METHOD OF OPTIMIZING SUPERCHARGER PERFORMANCE
A method of optimizing performance of a supercharger for a given application includes determining a desired pressure ratio of supercharger operation for the given application. One of a rotor lead and a rotor speed can be determined based on the given application. The other of the rotor lead and the rotor speed can be determined based on the pressure ratio and the one of the rotor lead and rotor speed. According to other features, the other of the rotor lead and the rotor speed can be determined based on a peak efficiency map.
1 . A method of optimizing performance of a supercharger for a given application, the method comprising:
determining a desired pressure ratio of supercharger operation for the given application;
determining one of a rotor lead and a rotor speed based on the given application; and
determining the other of the rotor lead and rotor speed based on the desired pressure ratio and the one of the rotor lead and rotor speed.
2 . The method of claim 1 wherein the other of the rotor lead and rotor speed is determined based on a peak efficiency map.
3 . The method of claim 2 , further comprising determining the rotor speed based on the desired pressure ratio and the determined rotor lead.
4 . The method of claim 3 wherein the rotor speed is about 11,000 RPM based on the desired pressure ratio of 1.4 and a determined rotor lead of about 300 mm.
5 . The method of claim 3 wherein the rotor speed is about 7,500 RPM based on the desired pressure ratio of 1.4 and a determined rotor lead of about 400 mm.
6 . The method of claim 3 wherein the rotor speed is about 12,500 RPM based on the desired pressure ratio of 1.6 and a determined rotor lead of about 300 mm.
7 . The method of claim 3 wherein the rotor speed is about 15,000 RPM based on the desired pressure ratio of 1.8 and a determined rotor lead of 300 mm.
8 . The method of claim 3 wherein the rotor speed is about 10,500 RPM based on the desired pressure ratio of 1.8 and a determined rotor lead of 400 mm.
9 . A method of optimizing performance of a supercharger for a given application, the method comprising:
determining a rotor lead based on the given application;
determining a rotor speed based on the given application; and
determining a desired pressure ratio of supercharger operation for the given application based on the determined rotor lead and the rotor speed.
10 . The method of claim 9 wherein the desired pressure ratio of the supercharger is determined based on a peak efficiency map.
11 . The method of claim 10 wherein the desired pressure ratio is 1.4 for a rotor speed of about 11,000 RPM and a rotor lead of 300 mm.
12 . The method of claim 10 wherein the desired pressure ratio is 1.4 for a rotor speed of about 7,500 RPM and a rotor lead of about 400 mm.
13 . The method of claim 10 wherein the desired pressure ratio is 1.6 for a rotor speed of about 12,500 RPM and a rotor lead of about 300 mm.
14 . The method of claim 10 wherein the desired pressure ratio is 1.8 for a rotor speed of about 15,000 RPM and a rotor lead of 300 mm.
15 . A method of optimizing performance of a supercharger for a given application, the method comprising:
determining a desired pressure ratio of supercharger operation for the given application based on a peak efficiency map;
determining a rotor speed based on the given application; and
determining a desired rotor lead based on the determined desired pressure ratio and the determined rotor speed of the given application.
16 . The method of claim 15 wherein the rotor lead is about 300 mm based on the desired pressure ratio of 1.4 and a determined rotor speed of 11,000 RPM.
17 . The method of claim 15 wherein the rotor lead is about 400 mm based on the desired pressure ratio of 1.4 and a determined rotor speed of 7,500 RPM.
18 . The method of claim 15 wherein the rotor lead is about 300 mm based on the desired pressure ratio of 1.6 and a determined rotor speed of 12,500 RPM.
19 . The method of claim 15 wherein the rotor lead is about 300 mm based on the desired pressure ratio of 1.8 and a determined rotor speed of 15,000 RPM.
20 . The method of claim 15 wherein the rotor lead is about 400 mm based on a pressure ratio of 1.8 and a rotor speed of 10,500 RPM.