ASSEMBLY FOR STARTING AN ENGINE AND STARTING METHOD

Abstract

An assembly for starting an engine comprises a starter to supply a required starting torque to the engine to start the engine in a starting phase, the starter being subject to dispersions varying the value of the torque supplied, an electronic starting device linked to the starter to supply an electrical current to the starter to electrically power it in the starting phase. The starter comprises a device for characterizing the dispersions of the starter, the electronic starting device is configured to cooperate with the device for characterizing the dispersions of the starter so as to determine the dispersions of the starter, and the electronic starting device is configured to adjust the electrical current supplied to the starter as a function of the determined dispersions to compensate the dispersions of the starter, so that the starter supplies the required starting torque to the engine.

Claims

1. A starting assembly for starting an engine comprising: a starter intended to supply a required starting torque to the engine to start the engine in a starting phase, the starter being subject to dispersions that vary the value of the torque supplied, an electronic starting device linked to the starter and intended to supply an electrical current to the starter to electrically power it in the starting phase, wherein the starter comprises a device for characterizing the dispersions of the starter comprising a means for storing a dispersion indicator, wherein the electronic starting device comprises a means for reading the dispersion indicator and is configured to read the dispersion indicator so as to determine the dispersions of the starter, and wherein the electronic starting device is configured to supply the electrical current to the starter as a function of the determined dispersions to compensate the dispersions of the starter, so that the starter supplies the required starting torque to the engine.

2. The starting assembly according to claim 1, wherein the dispersion indicator of the storage means is a value defined prior to a use of the starting assembly.

3. The starting assembly according to claim 1, wherein the device for characterizing the dispersions of the starter is a passive analogue device.

4. The starting assembly according to claim 1, wherein the means for storing a dispersion indicator is an ohmic conductor, and wherein the dispersion indicator is a resistance value.

5. The starting assembly according to claim 1, the dispersions of the starter being previously estimated and/or measured, wherein the dispersion indicator is predefined in conformity with the estimated and/or measured dispersions of the starter.

6. The starting assembly according to claim 1, wherein the device for characterizing the dispersions of the starter is a digital device.

7. An aircraft, comprising a starting assembly according to claim 1, wherein the engine is a propulsion engine of the aircraft and/or an auxiliary power engine of the aircraft.

8. A method for starting an engine implementing a starting assembly according to claim 1, comprising the following steps: determining the dispersions of the starter by the electronic starting device, adjusting the electrical current supplied to the starter as a function of the determined dispersions to compensate the dispersions of the starter, supplying the required starting torque to the engine for the starting of the engine by the starter.

9. The method for starting an engine according to claim 8, further comprising beforehand, the following steps performed just once: estimating and/or measuring the dispersions of the starter, and predefining the dispersion indicator in conformity with the estimated and/or measured dispersions of the starter.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0039] The invention will be better understood and other advantages will emerge on reading the detailed description of an embodiment given by way of example, the description being illustrated by the attached drawings in which:

[0040] FIG. 1 represents an engine starting assembly according to the invention;

[0041] FIG. 2 represents an embodiment of a starting assembly according to the invention;

[0042] FIG. 3 schematically illustrates the steps of a starting method according to the invention;

[0043] FIG. 4 schematically represents an aircraft comprising a starting assembly according to the invention.

DETAILED DESCRIPTION

[0044] In the interests of clarity, the same elements will bear the same references in the different figures. It should be noted that the invention applies to any type of starter-generator, whether with permanent magnets or with a wound rotor provided with a ring-brush system with DC excitation or brushless with single-phase or three-phase, or more generally polyphase, AC excitation. The invention is presented with the example of a starter-generator but it applies to any type of not necessarily current-generating synchronous or asynchronous starter.

[0045] FIG. 1 represents an assembly 10 for starting an engine 11 according to the invention. The assembly 10 for starting the engine 11 comprises a starter 12, for example a starter-generator, intended to supply a required starting torque to the engine 11 to start the engine 11 in a starting phase, the starter 12 being subject to dispersions that vary the value of the torque supplied. The assembly 10 for starting the engine 11 comprises an electronic starting device 13 linked to the starter 12 and intended to supply an electrical current to the starter 12 to electrically power it in the starting phase. According to the invention, the starter 12 comprises a device 14 for characterizing the dispersions of the starter 12, and the electronic starting device 13 is configured to cooperate with the device 14 for characterizing the dispersions of the starter 12 so as to determine the dispersions of the starter 12. Finally, the electronic starting device 13 is configured to adjust the electrical current supplied to the starter 12 as a function of the determined dispersions to compensate the dispersions of the starter 12, so that the starter 12 supplies the required starting torque to the engine 11. The required starting torque is a fixed starting torque which corresponds to the minimum torque to be supplied by the starter to ensure the starting of the engine.

[0046] The device 14 for characterizing the dispersions of the starter 12 comprises a means 15 for storing a dispersion indicator, and the electronic starting device 13 comprises a means 16 for reading the dispersion indicator.

[0047] The dispersion indicator of the storage means 15 can be a value defined prior to a use of the starting assembly 10, for example +5% or 10% or 12 Nm.

[0048] In other words, the invention makes it possible to group together all the construction dispersions of the starter in a device for characterizing same and to use same to be able to compensate them by the current in the starting of the engine. That makes it possible to reach the specified minimum starting torque in all cases. The current can be supplied by an inverter. The inverter is dimensioned so as to be able to supply the current needed to compensate the torque deficit of the least powerful starter. That makes it possible to avoid an overdimensioning (weight) of the starter to guarantee the torque requirement, on the one hand, and to reduce the dispersions of torque supplied on the other hand.

[0049] The starting assembly according to the invention allows the starter and inverter assembly to supply a fixed specified minimum torque, independently of the thermal state, and do so in order to minimize the weight of the starter. In other words, the invention makes it possible to produce a fixed given torque regardless of the construction dispersions of the starter itself, outside of the thermal aspects of the engine to be started and of the associated electronics.

[0050] According to the invention, the models and parameters of the starter are determined by computation and the models are established in the inverter, and it is only the uncertainties of construction of the starter, including the accuracy of the position coder, which are grouped together with a single value datum subsequently processed by the inverter. On an aeroplane, the inverter can be associated with any starter. Also the case on an aeroplane is that the same inverter is used to control the two starters of the two engines having different dispersions.

[0051] According to the embodiment considered, the device 14 for characterizing the dispersions of the starter 12 can be a passive analogue device or a digital device. In the case where the device 14 for characterizing the dispersions of the starter 12 is a digital device, it can for example be a ROM memory, a flash memory, an SSD disc, an RFID chip or any other medium capable of storing a dispersion indicator. The electronic starting device 13 is then configured to cooperate with the device 14 for characterizing the dispersions of the starter 12 so as to determine the dispersions of the starter 12. In other words, the starting device 13 then comprises a reading device capable of reading the dispersion indicator on the characterization device 14. Once the dispersion indicator is read by the electronic starting device 13, the electronic starting device 13 is then able to adjust the electrical current supplied to the starter 12 as a function of the dispersions to compensate the dispersions of the starter 12. Thus, the starter 12 supplies the required starting torque to the engine 11. In other words, the starter 12 is thus able to supply the engine 11 with a starting torque at least equal to the minimum torque required to ensure the starting of the engine 11. During the starting, the inverter reads the dispersion value and determines the current by a corrective factor associated with the dispersion value read in order to guarantee the specified minimum torque. The result therefore is a good modularity in the combination of an engine and of an inverter. It is possible to change the inverter without having to associate other additional data therewith since the inverter only reads the dispersion value.

[0052] FIG. 2 represents a particular embodiment of a starting assembly 20 according to the invention. The starting assembly 20 of the engine 11 represented in FIG. 2 comprises the same elements as the starting assembly 10 represented in FIG. 1. The difference lies in the device for characterizing the dispersions of the starter 12. In FIG. 2, the device 140 for characterizing the dispersions of the starter is a passive analogue device. More specifically, the means for storing the dispersion indicator is an ohmic conductor, and the dispersion indicator is a resistance value. The dispersions of the starter 12 are estimated and/or measured beforehand, and the dispersion indicator is predefined in conformity with the estimated and/or measured dispersions of the starter 12. During the process of manufacturing the starter 12, for example a starter-generator, tests are performed to identify the parameters influencing the torques supplied by the starter 12. It is then possible, as a function of the operating parameters provided for the starter 12 such as the different tolerances on the impedances of the rotor and of the stator, etc., to estimate the dispersions that the starter 12 will have in use. The dispersions can also be estimated using empirical formulae known to the manufacturer of the starter, by taking into account the operating parameters provided for the starter. Also, the dispersions of the starter can be determined jointly by measurements and estimations.

[0053] The estimated and/or measured dispersions are then stored in the characterization device 140 through a dispersion indicator.

[0054] In the embodiment of FIG. 2, an ohmic conductor is incorporated in the starter 12. This ohmic conductor has a certain resistance chosen in conformity with the estimated and/or measured dispersions prior to a use of the starter 12. For example, for an estimated dispersion of 6%, the resistance can for example have a value of 1 k (kilo-ohm). The electronic starting device 13, configured to cooperate with the device 14 for characterizing the dispersions of the starter 12, reads the value of the resistance and understands that it has to supply it with a current adapted to compensate the 6% of dispersions of the starter 12 in order for the starter, despite its 6% of dispersions, to be able to supply the minimal torque necessary to start the engine 11.

[0055] By proceeding according to the principle of the invention, there is an assurance that the starter delivers the torque required to start the engine, despite the dispersions of the starter. Compared to the prior art and as explained previously, it is therefore no longer necessary to use as torque reference a reference torque Cref corresponding to the required minimum torque Cmin multiplied by a gain in order to compensate the possible dispersions. The invention therefore allows for a saving in terms of cost, of weight and of volume since the equipment such as the starter, the electronic starting device and all the cables, are no longer overdimensioned relative to their size necessary to the correct operation of the starter during the starting.

[0056] FIG. 3 schematically illustrates the steps of a starting method according to the invention. The method according to the invention comprises a step 202 of determination of the dispersions of the starter 12 by the electronic starting device 13. Then, the method comprises a step 203 of adjustment of the electrical current supplied to the starter 12 as a function of the determined dispersions to compensate the dispersions of the starter 12. Finally, the method according to the invention comprises a step 204 of supply of the required starting torque to the engine 11 by the starter 12 for the starting of the engine 11. By virtue of the method according to the invention, the starter 12 safely and certainly supplies the minimum torque required for the starting of the engine 11 since the electronic starting device 13 is informed of the dispersions of the starter 12 and supplies appropriate electrical current to the starter 12 for the latter to supply the appropriate mechanical torque.

[0057] The method for starting an engine 11 comprises, beforehand, the steps 200 and 201 performed just once. During the manufacturing of the starter 12, the step 200 of estimation and/or of measurement of the dispersions of the starter 12, and the step 201 of predefinition of the dispersion indicator in conformity with the estimated and/or measured dispersions of the starter 12, take place.

[0058] FIG. 4 schematically represents an aircraft 50 comprising a starting assembly 10, 20 according to the invention. The aircraft 50 comprises a starting assembly 10, 20 as described previously. The engine 11 is a propulsion engine of the aircraft 50 and/or an auxiliary power engine of the aircraft 50.