Abstract: A mounting device includes a cradle including a first recess and configured to be mounted in a vehicle, a pivotable hinge member coupled to the cradle, and a docking tray coupled to the pivotable hinge member. The docking tray is configured to lock in a first position within the first recess in the cradle, and lock in a second position extending outward from the first recess in the cradle. The docking tray includes a second recess shaped and dimensioned to receive an electronic computing device.

Abstract: A mounting device includes a cradle including a first recess and configured to be mounted in a vehicle, a pivotable hinge member coupled to the cradle, and a docking tray coupled to the pivotable hinge member. The docking tray is configured to lock in a first position within the first recess in the cradle, and lock in a second position extending outward from the first recess in the cradle. The docking tray includes a second recess shaped and dimensioned to receive an electronic computing device.

Abstract: A mounting device includes a cradle including a first recess and configured to be mounted in a vehicle, a pivotable hinge member coupled to the cradle, and a docking tray coupled to the pivotable hinge member. The docking tray is configured to lock in a first position within the first recess in the cradle, and lock in a second position extending outward from the first recess in the cradle. The docking tray includes a second recess shaped and dimensioned to receive an electronic computing device.

Abstract: A mounting device includes a cradle including a first recess and configured to be mounted in a vehicle, a pivotable hinge member coupled to the cradle, and a docking tray coupled to the pivotable hinge member. The docking tray is configured to lock in a first position within the first recess in the cradle, and lock in a second position extending outward from the first recess in the cradle. The docking tray includes a second recess shaped and dimensioned to receive an electronic computing device.

Abstract: A preparation of peptides eluted from class II HLA molecules is disclosed. Methods of decreasing measles infections comprising inoculating human patients with a vaccine comprising one or more of the peptides and methods of diagnosing measles infections or immunity comprising analyzing human patients for the presence of one or more of the peptides or antibodies to the peptide(s) are also disclosed.

Abstract: A preparation of peptides eluted from class II HLA molecules is disclosed. Methods of decreasing measles infections comprising inoculating human patients with a vaccine comprising one or more of the peptides and methods of diagnosing measles infections or immunity comprising analyzing human patients for the presence of one or more of the peptides or antibodies to the peptide(s) are also disclosed.

Abstract: A vaccine for preventing or treating Orthopoxvirus infection that induces a protective or therapeutic immune response, wherein the vaccine comprises (1) an amino acid sequence of 20 amino acid or less (preferably 12 amino acid or less and most preferably 11 amino acid or less) of the formula X1-SEQ ID NO:1-X2, wherein X1 and X2 are peptides of 0-11 amino acid in length comprising either native or non-native amino acid sequences, (2) an antigen-presenting cell pulsed with the peptide, or (3) a cell sensitized in vitro to the peptide is disclosed.

Abstract: A preparation of peptides eluted from class II HLA molecules is disclosed. Methods of decreasing measles infections comprising inoculating human patients with a vaccine comprising one or more of the peptides and methods of diagnosing measles infections or immunity comprising analyzing human patients for the presence of one or more of the peptides or antibodies to the peptide(s) are also disclosed.

Abstract: A power operated container crushing device, the device comprising: an upper housing; a lower housing integral with the upper housing; and a crushing mechanism comprising a motor attached to and retained in upper housing, wherein said motor includes a motor hear for rotational engagement with a drive gear; a drive axle with the drive gear fixably attached at one end for rotation thereof and means to attach the drive axle to a threaded sleeve at the other; an elongated threaded sleeve fixably attached to the drive axle for rotation thereof; a threaded shaft for threadably engaging the threaded sleeve; and a crushing plate fixably attached to the threaded shaft; wherein when the motor rotates the motor gear in one direction, the crushing plate moves in a downward direction, and when the motor rotates in the opposite direction, the crushing plate moves in an upward direction.

Abstract: A power operated container crushing device, the device comprising: an upper housing; a lower housing integral with said upper housing; and a crushing mechanism comprising a motor attached to and retained in said upper housing, wherein said motor includes a motor gear for rotational engagement with a drive gear; a drive axle with said drive gear fixably attached at one end for rotation thereof and means to attach said drive axle to a threaded sleeve at the other; an elongated threaded sleeve fixably attached to said drive axle for rotation thereof; a threaded shaft for threadably engaging said threaded sleeve; and a crushing plate fixably attached to said threaded shaft; wherein when said motor rotates said motor gear in one direction, said crushing plate moves in a downward direction, and when said motor rotates in the opposite direction, said crushing plate moves in an upward direction.

Abstract: An augmentor screech suppressor for a gas turbine engine includes a screech suppressor liner mounted on a screech housing and an actuator for translating the screech suppressor liner axially forward and aft, with the actuator located outside the outer duct of the engine. In a preferred embodiment in a variable cycle gas turbine engine, a variable area bypass injector (VABI) valve with a circumferentially conical surface slopes into the screech suppressor liner surface and inner and outer crank arms transfer linear motion from the actuator through the outer duct wall, cooperating with idler arms to translate the screech suppressor housing, and thus the VABI valve and screech suppressor linear, axially between open and closed valve position.

Abstract: A variable area bypass injector (VABI) for a variable cycle gas turbine engine includes a circumferentially continuous valve with a conical surface sloping into a screech suppressor surface, a circumferentially segmented seal attached to the diffuser, and a valve actuator located outside the outer duct of the engine. Each seal segment is spring loaded to allow for different axial movement between circumferentially adjacent segments, and has a seat portion complimentary to the valve conical surface for sealingly engaging the valve when in closed position. Additionally, the seal segments are shaped with a low aerodynamic profile and cooperate with the VABI conical surface, when the valve is in an open position, to provide an annular conic channel that keeps the bypass flow attached to the VABI valve and core flowpath walls as it is injected into the core gas stream.

Abstract: A thrust augmentor heat shield for enclosing radially extending fuel pipes which can be attached to and removed from the outer duct wall from within the augmentor. The heat shield includes a hollow, elongate housing extending substantially entirely along the length of the fuel pipe, a nose projecting forwardly from the housing and received within a slot formed in the duct wall and a bolt for clamping the housing to the duct wall and urging the nose of the housing into the slot. The housing includes an opening between the outer duct wall and the diffuser wall for conveying cooling air radially inwardly along the housing, and openings along lateral sides of the housing in registry with the fuel discharge ports of the fuel tube. The housing includes a diffuser flowpath segment such that, when the housings are arranged in a spoke pattern, the segments form a continuous annular wall joined by splined connections.

Abstract: A variable area bypass injector (VABI) seal for a variable cycle gas turbine engine includes a circumferentially segmented seal attached to the diffuser. Each seal segment is spring loaded to allow for different axial movement between circumferentially adjacent segments, and has a seat portion complimentary to a VABI valve conical surface for sealingly engaging the VABI valve when the VABI valve is in closed position. Additionally, the seal segments are shaped with a low aerodynamic profile and cooperate with the VABI valve conical surface, when the valve is in an open position, to provide an annular conic channel that keeps the bypass flow attached to the VABI valve and core flowpath walls as it is injected into the core gas stream.

Abstract: A stowable and self-deployable array antenna includes flat, rectangular antenna panels hinged side-by-side so that when deployed they are coplanar, and they fold like an accordion for stowing. The deployed array antenna is stiffened by lateral stiffening panels hingedly attached to every other hinge between antenna panels, and to the unhinged ends of the antenna panels. Foldable longitudinal stiffening panels hinged between adjacent lateral stiffening panels. Each hinged connection includes a pair of thin spring elements, corresponding to a portion of a cylinder. The two spring elements of each hinge are spaced apart with their concave sides facing, and with the axes of the defining cylinder parallel. The hinge pivots, when the spring elements buckle, about a line orthogonal to a line extending between the cylinder axes. The hinges are used as the structural elements of self-deployable masts. The mast may have a polygonal cross-section.

Abstract: A stowable and self-deployable array antenna includes flat, rectangular antenna panels hinged side-by-side so that when deployed they are coplanar, and they fold like an accordion for stowing. The deployed array antenna is stiffened by lateral stiffening panels hingedly attached to every other hinge between antenna panels, and to the unhinged ends of the antenna panels. Foldable longitudinal stiffening panels are hinged between adjacent lateral stiffening panels. Each hinged connection includes a pair of thin spring elements, corresponding to a portion of a cylinder. The two spring elements of each hinge are spaced apart with their concave sides facing, and with the axes of the defining cylinder parallel. The hinge pivots, when the spring elements buckle, about a line orthogonal to a line extending between the cylinder axes. The hinges are used as the structural elements of self-deployable masts. The mast may have a polygonal cross-section.

Abstract: An exhaust port liner assembly for use in a cylinder head of a vehicle engine composed of spaced inner and outer tubular metal shells having a mass of heat insulating material within the spaced shells and a gasket within the said spaced shells adjacent the outlet port. A metal cylinder head is cast around the spaced inner and outer shells while a removable insert is positioned within the spaced shells adjacent the outlet port. After casting of the metal cylinder head, the insert is removed and replaced by a gasket member.

Abstract: An improved hat with a visor having at least one pre-formed fold line along which the visor can be folded into a compact configuration for storing in a pocket or the like, without permanently distorting the visor.

Abstract: A grommet and strain relief for rubber covered wire and the like comprising a tapered rubber plug having one or more wire receiving bores extending through the plug and each normally sealed by a membrane which is ruptured as the wire is inserted. The ruptured membrane grips the covering of the wire and forms a weatherproof seal.