143 results about "Deployable structure" patented technology

A valve prosthesis device is disclosed suitable for implantation in body ducts. The device comprises a support stent, comprised of a deployable construction adapted to be initially crimped in a narrow configuration suitable for catheterization through the body duct to a target location and adapted to be deployed by exerting substantially radial forces from within by means of a deployment device to a deployed state in the target location, and a valve assembly comprising a flexible conduit having an inlet end and an outlet, made of pliant material attached to the support beams providing collapsible slack portions of the conduit at the outlet. The support stent is provided with a plurality of longitudinally rigid support beams of fixed length. When flow is allowed to pass through the valve prosthesis device from the inlet to the outlet, the valve assembly is kept in an open position, whereas a reverse flow is prevented as the collapsible slack portions of the valve assembly collapse inwardly providing blockage to the reverse flow. The device is configured so that retrograde flow will be altered from laminar flow and directed towards the leaflets to effect closing.

A catheter apparatus for assessing denervation comprises: an elongated catheter body; a deployable structure coupled to the catheter body, the deployable structure being deployable outwardly from and contractible inwardly toward the longitudinal axis of the catheter body; one or more ablation elements disposed on the deployable structure to move outwardly and inwardly with the deployable structure; one or more stimulation elements spaced from each other and disposed on the deployable structure to move with the deployable structure, the stimulation elements being powered to supply nerve stimulating signals to the vessel; and one or more recording elements spaced from each other and from the stimulation elements, the recording elements being disposed on the deployable structure to move with the deployable structure, the recording elements configured to record response of the vessel to the nerve stimulating signals.

A deployable structure is disclosed. The deployable structure may include one or more slit-tube longerons; and one or more flat sheets coupled with the one or more slit-tube longerons. The one or more slit-tube longerons and the one or more flat sheets may be stowed by rolling the one or more slit-tube longerons and the one or more flat sheets together into a roll. In one embodiment, at least a portion of the one or more slit-tube longerons may be exposed when stowed. In another embodiment, the one or more slit-tube longerons may be manufactured from a shape memory material. These slit-tube longerons unroll into to a straight configuration when exposed to heat.

A deployable structure that may include a slit-tube longeron and a flat panel coupled with the slit-tube longeron. The slit-tube longeron may include a tubular member having a slit that runs along the longitudinal length of the slit-tube longeron. The deployable structure may be configured to couple with a satellite. And the deployable structure may be configured to transform between a stowed state and a deployed state where the tubular member is substantially straight when the deployable structure is in the deployed state, and the tubular member is wrapped around the satellite when the deployable structure is in the stowed state.

An open-lattice, foldable, self-deployable structure with a number of spaced, bendable longitudinal members forming cells each bounded by a portion of two spaced longitudinal members and two spaced diagonal members. The diagonal members are joined to the longitudinal members at the cell boundary intersections of the diagonal members and the longitudinal members. The longitudinal members are made of a material which bends by a predetermined amount below the material's yield point and the diagonal members are made of a material which both bends and twists by a predetermined amount below the material's yield point so that the structure can be collapsed and then self resurrected.

Affordable commercial service platforms in space focusing on customer affordability, quality microgravity services, innovation and combining five emerging space technologies. The invention provides an integrated approach to microgravity services in orbit. First, the reusable launch vehicle (RLV) offers affordable transportation services, platform reboost, and eliminates platform subsystems of propulsion, RCS, liquid storage/resupply, and the like. Second, deployable structures are not heavy for the launch, but expand in orbit. Third, orbital phone networks offer customers control of unmanned experiments. Fourth, an enhanced robotic system transfers payloads. Fifth, manufactured thin film solar cells in orbit offer advantages including weight/cost reductions. The orbital service platform has a low initial cost, expands as the market demands, is repairable, offers quality unmanned microgravity, leads to production facilities using similar hardware and offers numerous affordable commercial services.

The invention discloses a tension integral deployable antenna, which mainly solves the problems of large folded volume and low deployment reliability in the prior art. It consists of n quadrilateral planar expansion units connected to each other through Hooke hinge joints (3) to form a regular polygonal prism-shaped expansion structure; each quadrilateral planar expansion unit adopts a spring frame structure, and the center adopts four support rods (2) and rotating The pair (4) is fixedly connected to form a cross-shaped retractable structure, and the two straight rods of the cross-expanded structure can rotate relatively around the central axis of the plane rotating pair; through the second spring (1-2) of each quadrilateral plane unfolding unit And the tension of the fourth spring (1-4) makes the overall structure unfold from the folded state. The invention has the characteristics of high deployment reliability and small folded volume, and is particularly suitable as a deployment structure for large spaceborne antennas, and can be used in the field of aerospace.

A deployable structure for use in establishing a reflectarray antenna is provided that includes a flexible reflectarray and a deployment structure that includes an endless pantograph for deploying the flexible reflectarray from a folded, undeployed state towards a deployed state in which the flexible reflectarray is substantially planar. In a particular embodiment, the deployment structure includes a plurality of tapes that engage the endless pantograph and are used to establish a positional relationship between the deployed reflectarray and another component of the reflectarray antenna.

A retractable tape spring in-building method for a deployable structure comprising a main tape spring having an axis of deployment and of refurling substantially parallel to an unfurled axis X and comprising two ends, a secondary tape spring comprising two ends and a winding mandrel carried by a shaft parallel to an axis Z perpendicular to the axis X, the main tape spring being wound around the mandrel, a first end of the main tape spring being fixed to the mandrel, the method comprising the following steps: fixing a first end of the secondary tape spring a predefined distance away from a second end of the main tape spring, fixing a second end of the secondary tape spring on the mandrel. A deployable structure comprising a tape spring for a flexible structure is also provided.

Reconfigurable, expandable-collapsible structures based upon negative Poisson's ratio (NPR) auxetic unit cells achieve rapidly deployable apparatus, devices and systems. A plurality of joint bodies, each joint body having a plurality of connection features, are coupled to interconnecting link members with opposing ends, each end including connection features that engage with the connection features of the joint bodies. The link members pivot about different axes relative to the joint bodies, thereby forming an expandable and collapsible structure having a height and a width. The link members form an array of geometric unit cells when the structure is expanded, and the height and the width of the structure when expanded are both greater than the height and the width of the structure when collapsed. In certain embodiments the structures have unit cells based upon triangles or bowtie shapes.

A deployable structure with panels forming an antenna equipped with a solar generator includes: a set of antenna panels each having a substantially rectangular useful surface, the antenna panels abutting each other on first sides parallel to each other, at least one photovoltaic solar panel, each photovoltaic solar panel abutting an antenna panel on a second side of said antenna panel perpendicular to the first sides, first articulation systems, each of said articulation systems enabling an antenna panel to be caused to pivot relative to an adjacent antenna panel about an axis substantially parallel to the first sides of said antenna panels, a second articulation system for each photovoltaic solar panel, each of said articulation systems enabling a photovoltaic solar panel to be caused to pivot relative to the antenna panel that it abuts about an axis substantially parallel to the second side of said antenna panel.

A deployable structure comprises: a support, a tape spring fixed to the support, able to pass from a wound configuration wound about an axis Z, to a deployed configuration, and a mobile arm able to rotate with respect to the support about the Z-axis, able to form a first contact with the tape spring so as to control the deployment of the tape spring.

The invention discloses a cable-pole type deployable structure, obtained by mutual connection of octahedral basic units in two plane directions, wherein each octahedral base unit is composed of an inhaul cable and a pressure bar; the octahedral base unit is composed of an upper rectangular pyramid and a lower rectangular pyramid which have the same bottom surface; four edges of the bottom surface quadrilateral of the rectangular pyramid are composed of travel cables for only bearing tension; four edges of the upper rectangular pyramid are four upper oblique cables; four edges of the lower rectangular pyramid are four lower oblique cables; four horizontal pressure bars are connected from the four top points of the bottom surface quadrilateral of the rectangular pyramid to a central point of the quadrilateral; the intersection point of the four horizontal pressure bars is connected with the top point of the upper rectangular pyramid through a first vertical pressure bar; the intersection point of four horizontal pressure bars is connected with the top point of the lower rectangular pyramid by a second vertical pressure bar; adjacent octahedral basic units are connected through the top points of the bottom surface quadrangle of the pyramid; and the upper oblique cables of all basic units in each line and row in the deployable structure assembled by octahedral basic units in the same plane are connected to an active cable.