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US 5,961,738 AGranted
Solar array for satellite vehicles
AssigneeAEC-Able Engineering Co., Inc.
InventorsMax D. Benton, P. Alan Jones, Brian Spence, Earl McCutcheon, Carl Devillier
Life of this patent
Estimating the term…
Abstract
A solar array with a blanket having solar cells incorporated in modules that can readily be removed, replaced, and accordion-folded to a stowed condition. A scissors array having tracks in which scissors linkages are slidingly fitted enables the array to be stowed or deployed from a container in which the module are interleaved with soft, compressed leaves that protect the blanket from inertial forces during handling and launching.
Claims14
A solar array comprising:
- a solar array blanket comprising a plurality of solar power modules, each said module comprising a backplane bounded by a pair of parallel lateral edges and a pair of longitudinal edges, a solar cell laid on said backplane, said backplane including circuitry for incorporating said solar cell into a circuit, said backplane further including a pair of tabs carrying circuit connectors for said circuitry, one of said tabs extending from each longitudinal edge;
- a spine segment attached to each longitudinal edge, each said spine segment comprising a pair of rigid compression plates between which a longitudinal edge of at least one backplane is sandwiched, fasteners passing through holes in said backplane to hold said backplane against twisting or slipping relative to the spine segment, said spine segments at the outer longitudinal edges of said solar array blanket holding the edge of only one backplane, while a spine member between a pair of solar power modules holds an edge of two backplanes, and a tab compression plate overlaying a pair of adjacent tabs and holding them compressively between it and one of said compression plates, a hinge on one of said tab compression plates adapted to be connected to an aligned spine segment to form a spine that permits folding motion between two backplanes that are aligned in a longitudinal direction, and circuitry extending along at least one spine conductively interconnecting the circuitry of solar power modules which are adjacent along their lateral edges:
- deployment structure comprising a plurality of pairs of scissor arms joined in pairs at a respective central bearing, a plurality of lateral tracks, said lateral tracks being parallel to said lateral edges of the solar power modules said scissor arms having ends laterally slidable in said tracks, a spring in at least one of said tracks biasing its respective said ends toward one another, thereby tending to deploy said deployment means, one of said tracks including an offset flange to which at least one of said spines is connected;
- and
- a container for containing said solar blanket and deployment structure when in their stored configuration, said container forming a cavity, a pair of sets of soft flexible and compressible leaves rooted in said container, so disposed and arranged as to interleaf between adjacent solar power modules when the array is retracted with them in an accordion-fold pattern forming a continuous body to protect them from inertial forces, said leaves being soft and flexible and able to bend to release said modules when they are withdrawn from the cavity, and a closure to close said cavity and house the stored solar array.
2 more elements
In combination:
- a solar array blanket comprising a plurality of planar solar power modules each having parallel longitudinal and lateral edges, and a hinge joining adjacent lateral edges so that the blanket can be folded, accordion style, to a stored configuration;
- and
- a container to contain said solar blanket in a stored configuration, with said solar power modules in their folded condition, said container including a pair of sets of soft flexible and compressible fingers fixed to the container spaced apart from and facing each other, whereby to interleaf between adjacent modules to prevent them from abutting one another, and forming a continuous body to protect the modules from inertial forces, said fingers being deflectable to enable said interleaving and to permit said modules to be withdrawn from the container, said container including a closure to close the cavity when the solar blanket is stored therein.
A solar array blanket comprising a plurality of solar power modules, each said module comprising a backplane bounded by a pair of parallel lateral edges and a pair of longitudinal edges, solar cell laid on said backplane, said backplane including circuitry for incorporating said a solar cell into a circuit, said backplane further including a pair of tabs carrying circuit connectors for said circuitry, one of said tabs extending from each longitudinal edge;
- a spine segment attached to each longitudinal edge, each said spine segment comprising a pair of rigid compression plates between which a longitudinal edge of at least one backplane is sandwiched, fasteners passing through holes in said backplane to hold said backplane against twisting or slipping relative to the spine segment, said spine segments at the outer longitudinal edges of said solar array blanket holding the edge of only one backplane, while a spine member between a pair of solar power modules holds an edge of two backplanes, and a tab compression plate overlaying a pair of adjacent tabs and holding them compressively between it and one of said compression plates, a hinge on one of said tab compression plates adapted to be connected to an aligned spine segment to form a spine that permits folding motion between two backplanes that are aligned in a longitudinal direction, and circuitry extending along at least one spine conductively interconnecting the circuitry of solar power modules which are adjacent along their lateral edges.
Dependencies are inferred from the claim text.