Self-calibration method for the electric jacks of a turbojet nacelle
The invention relates to a method for the self-calibration of electric jacks ( 6 a, 6 b ) capable of actuating a mobile member ( 2 ) of a turbojet nacelle ( 1 ) and connected to at least one position measuring member, characterized in that it comprises the steps of: moving the jack(s) into a retracted position corresponding to a first position of the mobile member, storing one or more position values fed back by the position measuring member for the jack(s) in said retracted position; moving the jack(s) into an extended position corresponding to a second position of the mobile member; storing one or mom position values fed back by the position measuring member for the jack(s) in said extended position.
1. A method of self-calibration of a mobile cowl of a thrust reverser of a turbojet engine nacelle comprising at least one electric jack associated with at least one position-measuring member, the method comprising:
bringing the mobile cowl and the associated jack or jacks into a retracted position, corresponding to a first position of the mobile cowl,
setting up an electric stop by logging one or more position values of the associated jack or jacks returned by the position-measuring member or members in said retracted position,
bringing the mobile cowl and the associated jack or jacks into a deployed position, corresponding to a second position of the mobile cowl, and
setting up an electric stop by logging one or more position values of the associated jack or jacks returned by the position-measuring member in said deployed position, wherein the self-calibration is carried out during installation or maintenance operations such that in a flight operation, a deployed position and a retracted position of the associated jack or jacks are defined by said electric stops that are defined on the basis of actual mechanical stops of the mobile cowl and the associated jack or jacks.
2. The method as claimed in claim 1 , wherein the jack or jacks are actuated manually.
3. The method as claimed in claim 1 , wherein the jack or jacks are actuated electrically.
4. The method as claimed in claim 3 , wherein the retracted and deployed positions of the jacks are detected automatically by detecting mechanical stops.
5. The method as claimed in claim 4 , wherein the detection of the mechanical stops is performed by measuring variation in current drawn by an electric motor actuating the jack or jacks.
6. The method as claimed in claim 4 , wherein the detection of the stops is performed by measuring a rate at which the jacks deploy or retract.
7. The method as claimed in claim 6 , wherein the rate of deployment or of retraction is obtained by differentiating a position value returned by a position-measuring member.
8. The method as claimed in claim 1 , wherein the position-measuring member is a resolver.
9. The method as claimed in claim 1 , wherein the logged retracted and deployed position values are corrected by applying a margin of error.
10. A thrust reverser comprising at least one moving cowl that can be moved under action of at least one electromechanical member of the electric jack type, wherein it comprises an instrumentation and control interface capable of implementing a method as claimed in claim 1 .
11. The reverser as claimed in claim 10 , wherein the control interface is connected to a turbojet engine control unit and in the self-calibration method can be activated from a cockpit.