Coal nozzle assembly comprising two flow channels

1. A coal nozzle assembly for a steam generation apparatus comprising an elongated nozzle body having a nozzle tip at one end thereof; said nozzle tip comprising two channels each channel having a curved or buckled flow path, the nozzle tip further comprising means separating the channels from each other and splitting a stream of coal particles and primary air exiting the nozzle body into two partial streams inside the nozzle tip, wherein the directions of the flow paths of the channels at their ends distal from the nozzle body enclose an angle greater than 0° and equal to or less than 90° wherein the partial streams are redirected inside the nozzle tip through the curved or buckled flow paths such that they intersect and shear against each other upon exit of the nozzle tip before they are combusted.

2. A steam generating system which comprises a furnace and at least one coal nozzle assembly according to claim 1 .

3. A method to operate a steam generating system which comprises a furnace and at least one coal nozzle assembly according to claim 1 , the method comprising initially adjusting an angle of the nozzle tips during at least one of commissioning and adjusting the angle of the nozzle tips during operation of the system as a function of at least one of the load of the steam generating system and/or dependent from burned fuel.

4. A coal nozzle assembly for a steam generation apparatus comprising an elongated nozzle body and an inner shell having two nozzle tips at one end thereof; the coal nozzle assembly further comprising means being located in the inner shell upstream of said two nozzle tips and splitting a stream of coal particles and primary air from said nozzle body into partial streams flowing through the two nozzle tips, the directions of the flow paths of the two nozzle tips enclosing an angle (α) greater than 0° and equal to or less than 90°, wherein the two partial streams are redirected by means of the two nozzle tips such that they intersect and shear against each other upon exit of the nozzle tip before they are combusted.

5. Coal nozzle assembly according to claim 4 wherein that the nozzle tips are mounted for pivotal movement about an axis being orthogonal with respect to the longitudinal axis of the elongate body or the inner shell.

6. Coal nozzle assembly according to claim 4 wherein at least one of the nozzle body or the inner shell and the nozzle tips partially overlap.

7. Coal nozzle assembly according to in claim 4 wherein the assembly further comprises an air housing.

8. Coal nozzle assembly according to claim 7 wherein at least one of the nozzle body and/or the inner shell and the nozzle tips as well as the air housing limit at least one channel for conveying secondary air.

9. Coal nozzle assembly according to claim 4 wherein at least one of the nozzle body and/or the inner shell have at least one of a rectangular or truncated pyramid longitudinal section.

10. Coal nozzle assembly according to claim 4 wherein that the directions of the flow paths of the channels at their ends distal from the nozzle body enclose an angle that is at least one of greater than 15°; or greater than 30°; and/or less than 75°; or less than 60°.

11. Coal nozzle assembly according to claim 4 wherein each nozzle tip comprises exit faces and at least one shear bar arranged near the exit faces.

12. Coal nozzle assembly according to claim 4 wherein the assembly comprises at least one splitter plate to direct the flow of air and coal particles.

13. Coal nozzle assembly according to claim 4 wherein that a catalyst is applied to the internal walls of the nozzle tip.

14. Coal nozzle assembly according to claim 13 wherein that the catalyst is a perovskite-type catalyst with catalytic activity in a preferred temperature range, of 500° C. to 900° C.

15. Coal nozzle assembly according to claim 13 wherein that the catalyst is Lanthanum Strontium Titanate doped with metals.