear part of the left frame of the fuselage by a pin. A rectangular flange is screwed on the outer end of the piston rod, and the flange is connected to the door with screws, so that the gate cylinder reciprocates.
Locking mechanism
The locking mechanism consists of a spring-return cylinder (one-way action of the piston, resetting the piston by a spring) and parts connected to the front frame. Two sets of locking mechanisms are installed side by side in the upper hole of the front frame. The locking pin, the piston rod and the guide rod (into the oil) are integrated to ensure that the cover-locking-opening and other actions are repeated.
