Docking system for space modules

Claim 2

A docking system for space modules comprising a docking device having male and female coupling members carried by the two space modules respectively, said coupling members having complementary conical surfaces for contacting each other in the coupled condition, complementary locking means adapted to secure said coupling members against axial separation while permitting relative rotation therebetween, said locking means comprising resilient retaining means carried by one of said coupling members and arranged to snap engage a corresponding seat member rotatably mounted in the other coupling member, reference means on said conical coupling surfaces for providing the correct alignment for said modules, and a plurality of connecting devices arranged to lock the two space modules in a precise aligned position wherein each connecting device comprises a coupling seat located in one of said modules and a coupling shank carried by the other module and axially moveable between a withdrawn inoperative position and an extended coupling position, the coupling shank having a head which is expandable within said coupling seat to form the connection between the two modules.

Claim 3

Docking system according to claim 1, wherein the expandible head of the said coupling shank is essentially spherical and the coupling seat intended to cooperate with this expandible head has a corresponding shape.

Claim 4

Docking system according to claim 1, wherein the coupling shank has a tubular body with, in correspondence with the expandible head a series of longitudinal slits defining a pluratlity of petal sectors which are resiliently outwardly flexible.

Claim 5

Docking system according to claim 3, wherein the inner faces of the sectors define a substantially conical surface converging towards the end of the coupling shank and in that a thrust member is movable axially between the said sectors to cause the expansion of the sectors.

Claim 6

Docking system according to claim 4, wherein the coupling shank is slidable in a cylindrical casing fixed to the corresponding space module, and in that the thrust member is connected to an auxiliary control member mounted in its turn in a slidable manner within the coupling shank.

Claim 7

Docking system according to claim 5, wherein the auxiliary slidable member has a coaxial tubular spigot which is internally screw-threaded and in that the fixed casing is supported rotatably by a screw having one end engaged in the spigot and the opposite end controlled by an electric motor fixed to the casing.

Claim 8

Docking system according to claim 6, wherein the fixed casing has an end-of-stroke stop arranged to cooperate with the coupling shank to limit the maximum position of extension of the latter.

Claim 9

Docking system according to claim 5, wherein the thrust member is connected to the slidable auxiliary member by means of a ball joint.

Claim 10

Docking system according to claim 1, wherein the said resilient retaining means are carried by an element which is axially slidable relative to the body of the corresponding coupling member, and in that the latter has an electric motor and a screw-nut system for effecting the axial displacement of the slidable member so as to allow the locking of the resilient means in the engaged condition of the said seat. .

Claim 11

Docking system according to claim 1, wherein the two conical coupling surfaces have a slightly elliptical section.

Claim 12

Docking system according to claim 1, wherein the two coupling members have respective docking probe of which at least one is retractable and able to connect with the other probe in its extended condition and subsequently to retract to allow the final approach and contact of the two coupling members.

Claim 13

Docking system according to claim 1, wherein one of the two coupling members is carried by a shock absorber pylon movable axially between an extended condition and a withdrawn condition.

Claim 14

A docking system for space modules comprising a docking device including male and female coupling members carried by the two space modules respectively, said coupling members being arranged to allow relative rotation of the two modules about the axis of the docking device after they have been brought into coupled position, a plurality of connecting devices arranged to lock the two space modules in a precise relative position after the male and female members of the docking device have been brought into coupled position, each connecting device comprising a coupling seat located in one of the two modules and a coupling shank carried by the other module and axially moveable between a withdrawn inoperative position and an extended coupling position, the coupling shank having a head which is expandable within the coupling seat to form the connection between the two modules, said two coupling members having an infrared radiation indicator system for allowing the mutual coming together in an aligned condition, the infrared radiation indicator system including an infrared radiation transmitter device carried by one of the two coupling members, an infrared radiation receiver device carried by the other coupling member and including an objective, a mirror slightly inclined to a plane perpendicular to the axis of the objective and rotatably driven about this axis so as to reflect the focused infrared radiation onto a point on the internal surface of the objective which describes a circle on this surface upon rotation of the mirror and for infrared detectors positioned according to the four quadrants and corresponding to the internal surface of the objective.

Claim 15

A docking system for space modules comprising a docking device including male and female coupling members carried by the two space modules respectively, said coupling members being arranged to allow relative rotation of the two modules about the axis of the docking device after they have been brought into coupled position, a plurality of connecting devices arranged to lock the two space modules in a precise relative position after the male and female members of the docking device have been brought into coupled position, each connecting device comprising a coupling seat located in one of the two modules and a coupling shank carried by the other module and axially moveable between a withdrawn inoperative position and an extended coupling position, the coupling shank having a head which is expandable within the coupling seat to form the connection between the two modules, said two coupling members having an infrared radiation indicator system for allowing the mutual coming together in an aligned condition, the infrared radiation indicator system including an infrared radiation transmitter device carried by one of the two coupling members, an infrared radiation receiver device carried by the other coupling member and including an objective, a mirror slightly inclined to a plane perpendicular to the axis of the objective and rotatably driven about this axis so as to reflect the focused infrared radiation onto a point on the internal surface of the objective which describes a circle on this surface upon rotation of the mirror and for infrared detectors positioned according to the four quadrants and corresponding to the internal surface of the objective.