Abstract: A lock assembly portion may include a housing assembly, first and second latches, at least one latch drive, and at least one actuator. The housing assembly includes a first end portion and an opposite second end portion. The first latch is associated with the first end portion. The second latch is associated with the second end portion. The at least one actuator interfaces the latch drive to the first and second latches. Operation of the latch drive causes the first and second latches to move relative to one another between respective extended and retracted positions.

Abstract: An electric flossing apparatus comprising a flossing head which is detachably connected to a handle containing a reciprocating drive unit, a non-powered second handle to allow for the increased controllability of two-handed powered flossing and a disposable floss assembly that can be easily be attached to or released from the flossing head and handle. The floss is releasably attached to the flossing head in a manner that allows reciprocating motion to be imparted along the length of the floss no matter which direction that the floss exits the end of the flossing head or the shape of the path it takes. By using both hands for flossing the floss may be pulled straight and tensioned to facilitate insertion between tightly spaced teeth and then wrapped around a tooth to facilitate cleaning of the front, sides, and back of each tooth above, near, or just below the gum line. The reciprocating motion is imparted to the floss whenever the floss is tensioned.

Abstract: A separable connector assembly includes a connecting member having a threaded end, and a hollow housing having a cylindrical wall that contains a body rotatably mounted therein. This body is threadably engageable with the threaded end of the connecting member. A first mechanism releasably restrains the body from rotating, and a second mechanism is included for winding a spring about the cylindrical wall of the housing. A third mechanism is included for releasing the spring. A fourth mechanism is included for restraining the threaded end from rotating. A fifth mechanism is included for applying a selected tensile load. When the load is applied, a thread geometry of the connecting member causes the load to be resolved as a torque applied to the body sufficient to cause the body to rotate enabling the connecting member to translate out of engagement with the body and subsequently separate from the body.

Abstract: The invention is a separation system for releasably securing first and second structural members together along mating edges thereof. For example, the segments of a launch vehicle faring used to protect the payload until orbit is reached. In detail, the invention includes a plurality of latches with each latch including a male portion mounted in proximity the edge of the first structural member and a female portion mounted on the second structural member in proximity to the edge thereof. A locking device is mounted on the second structural member in proximity to the edge thereof, movable from a locked position securing the male portion to the female portion to a second position unlocking the male portion from the female portion. An actuation device is provided for sequentially moving the locking device of each latch from the first position to the second position, unlocking the male portions from the female portions of the plurality of latches.

Abstract: The invention is a separable connector that includes nut and bolt assemblies for joining two structural elements together. The thread geometry is selected such when the nut and bolt assemblies are threadably joined and a tension load applied therebetween, upon release of nut the tension load is converted into rotational energy causing the nut to rotate at high speed acting as a flywheel causing the nut to spin off of the bolt.

Abstract: In detail, the system includes at least one first pulley mounted on the first structural member and at least one-second pulley mounted on the second structural member. A cable is attached by one end to the first structural member and wound about the first and second pulleys and is attached by its second end to the second structural member. Preferably there are two or more first and second pulleys with the cable alternately wound between said first and second pulleys with one end of cable attached to the first structural member and the opposite end attached to the second structural member. Thus the cable holds the first and second structural members together. A system to sever the cable is included, which upon actuation will sever the cable allowing the two structural members to separate.

Abstract: The invention is a separable connector that includes nut and bolt assemblies for joining two structural elements together. The thread geometry is selected such when the nut and bolt assemblies are threadably joined and a tension load applied therebetween, upon release of nut the tension load is converted into rotational energy causing the nut to rotate at high speed acting as a flywheel causing the nut to spin off of the bolt.

Abstract: A system and method for docking a space object to a space travel vehicle is disclosed. The space travel vehicle includes a frame assembly which may be deployed into an at least generally funnel-shaped profile at the desired time. A web of sorts is attached to the frame assembly and is disposed into an at least generally funnel-profile by the deployment of the frame assembly as well. In one embodiment the web is in the form of a plurality of Velcro tape members. A space object contacting the web is detachably adhered thereto by including suitable fasteners on the space object as well. Retraction of the frame assembly directs the space object into a space object receptacle of the space travel vehicle, detaches the tapes from the captured space object, and retains the captured space object within the space object receptacle. After the captured space object has been retrieved, the frame assembly may thereafter be deployed to capture another space object in the above-described manner.

Abstract: An improved truss is disclosed that is deployable from a folded, or stowed position to an extended, or deployed position. The truss design facilitates compact storage and is particularly apt for space craft applications. In one aspect of the invention, a truss assembly is provided that includes at least three interconnected truss member sets, each of the truss member sets including first and second truss members that are pivotably interconnected, wherein the truss member sets combinatively define a polygonal structure in the deployed position. The first and second truss members of at least one of the truss member sets are pivotably interconnected to fold inwardly when in the folded position, and the first and second truss members of a second of the truss member sets are pivotably interconnected to fold outwardly when in the folded position.

Abstract: An improved support boom is disclosed for supporting instrumentation on extraterrestrial vehicles. The support boom includes first and second support legs which are each pivotably mountable at corresponding first ends to a support structure and which are interconnected at second ends to define a support boom structure. In one embodiment, flexure members are interposed in each of the support legs so as to pivot the support boom structure from a stowed position to a deployed, cantilevered position. The flexure members may be elongated with an arcuate cross-sectional configuration when straight (e.g., of carpenter's tape construction). Preferably, three support legs are included to define a tripod support arrangement, wherein each of the support legs includes at least one flexure member.

Abstract: An improved hinge assembly is disclosed that is particularly apt for use with deployable trusses utilized on satellites and other spacecraft. In one arrangement, the inventive hinge assembly comprises a tapered roller bearing assembly having tapered rollers angled towards a hinge axis, and a needle roller thrust bearing assembly positioned radially about at least a portion of the tapered roller bearing assembly to yield a compact and lightweight bearing arrangement, while providing satisfactory radial and axial loading bearing characteristics. An axial preload assembly may also be employed with the roller bearing assemblies in the invention to yield enhanced hinge stiffness and repeatability benefits. Such characteristics are of particular importance with deployable spacecraft truss assemblies for supporting instrumentation during orbit. An additional needle roller bearing assembly may be included at an axially spaced position from the tapered roller bearing assembly to provide overload protection (e.g.

Abstract: A fastening system for substantially inhibiting slippage between first and second members interconnected thereby is disclosed. The fastening system is particularly useful in instances where at least one of the first and second members is subject to shear loading. The fastening system may include a fastener having a shank portion which is receivable within first and second bores of the first and second members, respectively, and a nose portion of a nut member for engaging a proximal segment of the shank portion of the fastener proximate the second member to substantially inhibit tilting of the fastener relative to the first and/or second member(s).

Abstract: An alignment tolerant fastening system for interconnecting first and second members having first and second bores therethrough, respectively, is disclosed. The fastening system may include a fastening member having a shank portion which is receivable within the bores of the first and second members, a nut member for engaging at least a distal portion of the fastener shank portion proximate the second member, and first and second washers, at least one of which includes a plurality of serrations, positionable within the first bore of the first member, about the shank portion of the fastener. More specifically, for purposes of accommodating a misalignment between the first and second bores, the inner wall of the first washer is slidably engagable with the fastener shank portion and the outer wall of the second washer is slidably engagable or interconnectable with the first bore wall which defines the first bore of the first member.

Abstract: A locking apparatus for limiting displacement of a fastener relative to first and second members interconnected thereby is disclosed. The locking apparatus may include a locking member which is insertable within a first bore of the first member. In particular, the locking member may have an elastically deformable upper portion and a leg which extend between the fastener and the first member to substantially inhibit displacement (e.g., rotational) of the fastener relative to the first member.

Abstract: A connection apparatus utilizes a structural element made of fusible material supported directly in the connection load path of the device. A carrier mechanism is axially translatably supported in the device and utilizes a connecting member to connect two desired structures. The connection mechanism engages and holds the connecting member in a first axial position. In one embodiment, the connection mechanism releases the connecting member when translated to a second axial position. In another embodiment the connection mechanism tensions the connection when translated to the a second axial position. The fusible member is heated to transition from solid to liquid. In the liquid state, the fusible member no longer opposed axial load on the carrier mechanism. The fusible alloy comprises a low melting temperature alloy, such as bismuth-lead or bismuth-tin.

Abstract: A method and apparatus for separably connecting a first surface to a second surface. The apparatus includes a connecting member provided with a threaded end. A rotatable body threadably engagable with the threaded end is rotatably supported against the first surface for rotation about the threaded end to separably connect the connecting member. The rotatably supported body and the connecting member are restrained from rotation. The connecting member and rotatably supported body further have a selected matching thread geometry such that a tensile load applied to the member when connected with the rotatably supported body is resolved as a torque applied to the rotatably supported body sufficient to urge the body to rotate. When the rotatably supported body is released and allowed to rotate, the threaded member translates and threadably disengages the rotatably supported body to separate the connection.

Abstract: A harmonic traction motor for converting linear motion to rotational motion. A driven shaft is surrounded by the annulus of a shaft driving member having a circumference slightly larger than the circumference of the shaft. At least two actuating devices are connected between the support and the driving member at 90.degree. with respect to each other and sequentially energized to cause the annulus to exert a force around the shaft in a hypocycloidic motion. This motor has high torque, high stiffness, zero backlash and small volume and can be operated in a stepping mode and can be used as a brake or clutch, if desired.