Co-injection hot runner nozzle
A co-injection hot runner nozzle comprises an inner melt flow channel and an annular outer melt flow channel that surrounds the inner melt flow channel. The inner and outer melt flow channels have a first common source. The nozzle further comprises an annular intermediate melt flow channel disposed between the inner and outer melt flow channels. The annular intermediate melt flow channel is at least partly defined by a plurality of spiral grooves, each spiral groove having a respective inlet and defining a helical flow path. Lands between adjacent spiral grooves increase in clearance in a downstream direction. An annular axial flow path is defined over the lands. A plurality of feeder channels having a second common source is configured to supply melt to the plurality of inlets of the spiral grooves. The relationship of feeder channels to spiral grooves may be one-to-one. The inlets may be longitudinal channels.
1. A co-injection hot runner nozzle comprising:
an inner melt flow channel;
an annular outer melt flow channel that surrounds the inner melt flow channel, the inner and outer melt flow channels having a first common source;
an annular intermediate melt flow channel, disposed between the inner and outer melt flow channels, that is at least partly defined by a plurality of spiral grooves, each spiral groove having a respective inlet and defining a helical flow path, with lands between adjacent spiral grooves that increase in clearance in a downstream direction, wherein an annular axial flow path is defined over the lands; and
a plurality of feeder channels, having a second common source, for supplying melt to the plurality of inlets of the spiral grooves, wherein each of the feeder channels is for supplying melt to the inlet of a respective one of the spiral grooves; and
a plurality of flow transition channels arranged in a ring for producing an annular melt flow that, in operation, will flow through the annular outer melt flow channel, each of the flow transition channels having an inlet, an outlet with a part-annulus shape, and a pair of opposing side walls that diverges in the downstream direction.
2. The co-injection nozzle of claim 1 wherein each of the inlets comprises a longitudinal channel and further comprising, for each spiral groove, a flow redirection channel for redirecting longitudinally flowing melt from the respective inlet into the spiral groove.
3. The co-injection nozzle of claim 2 wherein each of the flow redirection channels comprises a gradual bend of about 70 degrees away from longitudinal.
4. The co-injection hot runner nozzle of claim 1 wherein the spiral grooves are formed in an inner wall of the annular intermediate melt flow channel.
5. The co-injection hot runner nozzle of claim 1 wherein the spiral grooves are formed in an outer wall of the annular intermediate melt flow channel.
6. The co-injection hot runner nozzle of claim 1 wherein each spiral groove decreases in depth in the downstream direction.
7. The co-injection hot runner nozzle of claim 1 wherein the inner melt flow channel is substantially cylindrical.
8. A co-injection hot runner nozzle comprising:
an inner melt flow channel;
an annular outer melt flow channel that surrounds the inner melt flow channel, the inner and outer melt flow channels having a first common source;
an annular intermediate melt flow channel, disposed between the inner and outer melt flow channels, that is at least partly defined by a plurality of spiral grooves, each spiral groove having a respective inlet and defining a helical flow path, with lands between adjacent spiral grooves that increase in clearance in a downstream direction, wherein an annular axial flow path is defined over the lands; and
a plurality of feeder channels, having a second common source, for supplying melt to the plurality of inlets of the spiral grooves,
wherein each of the inlets comprises a longitudinal channel and further comprising, for each spiral groove, a flow redirection channel for redirecting longitudinally flowing melt from the respective inlet into the spiral groove, and
wherein each of the flow redirection channels comprises a gradual bend of about 70 degrees away from longitudinal.