Electronic operational control device for a piloting member with cross-monitoring, piloting device and aircraft
First Claim
1. An electronic operational control device for a controlled piloting member of an aircraft piloting device including said controlled piloting member and another piloting member, the two piloting members both being connected to at least one same flying member of an aircraft, said controlled piloting member being mounted on a first electromechanical supporting box with at least one degree of freedom, the first electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate the controlled piloting member, said other piloting member being mounted on a second electromechanical supporting box with at least one degree of freedom, said second electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate said other piloting member, the electronic operational control device comprising:
- main monitoring inputs configured to receive signals delivered by sensors associated with the controlled piloting member;
electronic main monitoring circuits configured to digitally process the signals received at the main monitoring inputs and to detect any deviation of the signals corresponding to an operating fault and to generate a signal representing the operating fault;
cross-monitoring inputs configured to receive cross-monitored signals delivered by sensors associated with the other piloting member; and
at least one cross-monitoring electronic circuit configured to digitally process said cross-monitored signals delivered by the sensors associated with the other piloting member, said cross-monitoring circuit being configured to detect any deviation of said cross-monitored signals corresponding to the operating fault and to generate a signal representing the operating fault,wherein the device is encapsulated in a box adapted to be able to be mounted on said electromechanical supporting box of the controlled piloting member,the two piloting members are movable with the same degrees of freedom with respect to a frame of the aircraft, one of the cross-monitoring circuits being specific to each degree of freedom,for each degree of freedom of the controlled piloting member and of the other piloting member, the main monitoring circuit comprises a first electronic microcontroller configured to digitally process the signals delivered by the sensors associated with the controlled piloting member, andthe cross-monitoring circuit comprises another electronic microcontroller which processes the signals delivered by the sensors associated with the other piloting member, each other electronic microcontroller being distinct from said first electronic microcontroller.
1 Assignment
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Accused Products
Abstract
An electronic operational control device for an aircraft piloting device with two connected piloting members, includes electronic circuits for main monitoring from signals delivered by sensors associated with one of the piloting members, and at least one electronic circuit (52 to 55) for cross-monitoring, for digital processing of signals delivered by sensors (83, 93) associated with the other piloting member, adapted to detect any deviation of these signals corresponding to a fault and to generate a signal representing such a fault. A piloting device and an aircraft including such an electronic operational control device with cross-monitoring are also disclosed.
17 Citations
33 Claims
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1. An electronic operational control device for a controlled piloting member of an aircraft piloting device including said controlled piloting member and another piloting member, the two piloting members both being connected to at least one same flying member of an aircraft, said controlled piloting member being mounted on a first electromechanical supporting box with at least one degree of freedom, the first electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate the controlled piloting member, said other piloting member being mounted on a second electromechanical supporting box with at least one degree of freedom, said second electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate said other piloting member, the electronic operational control device comprising:
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main monitoring inputs configured to receive signals delivered by sensors associated with the controlled piloting member; electronic main monitoring circuits configured to digitally process the signals received at the main monitoring inputs and to detect any deviation of the signals corresponding to an operating fault and to generate a signal representing the operating fault; cross-monitoring inputs configured to receive cross-monitored signals delivered by sensors associated with the other piloting member; and at least one cross-monitoring electronic circuit configured to digitally process said cross-monitored signals delivered by the sensors associated with the other piloting member, said cross-monitoring circuit being configured to detect any deviation of said cross-monitored signals corresponding to the operating fault and to generate a signal representing the operating fault, wherein the device is encapsulated in a box adapted to be able to be mounted on said electromechanical supporting box of the controlled piloting member, the two piloting members are movable with the same degrees of freedom with respect to a frame of the aircraft, one of the cross-monitoring circuits being specific to each degree of freedom, for each degree of freedom of the controlled piloting member and of the other piloting member, the main monitoring circuit comprises a first electronic microcontroller configured to digitally process the signals delivered by the sensors associated with the controlled piloting member, and the cross-monitoring circuit comprises another electronic microcontroller which processes the signals delivered by the sensors associated with the other piloting member, each other electronic microcontroller being distinct from said first electronic microcontroller. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. An electronic operational control device for a controlled piloting member of an aircraft piloting device including said controlled piloting member and another piloting member, the two piloting members both being connected to at least one same flying member of an aircraft, the two piloting members being sticks movable with respect to a frame of the aircraft on a longitudinal horizontal pivot axis to enable a roll command, said controlled piloting member being mounted on a first electromechanical supporting box with at least one degree of freedom, the first electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate the controlled piloting member, said other piloting member being mounted on a second electromechanical supporting box with at least one degree of freedom, said second electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate said other piloting member, the electronic operational control device comprising:
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main monitoring inputs configured to receive signals delivered by sensors associated with the controlled piloting member; electronic main monitoring circuits configured to digitally process the signals received at the main monitoring inputs and to detect any deviation of the signals corresponding to an operating fault and to generate a signal representing the operating fault; cross-monitoring inputs configured to receive cross-monitored signals delivered by sensors associated with the other piloting member; at least one cross-monitoring electronic circuit configured to digitally process said cross-monitored signals delivered by the sensors associated with the other piloting member, said cross-monitoring circuit being configured to detect any deviation of said cross-monitored signals corresponding to the operating fault and to generate a signal representing the operating fault; roll main monitoring inputs configured to receive signals delivered by at least one roll angular position sensor of the controlled piloting member, and by at least one roll force sensor of the controlled piloting member; roll cross-monitoring inputs configured to receive cross-monitored signals delivered by at least one roll position sensor of the other piloting member, and by at least one roll force sensor of the other piloting member; and a roll cross-monitoring circuit configured to determine for each piloting member a theoretical force value according to at least one predetermined law from at least roll angular position signals of the piloting member, compare the theoretical force value with a measured force value delivered by at least one roll force sensor of a piloting member, and generate the operating fault signal when a difference between the values is, as an absolute value, greater than a predetermined threshold value, wherein the device is encapsulated in a box adapted to be able to be mounted on said electromechanical supporting box of the controlled piloting member, and the two piloting members are movable with the same degrees of freedom with respect to a frame of the aircraft, one of the cross-monitoring circuits being specific to each degree of freedom. - View Dependent Claims (14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 26, 27, 30, 31, 32)
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24. An electronic operational control device for a controlled piloting member of an aircraft piloting device including said controlled piloting member and another piloting member, the two piloting members both being connected to at least one same flying member of an aircraft, the two piloting members being sticks movable with respect to a frame of the aircraft on a transverse horizontal pivot axis to enable a pitch command, said controlled piloting member being mounted on a first electromechanical supporting box with at least one degree of freedom, the first electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate the controlled piloting member, said other piloting member being mounted on a second electromechanical supporting box with at least one degree of freedom, said second electromechanical supporting box including, for each degree of freedom, at least one motor configured to actuate said other piloting member, the electronic operational control device comprising:
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main monitoring inputs configured to receive signals delivered by sensors associated with the controlled piloting member; electronic main monitoring circuits configured to digitally process the signals received at the main monitoring inputs and to detect any deviation of the signals corresponding to an operating fault and to generate a signal representing the operating fault; cross-monitoring inputs configured to receive cross-monitored signals delivered by sensors associated with the other piloting member; at least one cross-monitoring electronic circuit configured to digitally process said cross-monitored signals delivered by the sensors associated with the other piloting member, said cross-monitoring circuit being configured to detect any deviation of said cross-monitored signals corresponding to the operating fault and to generate a signal representing the operating fault; pitch main monitoring inputs configured to receive signals delivered by at least one pitch position sensor of the controlled piloting member, and by at least one pitch force sensor of the controlled piloting member; pitch cross-monitoring inputs configured to receive cross-monitored signals delivered by at least one pitch position sensor of the other piloting member, and at least one pitch force sensor of the other piloting member; and a pitch cross-monitoring circuit configured to determine for each piloting member, a theoretical force value according to at least one predetermined law from at least pitch angular position signals of the piloting member, compare the theoretical force value with a measured force value delivered by at least one pitch force sensor of a piloting member, and generate the operating fault signal when a difference between the values is, as an absolute value, greater than a predetermined threshold value, wherein the device is encapsulated in a box adapted to be able to be mounted on said electromechanical supporting box of the controlled piloting member, and the two piloting members are movable with the same degrees of freedom with respect to a frame of the aircraft, one of the cross-monitoring circuits being specific to each degree of freedom. - View Dependent Claims (25, 28, 29, 33)
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Specification