초록 ▼

Self-latching deployment apparatus for a multi-paneled solar array comprises at least first and second in-line panels pivotally connected together for rotation about an in-line hinge axis between stowed and deployed positions. A first deployment and locking mechanism maintains the in-line panels in

Self-latching deployment apparatus for a multi-paneled solar array comprises at least first and second in-line panels pivotally connected together for rotation about an in-line hinge axis between stowed and deployed positions. A first deployment and locking mechanism maintains the in-line panels in the deployed position. First and second side panels are pivotally attached to opposite edges of the second in-line panel for rotation between stowed and deployed positions about secondary and tertiary hinge axes, respectively, transverse to the in-line hinge axis between the first and second in-line panels. A first restraint mechanism is engaged with the first side panel to temporarily overpower a drive mechanism for the first side panel and thereby temporarily maintain the first side panel in the stowed position but becomes disengaged from the first side panel when the first and second in-line panels reach the deployed position to enable the first side panel to move to the deployed position. A second restraint mechanism is engaged with the second side panel to temporarily overpower a drive mechanism for the second side panel and thereby temporarily maintain the second side panel in the stowed position but becomes disengaged from the second side panel when the first side panel reaches the deployed position to enable the second side panel to move to the deployed position.

대표청구항 ▼

[ What is claimed is:] [1.] Self-latching deployment apparatus for a multi-paneled solar array comprising:first and second in-line panels pivotally connected together for rotation between stowed and deployed positions about an in-line hinge axis;in-line panel drive means for moving said first and se

[ What is claimed is:] [1.] Self-latching deployment apparatus for a multi-paneled solar array comprising:first and second in-line panels pivotally connected together for rotation between stowed and deployed positions about an in-line hinge axis;in-line panel drive means for moving said first and second in-line panels between the stowed and the deployed positions;a first side panel pivotally connected to said second in-line panel for rotation between stowed and deployed positions about a secondary hinge axis transverse to said in-line hinge axis;first locking means for maintaining said first and second in-line panels in the deployed position;first side panel drive means for moving said first side panel between the stowed and the deployed positions; andfirst restraint means normally engaged with said first side panel to temporarily overpower said first side panel drive means to thereby temporarily maintain said first side panel in the stowed position but becoming disengaged from said first side panel when said first and second in-line panels reach the deployed position to enable said first side panel to move to the deployed position.