Injection lance assembly
View Patent ↗The system and method for preventing air leakage from the process side to the bearing side of a mill. The system includes a labyrinth seal ring comprising a series of knives defining first and second labyrinth paths from an air inlet to the process side and the bearing side of the system, respectively. The differences in the two paths such as provided by the number of knives used in each path creates a differential pressure drop which biases air from the air inlet to the process side. The labyrinth seal thus provides a reliable and superior method for reducing the potential for particulate in the process side of the mill from damaging the bearing system.
1. An injection lance assembly which can be inserted into a port in ductwork, the lance assembly comprising;
a) a tube for providing particulate flow into a fluid stream within the ductwork;
b) at least one wing which is deployable within the ductwork and may be inserted through the port with the tube; and
c) means for displacing the wing into a deployed position;
whereby the lance assembly when deployed in the ductwork has a larger diameter than the port.
2. The assembly of claim 1 wherein the means for displacing comprises a cable actuator.
3. The assembly of claim 1 wherein the tube further comprises a tip region, the tip region providing the means for displacing the wing.
4. The assembly of claim 1 , wherein the means for displacing comprises a punch rod.
5. The assembly of claim 1 , wherein the at least one wing comprises a pair of wings.
6. The assembly of claim 5 , wherein the wings pivot radially relative to the tube.
7. The assembly of claim 5 , wherein the wings deploy rotationally relative to the tube.
8. The assembly of claim 5 , wherein the wings are attached to the tube.
9. The assembly of claim 1 , further comprising a shroud defining a channel with the tube displaceable therethrough, the wing being attached to the shroud.
10. The assembly of claim 1 , wherein the tube comprises a plurality of tubes.
11. The assembly of claim 1 , wherein the tube includes a plurality of apertures along the length of the tube.
12. The assembly of claim 11 , wherein each of the plurality of apertures is at an axial location corresponding to the wing.
13. The assembly of claim 1 , further comprising a means for retracting the wing through the port.
14. The assembly of claim 13 , wherein the means for retracting uses the same structure as the means for displacing.
15. An injection lance assembly which can be inserted into first and second ports of a ductwork, the assembly comprising;
a) a tube for providing particulate flow into a fluid stream within the ductwork, the tube being through the first port;
b) a blade being displaced through the second port, the blade having first and second portions, the first portion providing a barrier to blunt passage of airflow therethrough, and the second portion including a curvature to encourage rotation of the blade;
whereby the blade when deployed has a rotation diameter greater than the diameter of the second port.