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  • 1
    Publication Date: 2019-06-28
    Description: Apparatus for adapting a general purpose and effector device to a special purpose and effector is disclosed which includes an adapter bracket assembly which provides a mechanical and electrical interface between the end effector devices. The adapter bracket assembly includes an adapter connector post which interlocks with a diamond shaped gripping channel formed in closed jaws of the general purpose end effector. The angularly intersecting surfaces of the connector post and gripping channel prevent any relative movement there between. Containment webs constrain the outer finger plates of the general purpose jaws to prevent pitch motion. Electrical interface is provided by conical, self aligning electrical connector components carried by respective ones of said end effectors.
    Keywords: MECHANICAL ENGINEERING
    Format: application/pdf
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  • 2
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: An apparatus for securing payloads in a space vehicle such as the space shuttle is described. The apparatus includes many latching assemblies carried by a platform on the vehicle and a like number of latching elements carried by the payload and adapted to mate with the latching assemblies. The novelty of the invention is believed to reside in the use of complementary hemispherical elements which automatically align and engage with one another. This enables a simple but effective mode of operation and avoids the need for hinged linkages and similar moving parts.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
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  • 3
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: A clamp-mount device is disclosed for mounting equipment to an associated I-beam and the like structural member of the type having oppositely extending flanges wherein the device comprises a base and a pair of oppositely facing clamping members carried diagonally on the base clamping flanges therebetween and having flange receiving openings facing one another. Lock means are carried diagonally by the base opposite the clamping members locking the flanges in the clamping members. A resilient hub is carried centrally of the base engaging and biasing a back side of the flanges maintaining tightly clamped and facilitating use on vertical as well as horizontal members. The base turns about the hub to receive the flanges within the clamping members. Equipment may be secured to the base by any suitable means such as bolts in openings. Slidable gate latches secure the hinged locks in an upright locking position. The resilient hub includes a recess opening formed in the base and a rubber-like pad carried in this opening being depressably and rotatably carried therein.
    Keywords: MECHANICAL ENGINEERING
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  • 4
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: A self-aligning electrical connector device includes a receptacle component having a conically contoured interior and a plug component having a correspondingly contoured conical body receivable in the receptacle component. The plug component has a number of spaced conductive ring elements with a mating face and the receptacle component includes corresponding spaced conductive ring elements providing mating interface with the mating face of the ring elements of the plug component when connected to it. Each ring element of the receptacle component has several segmented portions which defect downwardly when the plug component is inserted. A biasing force is asserted against the face of the ring elements of the plug component providing positive electrical contact and connection between the ring elements of the components.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
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  • 5
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-06-28
    Description: Rotational alinement not critical in design useful for remote manipulators. Plug and socket pushed together, plug rings deflect spring segments of corresponding socket ring. Particularly suitable for remote manipulators and making connections in "blind" locations.
    Keywords: ELECTRONIC COMPONENTS AND CIRCUITS
    Type: MFS-25211 , NASA Tech Briefs (ISSN 0145-319X); 8; 1; P. 08
    Format: text
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  • 6
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: The invention relates to an end effector device for robot or teleoperated type space vehicle which includes an inflatable balloon member carried on the end of tubular member which has a hollow center or conduit through which a suitable pressurized fluid is supplied. The device may be inserted into a variety of shaped openings or truss-type structures for handling in space.
    Keywords: MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT
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  • 7
    Publication Date: 2019-06-27
    Description: An apparatus for producing a structure in outer space from rolls of prepunched ribbon or sheet material that are transported from the earth to the apparatus located in outer space is described. The apparatus spins the space structure similar to a spider spinning a web utilizing the prepunched ribbon material. The prepunched ribbon material is fed through the apparatus and is shaped into a predetermined channel-shaped configuration. Trusses are punched out of the ribbon and are bent downwardly and attached to a track which normally is a previously laid sheet of material. The size of the overall space structure may be increased by merely attaching an additional roll of sheet material to the apparatus.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
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  • 8
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-06-28
    Description: End effector serves as "hand" for remote manipulator spacecraft system to grasp objects of various sizes. Device has built in flexible wrist joint "cartilage" for increased gripping force without significant strain on mechanical connections.
    Keywords: MACHINERY
    Type: MFS-23692 , NASA Tech Briefs (ISSN 0145-319X); 5; 2; P. 215
    Format: text
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  • 9
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: A payload retention concept that may be utilized on Space Shuttle missions is investigated. This concept appears to embody all the desirable features for the very demanding requirements for space flight. Desirable features include light weight, low cost, high reliability, excellent load distribution, versatility, and insensitivity to critical alignment.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-TM-82505 , NAS 1.15:82505
    Format: application/pdf
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  • 10
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-06-28
    Description: Quick-connect/disconnect clamp attaches instruments or equipment to I-beam, or similar flanged structures, without use of tools or much force.
    Keywords: MACHINERY
    Type: MFS-25510 , NASA Tech Briefs (ISSN 0145-319X); 8; 1; P. 115
    Format: text
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