초록 ▼

A supporting structure for a solar sail of a satellite is formed by support arms which are connected in a swiveling manner with a solar panel through unfolding joints, and a film is stretched between the support arms. A longitudinal connector is arranged parallel to one side edge of the solar panel,

A supporting structure for a solar sail of a satellite is formed by support arms which are connected in a swiveling manner with a solar panel through unfolding joints, and a film is stretched between the support arms. A longitudinal connector is arranged parallel to one side edge of the solar panel, which has support arms that are arranged in a joint direction in the plane of the film and form at least one U-shaped supporting structure between which the film of the solar sail can be stretched. Corner connectors are arranged in the interior angle areas between the longitudinal connector and the support arms. This arrangement simplifies known constructions while maintaining the existing functional safety in order to allow for achieving a noticeable weight reduction.

대표청구항 ▼

1. Supporting structure for a solar sail of a satellite, formed by support arms which are connected with a solar panel through unfolding joints in a swiveling manner with a solar sail film stretched between the support arms, wherein a longitudinal connector, which is arranged parallel to one side

1. Supporting structure for a solar sail of a satellite, formed by support arms which are connected with a solar panel through unfolding joints in a swiveling manner with a solar sail film stretched between the support arms, wherein a longitudinal connector, which is arranged parallel to one side edge of the solar panel contains the support arms, which are located in a joint direction in the plane of the film forming at least one U-shaped supporting structure, between which the film of the solar sail can be stretched, and wherein corner connectors are arranged in each of the respective interior angle areas between the longitudinal connector and the respective support arm. 2. Supporting structure as claimed in claim 1, wherein each of the corner connectors have a buckle-proof profile with connecting points without torsional buckling on the longitudinal connector and on one support arm. 3. Supporting structure as claimed in claim 2, wherein the corner connectors are each designed in one piece. 4. Supporting structure as claimed in claim 3, wherein the corner connectors are each formed by two semi-shells that form a positive lock in relation to each other. 5. Supporting structure as claimed in claim 1, wherein each corner connector is designed in two pieces. 6. Supporting structure as claimed in claim 5, wherein a buckle-proof profile with connecting points is arranged between the longitudinal connector and a support arm, and wherein a connecting point without torsional buckling is arranged between the longitudinal connector and the support arm. 7. Supporting structure as claimed in claim 1, wherein the supporting structure is formed by two adjacent U-shaped supporting structures; and wherein a longitudinal connector and three support arms are arranged for this purpose. 8. A satellite assembly comprising: a solar panel; a longitudinal connector extending along an edge of said solar panel, a solar sail; a pair of solar sail support arms extending laterally of said connector, a pair of corner connectors rigidly connecting the longitudinal connector with respective area of said support arm to form a U-shaped solar sail supporting structure with said solar sail stretched between the support arms; wherein said longitudinal connector is supported for pivotal movement at the edge of the solar panel to accommodate pivoting movement of the sail and U-shaped solar sail supporting structure between a storage position with the sail disposed folded on top of the solar panel and in use unfolded position with the sail disposed laterally of the solar panel. 9. A satellite assembly according to claim 8, wherein each of the corner connectors have a buckle-proof profile with connecting points without torsional buckling on the longitudinal connector and on one support arm. 10. A satellite assembly according to claim 8, wherein each corner connector is formed of two shell parts clamping engaging the longitudinal connector and one of the support arm. 11. A satellite assembly according to claim 8, wherein each corner connector includes a buckling resistor profile member extending diagonally fixedly at one side to the longitudinal connector at another side to one of the support arms. 12. A satellite assembly according to claim 8, wherein a pair of said U-shaped solar sail supporting structures are provided which have a common supporting arm. 13. A satellite assembly according to claim 8, wherein a plurality of solar panels are provided which are foldable with respect to one another and include solar panels without a solar sail connected therewith in addition to said solar panel with said solar sail and supporting structure. 14. A satellite assembly according to claim 13, wherein said solar panels are disposed on a plurality of solar panel assembly wings which in use extend laterally of a satellite body in different directions, and wherein each wing includes a solar panel with one of said solar sails and supporting structures.