초록 ▼

A system for generating supplemental electrical power from the low-pressure (LP) turbine spool of a turbofan engine includes a high-speed, high magnetic pole count, generator, a gearbox, a controller and a power converter. The LP turbine spool is mechanically coupled to the generator portion by the

A system for generating supplemental electrical power from the low-pressure (LP) turbine spool of a turbofan engine includes a high-speed, high magnetic pole count, generator, a gearbox, a controller and a power converter. The LP turbine spool is mechanically coupled to the generator portion by the gearbox for driving the generator portion. The controller portion has a speed-sensing element for sensing the LP turbine speed. The controller portion disables the power converter when the generator exceeds a predetermined speed, and enables the power converter when the generator portion is less or equal to the predetermined speed. The effective load on the generator is reduced to approximately zero when the LP turbine spool exceeds the predetermined speed, permitting the generator to be electrically bound up to the predetermined speed and mechanically bound in excess of the predetermined speed.

대표청구항 ▼

The invention claimed is: 1. A system for generating supplemental electrical power from the low-pressure (LP) turbine spool of a turbofan engine, the system comprising: a generator portion for generating electrical power, a gearbox for driving the generator portion, a controller portion for control

The invention claimed is: 1. A system for generating supplemental electrical power from the low-pressure (LP) turbine spool of a turbofan engine, the system comprising: a generator portion for generating electrical power, a gearbox for driving the generator portion, a controller portion for controlling an output of the generator; and a power converter for converting generator power to power a load; the LP turbine spool being mechanically coupled to the generator portion by the gearbox for driving the generator portion; and the controller portion in electrical communication with a speed sensing element for sensing a speed of the LP turbine spool; wherein during operation of the engine, the controller portion electronically disables the power converter in response to the speed of the generator portion exceeding a predetermined speed, and enables the power converter when the speed of the generator portion does not exceed the predetermined speed, such that the effective load on the generator portion is reduced to approximately zero when the LP turbine spool exceeds the predetermined speed. 2. The system of claim 1, wherein the generator portion having a speed and a high magnetic pole count, and the magnetic pole count inhibits the speed of the generator portion from exceeding a fundamental frequency limit of the power converter. 3. The system of claim 1, wherein the power converter is an electrically active power converter. 4. The system of claim 3, wherein the fundamental frequency limit is determined by a maximum pulse width modulated (PWM) frequency that can be achieved in the power converter. 5. The system of claim 1, wherein the generator portion is actively generating power during idle descent of an aircraft, the idle descent being associated with a generator speed less than or equal to the predetermined speed, and the generator is rotating passively with approximately zero load when the generator exceeds the predetermined speed. 6. The system of claim 1, wherein the generator portion has an active power generating range at speeds between about 1100 rpm multiplied by the gearbox ratio to and including 2200 rpm multiplied by the gearbox ratio; and a passive rotation range at speeds above 2200 rpm multiplied by the gearbox ratio to about 4500 rpm multiplied by the gearbox ratio. 7. The system of claim 6, wherein the gearbox ratio is in the range of five to ten. 8. The system of claim 1, wherein the generator portion having ten magnetic poles and twelve stator windings. 9. The system of claim 1, wherein the generator portion having a plurality of adjacent, non-overlapping magnetic pole pairs. 10. The system of claim 1, wherein the generator portion having a stator back iron portion and a rotor back iron portion, the stator back iron portion and the rotor back iron portion having significantly reduced thickness relative to low magnetic pole count generators. 11. The system of claim 2, wherein the generator portion having a plurality of electrical phases. 12. A system for generating supplemental electrical power from the low-pressure (LP) turbine spool of a turbofan engine, the system comprising: a generator portion for generating electrical power having a stator back iron portion and a rotor back iron portion, the stator back iron portion and the rotor back iron portion having significantly reduced thickness relative to low magnetic pole count generators; a gearbox for driving the generator portion, a controller portion for controlling an output of the generator; a power converter for converting generator power to power a load; the LP turbine spool being mechanically coupled to the generator portion by the gearbox for driving the generator portion; the controller portion in electrical communication with a speed sensing element for sensing a speed of the LP turbine spool; and wherein during operation of the engine, the controller portion electronically disables the power converter in response to the speed of the generator portion exceeding a predetermined speed, and enables the power converter when the speed of the generator portion does not exceed the predetermined speed, such that the effective load on the generator portion is reduced to approximately zero when the LP turbine spool exceeds the predetermined speed. 13. The system of claim 12, wherein the generator portion having a speed and a high magnetic pole count, and the magnetic pole count inhibits the speed of the generator portion from exceeding a fundamental frequency limit of the power converter. 14. The system of claim 12, wherein the power converter is an electrically active power converter. 15. The system of claim 14, wherein the fundamental frequency limit is determined by a maximum pulse width modulated (PWM) frequency that can be achieved in the power converter. 16. The system of claim 12, wherein the generator portion is actively generating power during idle descent of an aircraft, the idle descent being associated with a generator speed less than or equal to the predetermined speed, and the generator is rotating passively with approximately zero load when the generator exceeds the predetermined speed. 17. The system of claim 12, wherein the generator portion has an active power generating range at speeds between about 1100 rpm multiplied by the gearbox ratio to and including 2200 rpm multiplied by the gearbox ratio; and a passive rotation range at speeds above 2200 rpm multiplied by the gearbox ratio to about 4500 rpm multiplied by the gearbox ratio. 18. The system of claim 17, wherein the gearbox ratio is in the range of five to ten. 19. The system of claim 12, wherein the generator portion having ten magnetic poles and twelve stator windings. 20. The system of claim 12, wherein the generator portion having a plurality of adjacent, non-overlapping magnetic pole pairs.