M.m.a. Design, LLC

River Front Services, Inc.

Southwest Research Institute

Roccor, LLC

Harris Corporation

Thomas Jeffrey Harvey

Toby Justin Harvey

Anthony Miles Brown

Donald Ray Brown

Shane Eric Stamm

Leslie A Seal

Thomas J Rose

Mitchell T Wiens

Mark A Bailey

Christopher A Pelzmann

Colleen Roseanna Harvey

Ryan M VanHalle

Randy J Rose

Toby J Harvey

Dana Turse

William H Francis

Bruce L Davis

Bibb Bevis Allen

Andrew Tomchek

Timothy John Ring

Zachary McConnel

Kassi Butler

Jeffrey Edwin Oroke

Matthew John DeVito

Toby Harvey

Dave C Lenzi

Deployable devices, systems, and methods are provided. Some embodiments include a system that may include: multiple frames configured to support multiple elements; multiple longerons; multiple diagonals coupled with the multiple longerons; and multiple battens. One or more battens may be coupled with at least one or more longerons and one or more frames such that the respective batten is offset at least along a length of the respective longeron with respect to at least a hinge point between the respective longeron and another longeron from the multiple longerons or along a length of the respective frame with respect to a hinge point between the respective frame and another frame from the multiple frames. Some embodiments include a method for ensuring synchronous deployment of a system that may include orienting a hinge axis coupled with at least one longeron substantially perpendicular to a hinge axis coupled with two or more frames.

Rigid articulated batten integrated truss devices, systems, and methods

A passively deployable solar panel array. A truss backing is attached to the back of the solar panels and has longerons and hinge linkages that form a series of moveable parallelograms operable to fold and unfold. The truss backing further has springs and diagonals, with at least one spring and one diagonal associated with each of the parallelograms. The springs are operable to deploy the solar panels from a folded position to a deployed position. Each diagonal is operable to become in tension diagonally across its associated parallelogram once the solar panels are deployed into a final position.

Passively deployable solar panel array with truss backing and synchronizing linkages

The invention is directed to deployable reflectarray antenna structure. In one embodiment, the deployable reflectarray antenna structure includes a pair of flexible electrical elements, a feed antenna, and a deployment mechanism that employs a plurality of tapes to respectively transition the pair of flexible electrical elements from an undeployed state in which the elements are folded towards a deployed state in which the deployment mechanism and electrical elements cooperate to form a reflectarray and a subreflector of a reflectarray antenna structure. Further, the deployment mechanism also operates to position the reflectarray and subreflector relative to one another and to the feed antenna so as to realize a reflectarray antenna structure.

Deployable antenna structure

A passively deployable solar panel array. A truss backing is attached to the back of the solar panels, and has top segments, bottom segments, and hinge linkages that form a series of moveable parallelograms operable to fold and unfold. The truss backing further has springs and trusses, with at least one spring and one truss associated with each of the parallelograms. The springs are operable to deploy the solar panels from a folded position to a deployed position. Each truss is operable to become in tension diagonally across its associated parallelogram once the solar panels are deployed into a final position.

Passively deployable solar panel array with truss backing

Telescoping boom systems, devices, and methods are provided in accordance with various embodiments. For example, some embodiments include zero dead band telescoping boom systems, devices, and methods. Embodiments in general include hard stop preloading mechanisms for telescoping booms with multiple tube segments. Some embodiments provide components that facilitate the deployment sequencing of the multiple tube segments along with facilitating preloading of the multiple tube segments of a telescoping boom. The tools and techniques provided may be integrated into the multiple tube segments rather than being provided as a separate system. Some embodiments allow for precise deployment of the multiple tube segments of the telescoping boom systems, devices, and methods.

Telescoping boom systems, devices, and methods

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.

Deployable structure for use in establishing a reflectarray antenna

An explosive detonating system comprises connectable components to connect/disconnect a pathway that ignites an explosion. A firing actuator activates primers. An adapter connects the firing actuator to shock tube and channels the ignition force from the primers into the shock tube. A cap box houses blasting caps coupled to the end of the shock tube. A priming well is coupled to the cap box/blasting caps and detonating cord. When the firing actuator is initiated, the percussion caps ignite, sending an explosive jet of gas into the shock tube, which ignites an explosive liner. An explosive wave travels through the shock tube and activates the blasting caps, which activate the detonating cord in the priming well. The explosive is placed in a location to provide a desired explosive effect. For example, the system may be employed as a system to breach into structures, remove obstacles and/or barriers, or other applications.

Explosive detonating system and components

A tape drive comprises a roll of a tape that can be extended from a rolled state to an extended state. The tape includes a rigid material that supports the tape and a pliable material disposed at least partially on one side of the tape. A compression roller is disposed on a side of the tape and is biased toward the tape. A drive roller is disposed on the other side of the tape. The drive roller comprises an uneven surface that mechanically engages the pliable material of the tape, without protruding through the tape, as a result of the bias of the compression roller forcing the tape toward the drive roller. A motor turns the drive roller to extend the tape from the roll as the protrusions of the uneven surface of the drive roller mechanically engage the pliable material of the tape as the drive roller turns.

Structural tape deployment apparatus

An explosive detonating system comprises connectable components to connect/disconnect a pathway that ignites an explosion. A firing actuator activates primers (percussion caps). An adapter connects the firing actuator to shock tube and channels the ignition force into the shock tube. A cap box houses blasting caps coupled to the end of the shock tube. A priming well is coupled to the cap box/blasting caps and the detonating cord. When the firing actuator is initiated, the percussion caps ignite, sending an explosive wave into the adapter, which channels the wave into the shock tube and ignites the shock tube. The explosive wave travels through the shock tube and activates the blasting caps, which activate the detonating cord in the priming well. The explosive is placed in a location to provide a desired explosive effect. For example, the system may be employed as a system to breach structures or other applications.

A deployable prop is provided that is capable of transitioning from an undeployed state to a deployed state in which the prop can be used to support an object against or adjacent to a structural surface. In one embodiment, the deployable prop includes a bistable 'carpenter's' tape, a foot member that is engaged to one end of the tape, and a head member that is engaged to the other end of the tape. The tape, foot member, and head member can be placed in an undeployed state that has 'roll' shape and in a deployed state in which the tape extends substantially linearly between the foot and head members and can be used to support an object against or adjacent to a structural surface.

Deployable prop

Deployable reflectarray antenna structure

A panel structure for use in a deployable and cantilevered solar array structure is provided. A panel includes first and second planar panel sections and an intermediate panel section connecting the first and second sections. The planar panel sections are capable of being situated with respect to one another so as to have a V-tent-like shape when the panel is in a deployed state and to be coplanar when the panel is in a stowed state. When in the V-tent-like shape, the intermediate section of the panel extends in a straight line that is collinear or parallel to the longitudinal axis of the cantilevered solar array structure when deployed. The V-tent-like shape produces A panel structure that has a relatively high moment of inertia, is stiff, and can provide a large area for supporting solar cells.

Growing community of inventors

Nederland, CO, United States of America

Thomas Jeffrey Harvey