Unit for generating non-propulsive electrical power
A unit ( 1′, 10′, 100′ ) for generating non-propulsive electrical power for use on board an aircraft, the unit ( 1′, 10′, 100′ ) comprising an electricity production device ( 3, 30 ) comprising a gas turbine ( 31 ) and an electricity generator ( 32 ) mechanically connected to an outlet shaft ( 33 ) of the gas turbine ( 31 ), said electricity generator ( 32 ) including output electrical connections ( 320 ) for being electrically connected to an electrical power supply network ( 2, 20, 200 ) on board an aircraft. The unit ( 1′, 10′, 100′ ) includes energy storage means ( 5 ) and regulator means ( 6 ) configured to control the speed of rotation of the gas turbine ( 31 ) as a function of the electrical power required by the on-board electrical power supply network ( 2, 20, 200 ).
1. A unit for generating non-propulsive electrical power for use on board an aircraft, the unit comprising:
an electricity production device including a gas turbine, and an electricity generator mechanically connected to an outlet shaft of the gas turbine, said electricity generator including output electrical connections to be electrically connected to an electrical power supply network on board the aircraft;
energy storage means comprising a battery;
regulator means configured to control the speed of rotation of the gas turbine as a function of the electrical power required by the on-board electrical power supply network, the regulator means receiving feedback from the on-board electrical power supply network to control the speed of rotation of the gas turbine as the function of the electrical power required by the on-board electrical power supply network;
second power converter means connected between the energy storage means and the electricity production device, the second power converter means comprising
a mechanical transmission gearbox coupled to the outlet shaft of the gas turbine and including a mechanical coupling shaft, and
an electrical machine mechanically coupled to the mechanical transmission gearbox via the mechanical coupling shaft and electrically coupled to electrical terminals of said energy storage means; and
power management means comprising
a first module configured, in a first mode, to cause at least part of power produced based on operation of the electricity production device to be recovered and stored in said energy storage means, and
a second module configured, in a second mode, to cause the on-board electricity power supply network to be powered by both electricity produced from the gas turbine and energy from the energy storage means when electricity required by the on-board electricity power supply network is greater than a predetermined threshold,
wherein the power management means is configured to
actuate the first module when the speed of rotation of the gas turbine is at a maximum and the level of charge in the energy storage means is below a charge threshold so that the electrical machine delivers energy to the energy storage means, and
actuate the second module when electricity required by the on-board electricity power supply network is greater than the predetermined threshold by using the enemy stored by the energy storage means to operate the electrical machine to rotate the outlet shaft of the gas turbine via the mechanical transmission gearbox and the mechanical coupling shaft so as to assist acceleration of the gas turbine.
2. The unit according to claim 1 , wherein the regulator means are configured to cause an increase in the speed of rotation of the gas turbine to a speed higher than that required for generating the electrical power required by the on-board electrical power supply network, the power management means actuating the first module so as to recover the excess power for recharging the energy storage means.
3. The unit according to claim 1 , wherein the electricity production device includes first power converter means, said output electrical connections of the electricity generator being to electrically connect to the on-board electricity power supply network via the first power converter means.
4. The unit according to claim 1 , wherein the second power converter means further comprise a power converter, the electrical terminals of the energy storage means being electrically connected to said electrical machine via the power converter.
5. An aircraft including comprising:
a unit for generating non-propulsive electrical power coupled to an on-board electricity power supply network, the unit comprising
an electricity production device comprising a gas turbine and an electricity generator mechanically connected to an outlet shaft of the gas turbine, said electricity generator including output electrical connections for being electrically connected to an electrical power supply network on board the aircraft;
energy storage means comprising a battery;
regulator means configured to control the speed of rotation of the gas turbine as a function of the electrical power required by the on-board electrical power supply network, the regulator means receiving feedback from the on-board electrical power supply network to control the speed of rotation of the gas turbine as the function of the electrical power required by the on-board electrical power supply network;
second power converter means connected between the energy storage means and the electricity production device, the second power converter means comprising
a mechanical transmission gearbox coupled to the outlet shaft of the gas turbine and including a mechanical coupling shaft, and
an electrical machine mechanically coupled to the mechanical transmission gearbox via the mechanical coupling shaft and electrically coupled to electrical terminals of said energy storage means; and
power management means comprising
a first module configured, in a first mode, to cause at least part of power produced based on operation of the electricity production device to be recovered and stored in said energy storage means, and
a second module configured, in a second mode, to cause the on-board electricity power supply network to be powered by both electricity produced from the gas turbine and energy from the energy storage means when electricity required by the on-board electricity power supply network is greater than a predetermined threshold,
wherein the power management means is configured to
actuate the first module when the speed of rotation of the gas turbine is at a maximum and the level of charge in the energy storage means is below a charge threshold so that the electrical machine delivers energy to the energy storage means, and
actuate the second module when electricity required by the on-board electricity power supply network is greater than the predetermined threshold by using the energy stored by the energy storage means to operate the electrical machine to rotate the outlet shaft of the gas turbine via the mechanical transmission gearbox and the mechanical coupling shaft so as to assist acceleration of the gas turbine.