High suction pressure single screw compressor with thrust balancing load using shaft seal pressure and related methods
A high suction pressure thrust load balance assembly configured for use with a single screw compressor includes comprises a sealing baffle that is keyed to, so as to be rotatable along with, a main rotor drive shaft of the single screw compressor. The sealing baffle is configured to create a force or load to counteract the axial force of the main rotor drive shaft created during rotation of the main rotor drive shaft using the pressurized oil used to lubricate the mechanical shaft seal of the compressor.
1. A single screw compressor comprising:
a housing;
a main rotor that is secured within the housing and rotatably driven by a main rotor drive shaft, and operably engaged with a plurality of gate rotors that are also secured within the housing; and
a high suction pressure load balance assembly, the assembly comprising
a sealing baffle that is keyed to, so as to be rotatable along with, the main rotor drive shaft,
and wherein the sealing baffle is configured to create a force or load to counteract an axial force of the main rotor drive shaft created during a rotation of the main rotor; and
at least one bearing positioned between the housing and the main rotor drive shaft;
a seal housing;
at least two seals positioned with respect to the seal housing; and
a seal pressure cavity defined by the at least one bearing, the housing, the seal housing, the at least two seals and the main rotor drive shaft.
2. The single screw compressor of claim 1 , wherein the high suction pressure load balance assembly is structured to aid in preventing an excessive load on one or more shaft bearings during an operation of the compressor under a high input or suction pressure condition.
3. The single screw compressor of claim 2 , wherein the high input or suction pressure condition is greater than or equal to 300 psi.
4. The single screw compressor of claim 1 , wherein the sealing baffle projects into the seal pressure cavity.
5. The single screw compressor of claim 4 , wherein the sealing baffle is adjacent the at least one bearing.
6. The single screw compressor of claim 5 , wherein the at least one bearing is a roller bearing.
7. The single screw compressor of claim 1 , wherein the compressor further comprises at least one baffle adjacent the at least one bearing opposite the sealing baffle.
8. The single screw compressor of claim 1 , wherein the seal pressure cavity contains a volume of fluid.
9. The single screw compressor of claim 1 , wherein the sealing baffle has an outer surface which is smooth.
10. The single screw compressor of claim 1 , wherein the sealing baffle has an outer surface comprising at least one groove.
11. The single screw compressor of claim 1 , wherein the at least one bearing is a roller bearing.
12. A method of operating a single screw compressor in a high input or suction pressure environment, the method comprising:
providing the single screw compressor comprising
a housing;
a main rotor that is secured within the housing and rotatably driven by a main rotor drive shaft, and operably engaged with a plurality of gate rotors that are also secured within the housing;
a high suction pressure load balance assembly, the assembly comprising a sealing baffle that is keyed to, so as to be rotatable along with, the main rotor drive shaft;
at least one bearing positioned between the housing and the main rotor drive shaft;
a seal housing;
at least two seals positioned with respect to the seal housing; and
a seal pressure cavity defined by the at least one bearing, the housing, the seal housing, the at least two seals and the main rotor drive shaft, wherein the seal pressure cavity includes a volume of fluid;
creating a high input or suction pressure condition in which a suction pressure is created and is greater than or equal to 300 psi, and in which a high thrust load on the main rotor is created; and
using the high pressure suction load balance assembly to balance or counter the thrust load, thereby reducing a net thrust load on the main rotor.
13. The method of claim 12 , wherein the at least one bearing is a roller bearing.
14. The method of claim 12 , further comprising the step of creating a fluid pressure in the seal pressure cavity.
15. The method of claim 14 , wherein the step of using the high pressure suction load balance assembly to balance or counter the thrust load comprises using the fluid pressure in the seal pressure cavity to create a force that balances or counters the thrust load.
16. The method of claim 12 , wherein the sealing baffle has an outer surface which is smooth.
17. The method of claim 12 , wherein the sealing baffle has an outer surface comprising at least one groove.