Engine-control computer and method for detecting failures of such a computer

1. An engine-control computer comprising switches wherein switch voltage type outputs are configured to control some actuators, the computer further comprising a device for detecting internal or external failures with respect to the computer, the device comprising:

a circuit for acquisition of an input voltage of such a switch;

a circuit for acquisition of an output voltage of the switch;

an electrical monitoring circuit wherein first and second inputs are connected respectively to outputs of each of the two circuits, which tests the input and output voltage level of the switch, and delivers an invalid status if the input or output voltage of the switch is less than a defined threshold voltage; and

a circuit for acquisition of current flowing in the switch,

wherein the electrical monitoring circuit includes a third input connected to an output of the circuit for acquisition of the current flowing in the switch, tests a current level and delivers an invalid status if the current is less than a defined limit current and is configured to detect an external failure with respect to the computer, and

wherein the device further comprises:

a discrete state monitoring circuit, wherein an input is connected to the output of the circuit for acquisition of the current flowing in the switch, the discrete state monitoring circuit being configured to determine a state of the switch based on a current level of the current flowing in the switch; and

a deviation monitoring circuit, wherein one input receives an output signal of the discrete state monitoring circuit representative of the state of the switch, and wherein another input receives a discrete request signal representative of a required set-point of the switch, the deviation monitoring circuit being configured to test whether the state of the switch corresponds to the required set-point.

2. The computer according to claim 1 , wherein the device comprises:

an OR gate, wherein one input is connected to the output of the electrical monitoring circuit and wherein another input is connected to the output of the deviation monitoring circuit, and

a confirmation/rehabilitation circuit.

3. The computer according to claim 1 , wherein an electrical status at the output of the electrical monitoring circuit corresponds to a failure if the following test is confirmed:

for a low switch voltage type output current in the switch: i<60 mA AND v<5V;

for a high or very high switch voltage type output current in the switch: i<0.4 A AND v<5V.

4. The computer according to claim 1 , wherein the discrete state status at the output of the discrete state monitoring circuit is considered to be closed if the following test is confirmed:

for a low switch voltage type output current in the switch: i≧60 A;

for a high or very high switch voltage type output current in the switch: i≧0.4 A.

5. The computer according to claim 1 , wherein a deviation status at the output of the deviation monitoring circuit determines that a state of the computer switch is consistent with the discrete request signal:

if the discrete request signal for powering a load of the switch corresponds to supplying the switch voltage type output with the discrete state closed, then the deviation status is no failure;

or if the discrete request signal does not correspond to supplying the switch voltage type output with the discrete state not closed, then the deviation status is no failure;

otherwise, the deviation status indicates a failure.

6. The computer according to claim 1 , which is an aircraft engine-control computer.

7. A method for detecting internal or external failures of an engine-control computer according to claim 1 comprising switches wherein switch voltage type outputs are configured to control some actuators and a device for detecting the failures, the method comprising:

determining if there is a request to supply a load of the switch;

measuring a current flowing in the switch;

measuring a power supply voltage of the switch; and

giving a “failure detected” value if the result of the test [(Ā+ B )·(A+B)]+( B ·C) is equal to 1,

wherein A is equal to 1 if there is a request to supply a load of the switch, and equal to 0 otherwise,

wherein B is equal to 1 if the current flowing in the switch is greater than a defined current threshold, and equal to 0 otherwise, and

wherein C is equal to 1 if the power supply voltage of the switch is less than a defined voltage threshold, and equal to 0 otherwise.