FIG. 1 shows a cross section of the screw compressor regarding the invention
FIG. 2 shows the rotor pair
FIG. 3 shows the screw compressor housing
FIG. 4 shows the cavity volume, as a function of the male rotor position
FIG. 1 shows a screw compressor according to the invention for compression of a working fluid to a discharge pressure of 100 bar, e.g. for application in refrigeration systems operating with CO2 in a transcritical process featuring two rotors, a male rotor 1 and a female rotor 2 with the male rotor 1 having a drive-shaft end 3, and both rotors are enclosed in a housing 8 featuring at least an inlet port 7 for passing of the working fluid into the lobes of the rotor pair and at least an outlet port 9 for discharge of the gas due to rotation of the rotors. The profile sections of the rotors have shaft shoulders 4 enclosed in radial bearings 5 with the resulting axial forces being supported by axial bearings 6.
The profile section of male rotor 1 has five lobes, while profile section of the female rotor 2 has six lobes. The wrap angle of the male-rotor profile section is 1.4 times the value of the lobe-pitch angle and amounts to 100°. The axial length of the profile section of the rotor pair has the value of 1.4 times the axial lobe pitch of the male rotor.
For this case of operation, the bearings of the compressor according to the invention have been dimensioned sufficiently large. The service life of the bearings meets the requirements.
The internal leakage demonstrated by a geometrical relationship between the length of the rotor meshing line and the volume of the cavity is less by the factor 2 to 3 compared to known high-pressure screw compressors having a ratio of male-to-female rotor lobes of 6:8 so that the efficiency of the compressor according to the invention is higher than that of known high-pressure screw compressors.
LIST OF REFERENCE NUMBERALS USED:
1 male rotor
2 female rotor
3 driving shaft
4 shaft
5 radial bearing
6 axial bearing
7 inlet port
8 housing
9 outlet port
10 cavities
11 profile section
12 lobe pitch angle
13 wrap angle
14 economizer connection
15 transfer phase
16 male rotor diameter
17 profile length
18 connection to inlet port closes