Separable roller screw assembly for a space craft release mechanism system
The present disclosure relates to a separable roller screw assembly comprising: a first screw shaft having a first external thread and being axially separated from a second screw shaft having a second external thread; a planetary roller arrangement comprising multiple rotatable rollers radially arrayed about the first and second screw shafts, whilst being encapsulated by a rotatable nut module; the rotatable nut module being coaxially arranged about the first and second screw shafts and configured for maintaining the planetary roller arrangement, the first and second screw shafts in an axially fixed configuration to permit the assembly to carry a load in an axial direction corresponding to an axial tensile force, whilst enabling displacement of the first screw shaft relative to the second screw shaft when said assembly is released from said axially fixed configuration; and wherein each one of the multiple rollers comprises first and second roller external thread regions adapted to engage said first external thread and said second external thread, respectively. Moreover, the present disclosure relates to a space craft release mechanism for separating a first space craft element from a second space craft element and comprising a separable roller screw assembly. In addition, the present disclosure relates a clamp band system for a load bearing interface assembly of a space craft comprising a separable roller screw assembly.
1. A separable roller screw assembly comprising:
a first screw shaft comprising a first external thread, wherein the first screw shaft is axially separated from a second screw shaft comprising a second external thread;
a planetary roller arrangement comprising multiple rotatable rollers radially arrayed about the first screw shaft and the second screw shaft, wherein each of the multiple rollers is encapsulated by a rotatable nut module, and wherein each one of the multiple rollers comprises a first roller external thread region and a second roller external thread region adapted to engage the first external thread and the second external thread, respectively, the rotatable nut module is coaxially arranged about the first screw shaft and the second screw shaft and configured for maintaining the planetary roller arrangement, the first screw shaft and the second screw shaft in an axially fixed configuration to permit the separable roller screw assembly to carry a load in an axial direction corresponding to an axial tensile force, while enabling displacement of the first screw shaft relative to the second screw shaft when the separable roller screw assembly is released from the axially fixed configuration; and
wherein, when the separable roller screw assembly is released from the axially fixed configuration and subjected to the axial tensile force, the first screw shaft is permitted to displace axially from the second screw shaft via rotation of the planetary roller arrangement about the first screw shaft and the second screw shaft.
2. The separable roller screw assembly according to claim 1 , wherein the first screw shaft is axially displaceable from the second screw shaft at least until the first screw shaft is separated from any one of the rotatable nut module and the planetary roller arrangement.
3. The separable roller screw assembly according to claim 1 , wherein both the first screw shaft and the second screw shaft are axially displaceable relative to the rotatable nut module and the planetary roller arrangement.
4. The separable roller screw assembly according to claim 3 , wherein the first screw shaft and the second screw shaft are axially displaceable relative to the rotatable nut module at least until the first shaft and said second shaft are separated from the rotatable nut module and the planetary roller arrangement.
5. The separable roller screw assembly according to claim 1 , wherein the second screw shaft remains essentially axially non-displaceable relative to the rotatable nut module and the planetary roller arrangement.
6. The separable roller screw assembly according to claim 1 , wherein the rotatable nut module comprises an internal surface adapted for engaging the first roller external thread region and the second roller external region of each of the multiple rotatable rollers.
7. The separable roller screw assembly according to claim 6 , wherein the internal surface comprises an internal thread region adapted for engaging the first roller external thread region and the second roller external region of each of the multiple rotatable rollers.
8. The separable roller screw assembly according to claim 6 , wherein said internal surface is an essentially flat surface adapted for engaging the crest of the first roller external thread region and the second roller external region of each of the multiple rotatable rollers.
9. The separable roller screw assembly according to claim 1 , wherein said rotatable nut module is configured for maintaining the planetary roller arrangement, the first screw shaft and the second screw shaft in the axially fixed configuration by a locking mechanism configured to prevent the first screw shaft, the second screw shaft, the planetary roller arrangement and the rotatable nut module to rotate relative each other.
10. The separable roller screw assembly according to claim 9 , wherein the first screw shaft and the second screw shaft comprises first rotational stop unit and second rotational stop unit, respectively, and
the separable roller screw assembly further comprises a housing comprising a first recess and a second recess arranged on opposite sides of the housing, as seen in the axial direction, the first recess and the second recess accommodate the first rotation stop unit and the second rotational stop unit, respectively, whereby a locking arrangement is formed by the housing, the first rotational stop unit, the second rotational stop unit and the locking mechanism enabling the separable roller screw assembly to maintain the axially fixed configuration.
11. The separable roller screw assembly according to claim 9 , wherein the locking mechanism is configured for enabling a release of the separable roller screw assembly from the axially fixed configuration.
12. The separable roller screw assembly according to claim 1 , wherein the first roller external thread region and/or the second roller external thread region of each one of the multiple rollers extend along each one of the multiple rollers to form a continuous external thread section.
13. The separable roller screw assembly according to claim 6 , wherein the internal surface of the rotatable nut module forms a continuous internal thread section.
14. A space craft release mechanism for separating a first space craft element from a second space craft element, the space craft release mechanism comprising
a separable roller screw assembly comprising:
a first screw shaft comprising a first external thread, wherein the first screw shaft is axially separated from a second screw shaft comprising a second external thread;
a planetary roller arrangement comprising multiple rotatable rollers radially arrayed about the first screw shaft and the second screw shaft, wherein each of the multiple rollers is-encapsulated by a rotatable nut module, and wherein each one of the multiple rollers comprises a first roller external thread region and a second roller external thread region adapted to engage the first external thread and the second external thread, respectively, the rotatable nut module is-coaxially arranged about the first screw shaft and the second screw shaft and configured for maintaining the planetary roller arrangement, the first screw shaft and the second screw shaft in an axially fixed configuration to permit the separable roller screw assembly to carry a load in an axial direction corresponding to an axial tensile force, while enabling displacement of the first screw shaft relative to the second screw shaft when the separable roller screw assembly is released from the axially fixed configuration; and
wherein, when the-separable roller screw assembly is released from the-axially fixed configuration and subjected to the-axial tensile force, the first screw shaft is permitted to displace axially from the second screw shaft via rotation of the planetary roller arrangement about the first screw shaft and the second screw shaft.
15. The space craft release mechanism according to claim 14 , further adapted to connect to the first space craft element and the second space craft element, whereby, when the first screw shaft is axial displaced from the second screw shaft until the first screw shaft is separated from any one of the nut module and the planetary roller arrangement, the first space craft element is separated from the second space craft element.
16. The space craft release mechanism according to claim 15 , wherein the first screw shaft is connectable to the first space craft element and the second screw shaft is connectable to the second space craft element.
17. A clamp band system for a load bearing interface assembly of a space craft comprising:
a separable roller screw assembly comprising:
a first screw shaft comprising a first external thread, wherein the first screw shaft is axially separated from a second screw shaft comprising a second external thread;
a planetary roller arrangement comprising multiple rotatable rollers radially arrayed about the first screw shaft and the second screw shaft, wherein each of the multiple rollers is-encapsulated by a rotatable nut module, and wherein each one of the multiple rollers comprises a first roller external thread region and a second roller external thread region adapted to engage the first external thread and the second external thread, respectively, the rotatable nut module is-coaxially arranged about the first screw shaft and the second screw shaft and configured for maintaining the planetary roller arrangement, the first screw shaft and the second screw shaft in an axially fixed configuration to permit the separable roller screw assembly to carry a load in an axial direction corresponding to an axial tensile force, while enabling displacement of the first screw shaft relative to the second screw shaft when the separable roller screw assembly is released from the axially fixed configuration; and
wherein, when the-separable roller screw assembly is released from the-axially fixed configuration and subjected to the-axial tensile force, the first screw shaft is permitted to displace axially from the second screw shaft via rotation of the planetary roller arrangement about the first screw shaft and the second screw shaft.
18. The clamp band system according to claim 17 , comprising a clamp band structure comprising a first end part connected to a second end part via the separable roller screw assembly, wherein the first end part is expanded from the second end part when the first screw shaft of the separable roller screw assembly is axially displaced from the second screw shaft of the separable roller screw assembly.
19. A load bearing interface assembly comprising:
a clamp band system for a load bearing interface assembly of a space craft, wherein the claim band system comprises:
a separable roller screw assembly comprising:
a first screw shaft comprising a first external thread, wherein the first screw shaft is axially separated from a second screw shaft comprising a second external thread;
a planetary roller arrangement comprising multiple rotatable rollers radially arrayed about the first screw shaft and the second screw shaft, wherein each of the multiple rollers is-encapsulated by a rotatable nut module, and wherein each one of the multiple rollers comprises a first roller external thread region and a second roller external thread region adapted to engage the first external thread and the second external thread, respectively, the rotatable nut module is-coaxially arranged about the first screw shaft and the second screw shaft and configured for maintaining the planetary roller arrangement, the first screw shaft and the second screw shaft in an axially fixed configuration to permit the separable roller screw assembly to carry a load in an axial direction corresponding to an axial tensile force, while enabling displacement of the first screw shaft relative to the second screw shaft when the separable roller screw assembly is released from the axially fixed configuration; and
wherein, when the-separable roller screw assembly is released from the-axially fixed configuration and subjected to the-axial tensile force, the first screw shaft is permitted to displace axially from the second screw shaft via rotation of the planetary roller arrangement about the first screw shaft and the second screw shaft; and
wherein the load bearing interface assembly is arranged between a first space craft element and a second space craft element.
20. The load bearing interface assembly according to claim 19 , wherein the clamp band system is arranged to extend about the load bearing interface assembly.