Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
View Patent ↗A method improving acceleration efficiency of a gas generator of a gas turbine by reducing take-up of electric power, during transition phases, to conserve a sufficiently large surge margin for an operating line. The method increases acceleration/deceleration power of the gas generator by adjusting voltage of an electric network onboard the aircraft. After a phase of starting the gas turbine, voltage of the onboard network is adjusted by a voltage set value controlled by determining unballasting/ballasting status of a main electricity generation source of the onboard network. The status-determining is executed according to demand for taking power to be supplied for propulsion of the aircraft. The status-determining is followed by selecting a voltage set value from plural levels according to the determining the unballasting/ballasting status, and applying the selected set value to a control loop of the voltage supplied to the onboard network.
1. A method for controlling generation of electricity applied to an aircraft gas turbine and output into an on-board network, comprising:
after a phase for starting the gas turbine, regulating a voltage of the on-board network by a voltage set point controlled by determining an unloading/loading status of a main electricity-generating source of the on-board network according to a request for power bleed to be supplied to propulsion of the aircraft;
then, by selecting a voltage set point among plural levels according to a determination of the unloading/loading status; and
applying the selected set point to a loop for regulating voltage supplied to the on-board network.
2. A method for generating electricity according to claim 1 , in which a source of electricity is activated in a case of unloading of the main source to feed the on-board network, whereas a buffer source can be recharged when the main source is not being unloaded.
3. A method for generating electricity according to claim 1 , in which the unloading/loading status is determined among three statuses, of unloading, loading, and stabilized, according to a speed variation of the gas generator, and/or variations in a collective pitch of inclination of rotor blades in a case of a helicopter.
4. A method for generating electricity according to claim 3 , in which the unloading status is determined when the speed variation of the gas generator is at least equal to an upper bound, taken between +2 and +5% per time unit, and/or when the collective pitch variation is higher than an upper bound by +10 to +30% of a full travel per time unit in the case of a helicopter.
5. A method for generating electricity according to claim 3 , in which the loading status is determined when the speed variation of the gas generator is lower than or equal to a lower bound, taken between 2 and 5%, and/or when a collective pitch variation is lower than an upper bound by +10 to +30% of a full travel of the collective pitch per time unit.
6. A method for generating electricity according to claim 3 , in which the stabilization status is determined when the speed variation or the collective pitch are contained between ranges within upper and lower bounds.
7. A method for generating electricity according to claim 1 , in which at least three levels of the voltage set point are determined in the set point selection, in relation with three unloading/loading/stabilized statuses that have been determined of:
a median set-point level is selected when a stabilization status has been determined in or when a state of the on-board network is defective;
a lower set-point level is selected when an unloading status has been determined; and
an upper set-point level is selected when a loading status has been determined or when a stabilized status has been determined to recharge the buffer source of electricity, or further to an acceleration phase of the gas generator during an unloading status.
8. A method for generating electricity according to claim 7 , in which the voltage set point applied to the on-board network is adjusted according to a state of work of the on-board network and/or a state of charge of the buffer source.
9. A method for generating electricity according to claim 8 , in which the state of the on-board network is established according to a state of failure or defect of the network, or a state of work or sensitivity of controls of consumers and accessories.
10. An electrical generation system in a helicopter capable of implementing the method according to claim 1 , comprising:
a reversible starter-generator;
a gas generator capable of driving a mechanism of a propulsion-wing rotor and coupled with the starter-generator which is capable of supplying it with the electric energy source;
devices for measuring a speed of the gas generator or a starter-generator;
an on-board network that can be fed by the starter-generator; and
a numerical control unit;
in which the numerical control unit includes a module for selecting the voltage set point of the on-board network and a regulation loop coupled with a regulator, the module capable of selecting a voltage set point from the data supplied by the devices for measuring a speed, for measuring a position of a collective pitch of the propulsion wing and for measuring a voltage of the on-board network, and the control unit is capable of applying the selected voltage set point to the on-board network via the regulation loop.
11. An electrical generation system according to claim 10 , in which a buffer battery is capable of substituting for the starter-generator to form electrical generation for the on-board network at least during unloading statuses of the starter-generator.
12. An electrical generation system according to the claim 11 , in which a device is capable of monitoring a state of charge of the battery and sensors are capable of detecting malfunctions of the network, or of electric controls.