Pressurized-air supply unit for aircraft
A pressurized air supply unit ( 1; 1 ′) for an aircraft, comprising: a load compressor ( 30; 30 ′) configured to supply pressurized air ( 3 ), the load compressor ( 30; 30 ′) having a compressor shaft ( 23; 23 ′); and a drive portion ( 10 ) configured to supply power via an output shaft ( 20 ); the pressurized air supply unit ( 1; 1 ) being characterized in that it comprises: a gearbox ( 50 ); an electric motor ( 40 ), the electric motor ( 40 ) being coupled to said compressor shaft ( 23; 23 ′) via the gearbox ( 50 ); and a coupling system ( 25 ) configured to enable the output shaft ( 20 ) to drive the compressor shaft ( 23; 23 ′) and to prevent the compressor shaft ( 23; 23 ′) from driving the output shaft ( 20 ), and in that the output shaft ( 20 ) and the compressor shaft ( 23 ) lie on the same axis.
1. A pressurized air supply unit for an aircraft, comprising:
a load compressor configured to supply pressurized air, the load compressor comprising a compressor shaft; and
a gas generator configured to supply power via an output shaft;
a gearbox;
an electric motor, the electric motor being coupled to said compressor shaft via the gearbox; and
a coupler configured to enable the output shaft to drive the compressor shaft and to prevent the compressor shaft from driving the output shaft,
wherein the output shaft and the compressor shaft lie on the same axis.
2. The pressurized air supply unit for an aircraft according to claim 1 , wherein the coupler is a non-controlled coupler.
3. The pressurized air supply unit for an aircraft according to claim 2 , wherein the non-controlled coupler includes a freewheel.
4. The pressurized air supply unit for an aircraft according to claim 1 , wherein a portion of the output shaft extends through the compressor shaft.
5. The pressurized air supply unit for an aircraft according to claim 4 , wherein the load compressor is interposed between the gearbox and the gas generator.
6. The pressurized air supply unit for an aircraft according to claim 1 , wherein the gearbox is interposed between the load compressor and the gas generator.
7. The pressurized air supply unit for an aircraft according to claim 1 , wherein the coupler is situated in a casing of the gearbox.
8. The pressurized air supply unit for an aircraft according to claim 1 , wherein the electric motor is a reversible motor capable of producing electricity.
9. An aircraft including the pressurized air supply unit according to claim 1 .
10. The aircraft according to claim 9 , further comprising an on-board source of electricity, the electric motor being configured to receive electricity from said on-board source of electricity.
11. The pressurized air supply unit for an aircraft according to claim 1 , wherein the coupler comprises a clutch.
12. The pressurized air supply unit for an aircraft according to claim 1 , wherein the coupler comprises a roller freewheel.
13. The pressurized air supply unit for an aircraft according to claim 1 , wherein the coupler comprises a freewheel.
14. The pressurized air supply unit for an aircraft according to claim 1 , wherein the coupler comprises a centrifugal throwout freewheel.
15. A method of starting the pressurized air supply unit for an aircraft according to claim 1 , the method comprising the following steps:
starting the gas generator;
increasing a speed of operation of the gas generator until it reaches a desired rotation speed of a shaft of the electric motor; and
starting the electric motor and, simultaneously, stopping the gas generator so as to maintain the desired rotation speed of the shaft of the electric motor substantially constant.