Massachusetts Institute of Technology

Samuel Eli Calisch

Neil Adam Gershenfeld

Kenneth C Cheung

A method of producing inductive sensors, including LVDTs and inductive encoders, manufactured by plotting fine wire onto a planar substrate. A sensor is constructed using a computer-controlled machine to place wire onto a planar adhesive substrate. This substrate forms a predictable and uniform surface to deposit each turn of wire, and so the placement accuracy is considerably better than conventional coil winding. This planar substrate can then be manipulated into a desired three-dimensional shape (e.g., by folding, rolling, corrugating, winding, etc.), carrying the wire along with it. In particular, the same CNC machine used to place the wire can be used to cut, crease, score, or otherwise pattern the substrate to facilitate the three-dimensional arrangement.

Precision planar coil placement for three-dimensional inductive sensors

A method of forming a structural honeycomb includes cutting and folding a substrate sheet according to predetermined cutting and folding patterns and fold angles that cause the sheet to form a honeycomb having cells that each have at least one face abutting, or nearly abutting, the face of another cell. The honeycomb is then stabilized by joining abutting, or nearly abutting, faces to hold the honeycomb together. The honeycomb may have a prespecified three-dimensional shape. The folding pattern may include corrugation, canted corrugation, or zig-zag folds. Joining may employ fixed and/or reversible joinery, including slotted cross section, tabbed strip, angled strip, integral skin, sewn, or laced. At least some folds may be partially-closed to create bends and twists in the honeycomb structure. Some surfaces of the honeycomb may be covered with a skin or face sheet. The substrate sheet may have flexible electronic traces.

Fabrication of three-dimensional kirigami structures with tunable properties

Flexural digital materials are discrete parts that can be assembled into a lattice structure to produce an actuatable structure capable of coordinated reversible spatially-distributed deformation. The structure comprises a set of discrete flexural digital material units assembled according to a lattice geometry, with a majority of the discrete units being connected, or adapted to be connected, to at least two other units according to the geometry. In response to certain types of loading of the structure, a coordinated reversible spatially-distributed deformation of at least part of the structure occurs. The deformation of the structure is due to the shape or material composition of the discrete units, the configuration of connections between the units, and/or the configuration of the lattice geometry. Exemplary types of such actuatable structures include airplane wing sections and robotic leg structures. An automated process may be employed for constructing an actuatable structure from flexural digital materials.

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Crawfordsville, IN, United States of America

Samuel Eli Calisch