Electric charger for aeronautical maintenance equipment
The invention concerns a charger for aeronautical maintenance equipment, the charger comprising at least one so-called “high-frequency” input electrical connector comprising a plurality of power supply pins capable of receiving a three-phase AC voltage delivered by an external power supply source at a frequency of 400 Hz, and two detection pins, a so-called “high-frequency” charging module, connected to the at least one high-frequency input electrical connector, intended to be connected to a power storage module of the aeronautical maintenance equipment, and capable of converting the AC voltage received at the plurality of power supply pins of the high-frequency input electrical connector into a DC voltage for charging the storage module, and a control module capable of generating a detection voltage between the detection pins of the high-frequency input electrical connector allowing the external power supply source, when it detects the detection voltage, to authorize the supply of the AC voltage to the plurality of power supply pins of the high-frequency input electrical connector.
1 . A charger for aeronautical maintenance equipment, said charger comprising:
at least one high-frequency input electrical connector comprising a plurality of supply pins able to receive a three-phase AC voltage delivered by an external power source at a frequency of 400 Hz, and two detection pins,
a high-frequency charging module connected to said at least one high-frequency input electrical connector and for being connected to an electric energy storage module of said aeronautical maintenance equipment, said high-frequency charging module configured to convert the AC voltage received on the plurality of power supply pins of the at least one high-frequency input electrical connector into a direct current voltage to charge said storage module,
a control module configured to generate a detection voltage across the detection pins of the at least one high-frequency input electrical connector for the external power source, upon detecting said detection voltage, to allow supply of the AC voltage to the plurality of supply pins of the at least one high-frequency input electrical connector, and
wherein the control module is configured to receive a set point from a monitoring module of the storage module and to regulate the DC voltage supplied by the high-frequency charging module depending on said set point.
2 . The charger according to claim 1 , wherein the at least one high-frequency input electrical connector comprises a plurality of high-frequency input electrical connectors.
3 . The charger according to claim 1 , wherein the high-frequency charging module comprises a rectifier and a step-up converter.
4 . The charger according to claim 1 , comprising:
at least one low-frequency input electrical connector distinct from the at least one high-frequency input electrical connector and configured for receiving a single-phase or three-phase AC voltage delivered by an external power source at a frequency of between 45 and 65 Hz,
a low-frequency charging module, connected to the at least one low-frequency input electrical connector and for being connected to the storage module, said low-frequency charging module configured for converting the AC voltage received on the at least one low-frequency input electrical connector into a DC voltage for charging the storage module.
5 . The charger according to claim 4 , wherein the low-frequency charging module and the high-frequency charging module are implemented by a same physical entity in a single low-frequency or high-frequency charging module.
6 . The charger according to claim 5 , wherein the control module is configured to detect connection of an external power source to the at least one high-frequency input electrical connector or to the at least one low-frequency input electrical connector and to adapt operation of the low-frequency or high-frequency charging module depending on the frequency of the AC voltage provided on the input electrical connector detected.
7 . The charger according to claim 4 , wherein the low-frequency charging module and the high-frequency charging module are implemented by two distinct physical entities.
8 . The charger according to claim 7 , wherein the control module is configured to detect connection of an external power source to the at least one high-frequency or low-frequency input electrical connector and to electrically connect the at least one low-frequency input electrical connector to the low-frequency charging module when the connection has been detected on the at least low frequency input electrical connector or the at least one high-frequency input electrical connector to the high-frequency charging module when the connection has been detected on the at least one high-frequency input electrical connector.
9 . The charger according to claim 1 , wherein the control module is configured to determine or receive charging power information from the external power source and to adapt the charging current of the storage module based on said charging power information.
10 . An aeronautical maintenance equipment for use in an aeronautical zone, said aeronautical maintenance equipment comprising:
the charger according to claim 1 ,
a storage module, connected to said charger, configured to store electric energy when said storage module is supplied with a DC voltage delivered by said charger.
11 . The aeronautical maintenance equipment according to claim 10 , comprising a power generation module, connected to the storage module, configured to produce a high-frequency or low-frequency DC or AC voltage from a fuel or a fuel cell in order to recharge the storage module.
12 . A system comprising the aeronautical maintenance equipment, according to claim 10 , and an external power source, electrically connected to said aeronautical maintenance equipment, said external power source being able to deliver a single-phase or three-phase 50 or 60 Hz or three-phase 400 Hz AC voltage, to charge the storage module of the aeronautical maintenance equipment via the charger of said aeronautical maintenance equipment.
13 . A method for charging an electric energy storage module of the aeronautical maintenance equipment, according to claim 10 , by an external power source capable of delivering a three-phase AC voltage delivered at a frequency of 400 Hz, said method comprising the steps of:
electrically connecting the external power source to the at least one high-frequency input electrical connector of the charger of the aeronautical maintenance equipment so as to deliver a three-phase AC voltage at a frequency of 400 Hz,
converting, by the high-frequency charging module of the charger of the aeronautical maintenance equipment, said AC voltage into a DC voltage,
charging the storage module of the aeronautical maintenance equipment from said DC voltage.
14 . A charger for aeronautical maintenance equipment, said charger comprising:
at least one high-frequency input electrical connector comprising a plurality of supply pins able to receive a three-phase AC voltage delivered by an external power source at a frequency of 400 Hz, and two detection pins,
a high-frequency charging module connected to said at least one high-frequency input electrical connector and for being connected to an electric energy storage module of said aeronautical maintenance equipment, said high-frequency charging module configured to convert the AC voltage received on the plurality of power supply pins of the at least one high-frequency input electrical connector into a direct current voltage to charge said storage module,
a control module configured to generate a detection voltage across the detection pins of the at least one high-frequency input electrical connector for the external power source, upon detecting said detection voltage, to allow supply of the AC voltage to the plurality of supply pins of the at least one high-frequency input electrical connector, and
wherein the at least one high-frequency input electrical connector comprises a plurality of high-frequency input electrical connectors.
15 . The charger according to claim 14 , wherein the high-frequency charging module comprises a rectifier and a step-up converter.
16 . The charger according to claim 14 , wherein the control module is configured to determine or receive charging power information from the external power source and to adapt the charging current of the storage module based on said charging power information.
17 . A charger for aeronautical maintenance equipment, said charger comprising:
at least one high-frequency input electrical connector comprising a plurality of supply pins able to receive a three-phase AC voltage delivered by an external power source at a frequency of 400 Hz, and two detection pins,
a high-frequency charging module connected to said at least one high-frequency input electrical connector and for being connected to an electric energy storage module of said aeronautical maintenance equipment, said high-frequency charging module configured to convert the AC voltage received on the plurality of power supply pins of the at least one high-frequency input electrical connector into a direct current voltage to charge said storage module,
a control module configured to generate a detection voltage across the detection pins of the at least one high-frequency input electrical connector for the external power source, upon detecting said detection voltage, to allow supply of the AC voltage to the plurality of supply pins of the at least one high-frequency input electrical connector, and
wherein the high-frequency charging module comprises a rectifier and a step-up converter.
18 . The charger of claim 17 , wherein the control module is configured to receive a set point from a monitoring module of the storage module and to regulate the DC voltage supplied by the high-frequency charging module depending on said set point.
19 . The charger according to claim 17 , wherein the at least one high-frequency input electrical connector comprises a plurality of high-frequency input electrical connectors.