Electric jack comprising stress-limiting means and space launcher comprising a nozzle supported by such a jack

1. An electromechanical actuator, for moving a first element with respect to a second element, the actuator comprising:

a movable member ( 14 ) provided with connecting means for being attached to said first element,

a frame provided with attaching means for being attached to said second element,

a driving unit which drives the movable member in translation relative to said frame, and

at least one mechanical energy absorbing-dissipating structure located on a strain path between said first element and a surface of said frame of the actuator, said at least one mechanical energy absorbing-dissipating structure comprising:

a deformable chamber containing at least one porous capillary matrix having open pores and an associated liquid having a wetting angle higher than 90 degrees relative to said matrix and selected such that at least part of said liquid penetrates the pores of said matrix, when an external mechanical pressure applied to the chamber is equal to or higher than a first pressure level PI, and is spontaneously rejected off the pores of said matrix by capillary action, when said external mechanical pressure applied to the chamber is lower than a second pressure level P2 which is lower than said first pressure level P1 such that the at least one energy absorbing-dissipating structure limits a level of strains which may be transmitted to the frame of the electromechanical actuator by the first element via the movable member of the electromechanical actuator,

wherein said movable member is in said strain path and said external mechanical pressure applied to said deformable chamber is a sum of forces applied to said movable member by said driving unit and an external strain applied to said first element.

2. The actuator according to claim 1 , wherein the at least one energy absorbing-dissipating structure of the actuator is accommodated inside a cavity through which said movable member of the actuator passes at least partly, and is interposed between a wall of said cavity and strain transmitting means which are configured to exert a pressure against the deformable chamber of said at least one energy absorbing-dissipating structure for transmitting strains between said first element and said frame of the actuator.

3. The actuator according to claim 2 , wherein said strain transmitting means are carried by said movable member.

4. The actuator according to claim 3 , wherein said connecting means ( 20 ) of said movable member ( 14 ) to said first element comprise a hollow body ( 24 ) slidingly mounted on said movable member ( 14 ) and inside which said cavity ( 26 ) is provided.

5. The actuator according to claim 3 , wherein said frame comprises a hollow body inside which said cavity is provided and wherein the driving unit for driving said movable member is fixedly accommodated in said cavity.

6. The actuator according to claim 5 , wherein said strain transmitting means comprise one or more plates respectively cooperating with the at least one energy absorbing-dissipating structure and each arranged between said driving unit and said corresponding energy absorbing-dissipating structure.

7. The actuator according to claim 2 , wherein said frame ( 12 ) comprises a hollow body ( 54 ) inside which said cavity ( 26 ) is provided, and wherein said strain transmitting means ( 60 , 62 ) aid in supporting the driving unit ( 16 ) for driving said movable member ( 14 ) inside said cavity ( 26 ).

8. The actuator according to claim 2 , further comprising a second mechanical energy absorbing-dissipating structures located on a respective strain path between said first element and the surface of said frame of the actuator and comprising a second deformable chamber containing at least one porous capillary matrix having open pores and an associated liquid having a wetting angle higher than 90 degrees relative to said matrix and selected such that at least part of said liquid penetrates the pores of said matrix, when a second external mechanical pressure applied to said second chamber is higher than a third pressure level P3, and is spontaneously rejected off the pores of said matrix by capillary action, when said second external mechanical pressure applied to said second chamber is lower than a fourth pressure level P4 which is lower than said third pressure level P3, said at least one energy absorbing-dissipating structure and said second mechanical energy absorbing-dissipating structure being provided on either side of said strain transmitting means such that said first element can bias said structures in two respective opposite directions.

9. The actuator according to claim 1 , wherein the force applied by the driving unit is zero.

10. An engine for a space launcher, including

at least one jet nozzle, and

at least one electromechanical actuator for moving a first element with respect to a second element, said at least one electromechanical actuator comprising:

a movable member ( 14 ) provided with connecting means for being attached to said first element,

a frame provided with attaching means for being attached to said second element, wherein said movable member is translationally movable with respect to said frame,

a driving unit which drives the movable member in translation, and

at least one mechanical energy absorbing-dissipating structure located on a strain path between said first element and said frame of the actuator, said at least one mechanical energy absorbing-dissipating structure comprising:

a deformable chamber containing at least one porous capillary matrix having open pores and an associated liquid having a wetting angle higher than 90 degrees relative to said matrix and selected such that at least part of said liquid penetrates the pores of said matrix, when an external mechanical pressure applied to the chamber is equal to or higher than a first pressure level PI, and is spontaneously rejected off the pores of said matrix by capillary action, when said external mechanical pressure applied to the chamber is lower than a second pressure level P2 which is lower than said first pressure level P1 such that the at least one energy absorbing-dissipating structure limits a level of strains which may be transmitted to the frame of the electromechanical actuator by the first element via the movable member of the electromechanical actuator,

wherein said movable member is in said strain path and said external mechanical pressure applied to said deformable chamber is a sum of forces applied to said movable member by said driving unit and an external strain applied to said first element.

11. The engine according to claim 10 , wherein the force applied by the driving unit is zero.

12. A space launcher, comprising at least one engine including:

at least one jet nozzle, and

at least one electromechanical actuator for moving a first element with respect to a second element, the at least one electromechanical actuator comprising:

a movable member provided with connecting means for being attached to said first element,

a frame provided with attaching means for being attached to said second element, wherein said movable member is translationally movable with respect to said frame,

a driving unit which drives the movable member in translation, wherein said actuator; and

at least one mechanical energy absorbing-dissipating structure located on a strain path between said first element and said frame of the actuator, the at least one mechanical energy absorbing-dissipating structure comprising

a deformable chamber containing at least one porous capillary matrix having open pores and an associated liquid having a wetting angle higher than 90 degrees relative to said matrix and selected such that at least part of said liquid penetrates the pores of said matrix, when an external mechanical pressure applied to the chamber is equal to or higher than a first pressure level PI, and is spontaneously rejected off the pores of said matrix by capillary action, when said external mechanical pressure applied to the chamber is lower than a second pressure level P2 which is lower than said first pressure level P1 such that the at least one energy absorbing-dissipating structure limits a level of strains which may be transmitted to the frame of the electromechanical actuator by the first element via the movable member of the electromechanical actuator,

wherein said movable member is in said strain path and said external mechanical pressure applied to said deformable chamber is a sum of forces applied to said movable member by said driving unit and an external strain applied to said first element.

13. The space launcher according to claim 12 , wherein the force applied by the driving unit is zero.