초록 ▼

An adjustment method and system for an auxiliary power unit (APU) allows the APU speed to vary based on the inlet air temperature to the APU compressor. The APU is controlled by a control law that allows the APU speed to float within a selected range based on speed and electric power generators phas

An adjustment method and system for an auxiliary power unit (APU) allows the APU speed to vary based on the inlet air temperature to the APU compressor. The APU is controlled by a control law that allows the APU speed to float within a selected range based on speed and electric power generators phase matching criteria that provides smooth power transfer between the APU and a main engine generator. The specific APU mechanical speed for a given temperature may be determined from a compressor map that identifies the optimum combination of pressure ratio, flow rate and efficiency for a given inlet temperature, and avoids running the APU near mechanical resonant vibration conditions.

대표청구항 ▼

What is claimed is: 1. A method for controlling a gas turbine auxiliary power unit (APU), comprising: detecting an inlet temperature; and varying an APU shaft speed in response to the inlet temperature to maintain a corrected speed between a minimum mechanical speed and a maximum mechanical speed.

What is claimed is: 1. A method for controlling a gas turbine auxiliary power unit (APU), comprising: detecting an inlet temperature; and varying an APU shaft speed in response to the inlet temperature to maintain a corrected speed between a minimum mechanical speed and a maximum mechanical speed. 2. The method of claim 1, wherein the varying step comprises: increasing the APU shaft speed when the detected inlet temperature increases; and decreasing the APU shaft speed when the detected inlet temperature decreases. 3. The method of claim 2, wherein the varying step further comprises: calculating the corrected speed from the APU shaft speed and the inlet temperature; and maintaining the corrected speed within a selected optimum region with the increasing and decreasing steps. 4. The method of claim 3, wherein the optimum region corresponds to a substantially constant corrected speed. 5. The method of claim 4, wherein the substantially constant corrected speed is between 95% and 105% of a design speed. 6. The method of claim 3, further comprising: overriding the maintaining step during a power transfer operation between the APU and a main engine. 7. A method for controlling an auxiliary power unit (APU), comprising: detecting an inlet air temperature; calculating a corrected speed from an APU shaft speed and the inlet temperature; and maintaining the corrected speed within a selected optimum region by varying the APU shaft speed based on the inlet air temperature, wherein the APU shaft speed is increased when the detected inlet air temperature increases and wherein the APU shaft speed is decreased when the detected inlet air temperature decreases. 8. The method of claim 7, wherein the step of calculating the corrected speed comprises dividing the APU shaft speed by a normalized inlet temperature value calculated from the inlet temperature. 9. The method of claim 7, wherein the corrected speed in the optimum region is between approximately 95% and 105% of a design speed. 10. The method of claim 7, further comprising overriding the maintaining step during a power transfer operation between the APU and a main engine. 11. The method of claim 7, wherein the maintaining step further comprises adjusting a flow through the APU. 12. The method of claim 1, further comprising the steps of: defining the minimum mechanical speed as 85% Nmech; and defining the maximum mechanical speed at 107% Nmech wherein % Nc=% Nmech/THETA)^0.5. 13. The method of claim 1, wherein the varying step is in response to a compressor map.