SYSTEM CONTROLLER FOR A HYBRID AIRCRAFT PROPULSION SYSTEM

Abstract

Control logic for a power sharing system on a hybrid propulsion aircraft, utilizing parallel multiple control loops outputting difference commands which provide bumpless transfer between control loops without integrator wind up or reset logic, allowing for efficient load distribution between electric generators and batteries powering electric motors.

Claims

1. A method for controlling power sources in an electrical system comprising: receiving data at a system control regarding instantaneous operating parameters of a first power source and a second power source; predetermining data regarding operating limits of the first power source and the second power source; determining the instantaneous operating parameter of the first power source and the second power source in closest proximity to an operating limit; and, controlling at least one of the first power source or the second power source based on the determination.

2. The method of claim 1, wherein the instantaneous operating parameters are prioritized based on potential adverse effects if a limit is exceeded.

3. The method of claim 1, further comprising receiving at the system control data regarding a power demand of the electrical system; wherein the power demand of electrical system is an electric motor driving a propeller or fan.

4. The method of claim 1, wherein the instantaneous operating parameters comprise current, voltage, torque, or speed.

5. The method of claim 1, wherein the operating limits comprise maximum current, minimum current, maximum torque, minimum torque.

6. The method of claim 1, wherein the electric motor is powered by both the first power source and the second power source.

7. The method of claim 1, wherein the first power source is a battery and normally operates at a first reference rate.

8. The method of claim 7, wherein the battery acts as a voltage regulator.

9. The method of claim 8, wherein the battery normally accounts for fast transient loads.

10. The method of claim 9, wherein the second power source is an electric generator and normally accounts for sustained load changes.

11. The method of claim 1, wherein the first power source and the second power source are generators.

12. A method for controlling two or more power sources in an electrical system comprising: receiving data at a system control regarding instantaneous operating parameters of the two or more power sources; predetermining data regarding operating limits of each of the two or more power sources; determining for each of the two or more power sources a relative margin between the received data and the predetermined data, ranking the two or more powers sources as a function of the relative margins; receiving at the system control, an indication of a change in power demand of the electrical system, and selecting one of the two or more power sources based on the ranking and controlling the one of the two or more power sources in response to the change in power demand.

13. The method of claim 12, wherein the at least one of the two or more power sources is an electric generator.

14. The method of claim 13, wherein at least one of the two or more power sources is a battery.

15. The method of claim 14, wherein the instantaneous operating parameters comprise battery current, battery voltage, generator torque, generator current, generator voltage, generator speed.

16. The method of claim 14, wherein the operating limits comprise maximum battery current, minimum battery current, maximum generator torque, minimum generator torque.

17. The method of claim 12, wherein an electric motor is powered by all of the two or more power sources.

18. The method of claim 17, wherein the battery normally operates at a reference rate and is preferentially selected to regulate voltage and and supply power for fast transient loads when all of the two or more power sources have large relative margins.

19. The method of claim 13, wherein the electric generator is preferentially selected to supply power for sustained load changes, when all of the two or more power sources have large relative margins.

20. A method for controlling power supplies in an electrical system having a battery, an electric generator, and an electric motors comprising: receiving data at a system control regarding instantaneous operating parameters of the battery and the electric generator; predetermining data regarding operating limits of the battery and electric generator; receiving at the system control data regarding a power demand of the electrical system; dividing the instantaneous operating parameters into control loops; assigning a priority to each control loop; determining a limiting instantaneous operating parameter of the battery and electric generator by proximity to a limit within a control loop assigned the lowest priority; comparing the limiting instantaneous operating parameter to an operating parameter of each successive higher priority control loop for proximity to a limit; determining a controlling operating parameter based on the comparison; and, sending a command to control the electric generators or battery to output power to meet the power demand based on the determination.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0009] The following will be apparent from elements of the figures, which are provided for illustrative purposes.

[0010] FIG. 1 depicts a basic load sharing system diagram.

[0011] FIG. 2 depicts a flow chart of the control loop hierarchy.

[0012] FIG. 3 depicts a diagram of information flow of the load sharing system.

[0013] The present application discloses illustrative (i.e., example) embodiments. The claimed inventions are not limited to the illustrative embodiments. Therefore, many implementations of the claims will be different than the illustrative embodiments. Various modifications can be made to the claimed inventions without departing from the spirit and scope of the disclosure. The claims are intended to cover implementations with such modifications.

DETAILED DESCRIPTION

[0014] For the purposes of promoting an understanding of the principles of the disclosure, reference will now be made to a number of illustrative embodiments in the drawings and specific language will be used to describe the same.

[0015] The present disclosure is directed to systems and methods for power sharing within a hybrid power airplane.

[0016] Power Sharing system shown in FIG. 1 uses two or more power sources, typically a battery or electrical storage system to control voltage and power an electric engine. A turbine generator provides power to share loading demanded by the electric engine. The system controller 101 receives feedback from the turbine generators, battery and load, compares the feedback against reference values and uses the most limiting result to generate commands to control the output of the turbine generators and battery.

[0017] During steady operations the battery may act as the voltage regulator of the system and may vary its output for small fast transient load fluctuations. Otherwise the battery may operate at a predetermined reference rate for steady-state operations. Large or sustained load changes may be handled by the turbine generators, allowing the battery to remain at or near its reference rate. This may continue until the load drops or the turbine nears an operating limit at which point battery output power may increase to prevent the limit being reached.

[0018] If the battery trends towards an operating limit or away from its reference rate, loading may be shifted to the turbine generator to ensure the battery can return to its reference rate and not exceed a limit even if there is no change in load. The operating limits are arranged in a hierarchy to ensure load sharing is offset prior to reaching a limit.

[0019] FIG. 2 depicts the hierarchy of multiple control loops used by the system controller 101, here five are depicted. A control loop may output a difference command as a function of the proximity to a limit. This difference command can be used by a common integrator to produce a demand signal.

[0020] The priorities within the hierarchy are based on potential adverse effects, as well as ensuring controlling for one limit will not cause the system to exceed another. The minimum torque limit is the highest priority as it acts to prevent reversing of the generator torque causing them to motor against engine power which can have an impact on shaft life, and is compared to the most limiting case of the other four control loops. The minimum current limit is the next highest priority as it acts to prevent large voltage drops from the battery limiting its current, and is compared to the most limiting case between the max current limiter, the max torque limiter, and the current regulator. The max current limiter's priority is just below the minimum current limiter as it helps to avoid a limit that would result in the power storage self limiting the current to prevent overcharging, and is compared to the most limiting case between the max torque limiter and the current limiter, the two nominal operating states of the system. The max torque limiter is a higher priority than the current regulator and acts in a predictive manner allowing the battery to take on loads which may cause the engines to exceed torque limits. This torque limit may also be set artificially low to prevent overuse of the engine, improving fuel burn or engine life. The current regulator is the lowest priority and the normal mode of operation raising and lowering generator torque to provide a baseline load sharing between the battery and generators. The current regulator is normally set to produce zero battery current, neither charging nor discharging. Either the current regulation setpoint or engine torque limit can be varied to produce battery charging or discharging current. The common integrator receives inputs from various control loops and based on the hierarchy passes on the appropriate current reference to the current tracking control loop. The current tracking control loop may send commands to the generators, engine, and/or battery to increase or decrease generator torque, generator current, or battery current.

[0021] FIG. 3 depicts a system diagram according to an embodiment of the disclosure. Rectifiers 303 may provide torque control of the generators. Inverters 309 may provide speed control of the motors. Both inverters 309 and rectifiers 303 may provide data to the system controller 301, such data may contain voltage, current, torque, speed and status. The system controller 301 may provide data to the rectifiers which may include power, operating mode, torque reference, network management, error checking, and active discharge. To the inverters 309, the system controller 301 may provide data including power, operating mode, speed reference, network management, error checking, and active discharge. The operator interface 311 may provide data to the system controller 301 which may include engine torque limits, and operating commands such as shutdown and emergency stop. The system controller 301 may provide status and to the operator interface 311. An insulation monitoring device (IMD) 313 may be used to detect ground faults and may provide the system control with data including measured resistances. The system controller 301 may receive inputs from an Electronic Engine Controller (EEC) 305 which may provide engine speed control. The EEC 305 may provide data to the system control which may include output torque, gas turbine speed, power turbine speed, and status. The Energy Storage System (ESS) 307 may provide voltage control and provide power for fast transient loads. The ESS 307 may send data to the system controller 301 which may include voltage, current, status, and current limits. The system control may provide to the ESS 307 operating mode, contactor commands, shutdown and emergency stop.

[0022] Although depicted as two, the system may accommodate multiple rectifiers 303 and inverters 309 each set associated with an exclusive turbine generator, thus allowing the generators to operate with different operating conditions. The system may operate in series, parallel, or turbo-electric modes. The system may be expanded to monitor propeller pitch, turbulence, air bursts, and hotel loads.

[0023] Other embodiments of the system may use additional control loops including component temperatures and battery state of charge.

[0024] Some embodiments of the system may include parallel hybrid operation, in which the machines attached to the engine shaft (103, 303) are used as motors (adding their torque to that of the engine to drive a load on the shaft, normally a prop or fan). This mode generally doesn't use any additional motors-driven props (309) since the engine is not producing any electrical power. In some embodiments the power sharing may be between multiple batteries and/or multiple generators per engine and/or multiple engines. Some embodiments may perform a to turbo-electric operation, in which there is no battery in the system. This would entail using shifting power shared between multiple generators and/or engines.

[0025] Although examples are illustrated and described herein, embodiments are nevertheless not limited to the details shown, since various modifications and structural changes may be made therein by those of ordinary skill within the scope and range of equivalents of the claims.