Opterus Research and Development, Inc.

Roccor, LLC

L'garde, Inc.

Thomas W Murphey

Levi Nicholson

William H Francis

Patrick Alexander Rodriguez

Michael Folkers

Kyle Egan

Erik Pranckh

Todd Whitaker

Bruce L Davis

Kellie A Craven

Philip Keller

Kevin Cox

Tayler Thomas

Daniel Hunt

Edward Smutney

Juan M Mejia-Ariza

Carter Fortuin

A deformable support apparatus includes a deformable body configured to transition between at least an extended state and a contracted state where a stiffness of the deformable body in the extended state is greater than a corresponding stiffness of the deformable body in the contracted state. The deformable body includes a first member and a second member coupled to and in opposition to the first member, and arranged about a longitudinal axis. In the extended state, the first member has at least a first curved portion and the second member has at least a second curved portion. The at least a first curved portion is a positive curved portion with respect to the longitudinal axis and the at least a second curved portion is a negative curved portion with respect to the longitudinal axis.

Collapsible tubular mast (CTM) with surface material between trusses

A retractable mast solar array includes a collapsible boom extensible by a boom deployer. At least one foldable upper arm assembly is coupled to the collapsible boom. At least one foldable lower arm assembly coupled to the collapsible boom. A foldable solar array includes two or more columns of blanket elements, each column of blanket elements is affixed at one end to the at least one foldable upper arm assembly and at an opposite end to the at least one foldable lower arm assembly. In a stowed state, the two or more columns of blanket elements are stowed folded in either or both of the at least one foldable upper arm assembly or the at least one foldable lower arm assembly, and in a deployed state, the two or more columns of blanket elements are unfolded to a deployed solar array.

Retractable mast solar array

A method of in-space assembly includes: providing a roll of spooled high strength composite (HSC) boom, a robotic arm, and a printhead disposed at about an end of the robotic arm, the roll of spooled high strength composite boom feedingly coupled to the printhead; positioning the robotic arm; dispensing from the roll of spooled high strength composite boom a length of high strength composite boom; positioning again the robotic arm; dispensing another length of high strength composite boom from the roll of spooled high strength composite boom or from another roll of spooled high strength composite boom; joining by the printhead; and repeating said step of positioning to said step of joining until a desired structure is assembled in part or in whole. A system for in-space assembly and printhead to print struts for in-space assembly are also described.

In space assembly

A self-deployable array of panels includes a plurality of panels, each panel having a first compressed panel thickness state and a second expanded panel thickness state, and including a spring bias element biased to the second expanded panel thickness state. A plurality of locking hinges hingedly couple each of the panels to an adjoining panel. Each locking hinge is biased to an open position. A release of stored potential energy of both of the spring bias element biased to the second expanded panel thickness state, and the locking hinges biased to the open position causes the self-deployable array of panels to self-deploy from a folded stowed state. A single part offset locking hinge is also described.

Morphing self-stiffening array (MOSSA) and hinge

A doubly curved reflector for compact storage in a folded state includes a plurality of gores, each gore having on either long side a gore side curve. At least one hinge is mechanically coupled between each adjacent gore, the at least one hinge including a fold roll hinge or a living hinge. In a stowed doubly curved reflector state each gore folds about the at least one hinge when folded closed such that a face surface of each gore folds against an adjacent face surface of another gore into a substantially cylindrical structure. In a deployed doubly curved reflector state, each hinge. A doubly curved reflector for compact storage in a folded state and a locked open state, a method of manufacture, and a method for designing a substantially wrinkle free doubly curved foldable reflector having gores of a composite material are also described.

Wrinkle free foldable reflectors made with composite materials

A deformable boom device includes a pair of shells, each shell of a substantially same arc length. A pair of hinges is mechanically coupled to the pair of shells to join the pair of shells into an open cross section as deployed in an extended state, and into about a flat structure in a flattened state. At least one of the pair of shells can include an about semi-circular cross section.

Living hinge boom

A boom deployer to deploy or retract a deformable boom includes a boom deployer frame. An integrated motor-spool assembly is translatably mounted in the boom deployer frame. At least one belt tensioning assembly is also translatably mounted in the boom deployer frame. The belt tensioning assembly tensions at least one recirculating belt which rolls over a roller of the belt tensioning assembly. The at least one recirculating belt is configured to roll over a rolled deformable boom, the deformable boom clamped to and rolled on the integrated motor-spool assembly. A boom deployer with a tensioned stationary belt is also described.

Boom deployer

A trussed collapsible tubular mast includes a deformable beam having an extended state, a flattened state, and a rolled state, where a stiffness and strength of the deformable beam in the extended state is greater than a different stiffness and a different strength of the deformable beam in the flattened state. At least one collapsible tubular mast wall has a plurality of truss members of a first material having a first material thickness. At least one truss member is disposed substantially perpendicular to a longitudinal axis of the trussed collapsible tubular mast. Disposed between the truss members is a wall area of a second material thickness less thick than the first material thickness.

Methods, systems, and devices for foldable tube with unitary hinge are provided in accordance with various embodiments. Some embodiments include a device that may include one or more foldable tube sections configured to facilitate the deployment of an object with respect to an end portion of at least one of the one or more foldable tube sections; each of the one or more foldable tube sections may include one or more unitary hinge regions. The unitary hinge regions may include one or more longitudinal hinge regions configured to enable folding that is transverse to a primary axis of a respective foldable tube section. The unitary hinge regions may include a lateral hinge region configured to enable flattening that is parallel to a primary axis of a respective foldable tube section. Some embodiments may include a wire harness disposed within an interior portion of one or more foldable tube sections.

Foldable tube with unitary hinge devices, systems, and methods

A deformable device includes a deformable beam or hinge having an extended state, a flattened state, and a rolled state if a beam, where a stiffness and strength in the extended state is greater than a different stiffness and strength in the flattened state, the deformable beam or the hinge deformable along a long axis. An end face cross section transverse to the long axis includes a first periodic curved member which defines at least two shaped curves. A second periodic curved member defines at least two shaped curves. The second periodic curved member is mechanically coupled to the first periodic curved member at respective ends of the end face cross section. The first arc length of the first periodic curved member and the second arc length of the second periodic curved member are of about a same arc length.

Deformable structures collapsible tubular mast (CTM)

Methods, systems, and devices for furlable antenna blade components are provided in accordance with various embodiments. For example, some embodiments include a device that may include one or more furlable antenna blade components; each of the one or more furlable antenna blade components may include one or more conductive elements. In some embodiments, each of the one or more furlable antenna blade components include one or more laminate layers. Some embodiments include a method that may include: furling one or more furlable antenna blade components around a central axis; and/or securing the one or more furlable antennae blade components when in a furled state.

Furlable antenna blade devices, systems, and methods

A deformable device includes a deformable beam or hinge having an extended state, a flattened state, and a rolled state if a beam, where a stiffness and strength of the deformable beam or the hinge in the extended state is greater than a different stiffness and strength of the deformable beam or the hinge in the flattened state. A cross section includes a first about V shape half and a second about V shape half. Each half includes a vertex with at least one curve extending into two walls at least one of the walls including a plurality of truss members, both of the walls extend into a joining edge. The first about V shape half and the second about V shape half are joined together at a seam of a joining edge of the first about V shape half and the second about V shape half.

A deformable device has an extended state, a flattened state, and a rolled state if a beam, where a stiffness and strength of the deformable beam or hinge in the extended state is greater than a different stiffness and strength of the deformable beam or hinge in the flattened state. An end face cross section includes a main C curved member which defines an about circular shape of an arc ranging between about a quarter arc and a substantially full circle. A periodic C curved member defines at least two about C shaped curves. The periodic C curved member has a first periodic C curved member end mechanically coupled to the first main C curved member end, and a second periodic C curved member end mechanically coupled to the second main C curved member end. A deformable device with a V shaped member is also described.

Growing community of inventors

Fort Collins, CO, United States of America

Thomas W Murphey