The present invention relates to an electromechanical motor vehicle power steering mechanism having the features of the preamble of claim 1.
In an electric power steering apparatus the steering assist force is applied to a steering mechanism by driving an electric motor in accordance with steering torque that is applied to a steering wheel by a driver.
Usually, the control of the electric motor is carried out using electronic components. Electronic components can fail abruptly. In this case the steering assist force is no longer present which is uncomfortable for the driver.
The published patent application DE 10 2010 050 818 A1 describes a fail-safe unit which supplies power to the motor even if one of two separate power supply units fails. The power supply units are completely independent from each other. A disadvantage of this solution is that a synchronisation unit is needed, which in the event of failure cannot guarantee power supply to the motor. Further, redundancy means undesired multiple component cost and board area.
It is object of the present invention to provide an improved redundant power supply to an electric motor of an electric power steering apparatus, while keeping the number of components at a minimum to save cost and space.
This object is achieved by an electromechanical motor vehicle power steering mechanism having the features of claim 1.
Accordingly, an electromechanical motor vehicle power steering mechanism with an electric motor providing a steering assist force and a control unit controlling the current to the electric motor are provided, whereas the control unit includes two redundant power supply units each connected to a vehicle battery, whereas the two power supply units each comprise a primary winding and a secondary winding as part of a flyback transformer with a shared magnetic core. By sharing the magnetic core of the flyback transformer cost and space can be reduced clearly.
It is also possible that the power supply units are connected to one common vehicle battery or each power supply unit are connected to separate vehicle batteries in order to provide power supply to the electric motor.
It is advantageous if the magnetic core has two air gaps forming two independent closed flux lines for each of the power supply units, so that the power supply units can act independently from each other.
In a preferred embodiment, the magnetic core of the transformer is e-shaped with a middle leg and two side legs, whereas the primary winding and the secondary winding of one power supply unit are wound around one side leg, respectively. Preferably, the two air gaps are formed between the two ends of the side legs and the middle leg. Thereby it is advantageous, if the middle leg is t-shaped.
It is preferred, that the electric motor is a permanently excited electric motor including at least three phase windings.
Favourably, the two power supply units each comprise of a flyback controller, a flyback driver circuit, a closed-loop controller, a closed-loop controller and a motor driver.
An exemplary embodiment of the present invention is described below with aid of the drawings. In all figures the same reference signs denote the same components or functionally similar components.
In
The control unit 9 is illustrated in detail in
At specific intervals set by the flyback controller 17, 117, the primary winding 19, 119 of the flyback transformer 16 is driven by the flyback driver circuit 18, 118 from the battery 15, 115. The primary inductance causes the current to build up in a ramp. When the DC supply of the primary winding 19, 119 is shut off, the current in the primary winding 19, 119 collapses leaving the energy stored in the magnetic core 24 of the flyback controller 17, 117 and the stored energy is transferred to the closed-loop controller 21, 210 via the secondary winding 20, 200 supplying the closed-loop controller 22, 220 with power. The flyback transformer 16 is preferably operated in discontinuous mode; the energy stored in the magnetic core 24, which is in the example a ferrite core but could also be an iron core, is completely emptied from the core 24 during the flyback period. The cycle is then repeated. The interval connecting the primary winding 19, 119 to the supply of direct current is determined from various measured signals e.g. input voltage, output voltage, primary current.
The redundant power supply units A, B share the ferrite core 24 of the flyback transformer 16. To make them independent, each part needs its own air gap, where the energy for the given part is stored. This way there is negligible influence and disturbance between the power supply units using the same core 24.
In event of fault, determined by a flyback controller 17, 117, the respective flyback driver circuit 18, 118 is continuously deactivated. Power will continue to flow via the redundant functional and error-free flyback driver circuit 18, 118. The independence between the two power supply units A, B is given by the decoupled side legs 28 of the shared ferrite core 24, eliminating energy coupling between the two redundant power supply units A, B.
According to the invention, the energy density of a magnetic core is used for multiple parts of the circuitry. To make them independent, each part has its own air gap, where the energy for the given part is stored. This way there is negligible influence and disturbance between the circuits using the same core. The magnetic core is preferably shared by two power supply units each supplying energy to an own controller, which is controlling the motor drivers signals to the electric motor.
The power inductor in a power supply is both expensive and large. The most costly part is the ferrite material and one of the biggest parts is the ferrite core. By sharing the magnetic core between the redundant power supply units, cost and space can be saved.
The present invention is not dependent on the specific design of the steering mechanism or limited to the number of controllers and number of transformer windings.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2015/065586 | 7/8/2015 | WO | 00 |