Carbitex, Inc.

Massachusetts Institute of Technology

Junus Ali Khan

Kevin Lynn Simmons

Tyler Andre Kafentzis

Keshava Bhamidipaty

Skylar J E Tibbits

Tyler Ross Carpenter

Athina Papadopoulou

Matthew Patrick Westman

An anisotropic composite material assembly comprising a first layer with a tensile modulus different from its compressive modulus and that exhibits variable modulus behavior. The first layer elastically buckle under compressions. A second layer has a tensile modulus substantially the same as its compressive modulus. The first and second layers are joined together, and the assembly is bendable in a first direction with an outer surface of the first layer being in compression and the assembly has a first bending stiffness during bending in the first direction. The assembly is bendable in a second direction opposite the first direction with the outer surface of the first layer being in tension, and the assembly has a second bending stiffness greater than the first bending stiffness during bending in the second direction.

Joined fiber-reinforced composite material assembly with tunable anisotropic properties

A self-transforming structure is formed from a flexible, fibrous composite having a weave pattern of fibers woven at intersecting angles, the weave pattern having a boundary and one or more axes for the fibers, and an added material coupled to the flexible, fibrous composite to form a structure, wherein the flexible, fibrous composite and the added material have different expansion or contraction rates in response to an external stimulus to cause the structure to self-transform, and wherein the added material has a grain pattern oriented relative the weave pattern of the flexible, fibrous composite. Applications of the self-transforming structures include aviation, automotive, apparel/footwear, furniture, and building materials. One particular example is for providing adaptive control of fluid flow, such as in a jet engine air inlet.

Self-transforming structures

An axially stretchable fiber-reinforced composite material, comprising an elastically deformable matrix having a low modulus of elasticity, and a fabric core encapsulated by the matrix. The core comprises first fibers interlaced with second fibers, with the first fibers being in a non-parallel orientation relative to the material's longitudinal axis, and the second fibers are non-parallel relative to the first fibers when the composite material is in a retracted position. The composite material is stretchable between the retracted and extended positions. The fibers have a high modulus of elasticity. The composite material has a non-linear modulus relative to elongation of the composite material between the retraced and extended positions. Movement of the material toward the extended position causes the first and second fibers to rotate relative to each other and in a direction toward alignment with the longitudinal axis, and the matrix material biases the composite material toward the retracted position.

Stretchable fiber-based composite-material

Provided are methods for preparing fabric laminated with polymer film(s) and the laminated fabric prepared according to the methods disclosed herein. The laminated fabric has flexibility similar to fabric not laminated with polymer films and improved adhesion and tensile strength.

Composite materials with binder-enhanced properties and method of production thereof

A flexible fiber-reinforced composite material is manufactured by impregnating a fiber reinforcement material with a non-epoxy matrix material. Subsequently, the impregnated fiber reinforcement material is dried and cured, resulting in a flexible fiber-reinforced composite material that exhibits a tensile modulus between 10 MPa and 42 MPa at 20 percent elongation.

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Pasco, WA, United States of America

Junus Ali Khan