Abstract:
An anti-sag management assembly includes a cross member operatively coupled at opposed first and second ends to brackets that are adapted for movable engagement with stationary portions of first and second telescoping slide assemblies. A slider movably engages the cross member. A first arm is operatively coupled to an arm bracket that is adapted for connection to a movable portion of the first telescoping slide assembly and to the slider. A second arm operatively coupled to a second arm bracket that is adapted for connection to the stationary portion of the first telescoping slide assembly and to the slider. Upon extension of the movable portion of the telescoping slide rail assemblies the slider is moved from a first operative position adjacent the second member bracket to a second operative position adjacent the first member bracket and upon retraction of the device the slider is moved from the second operative position to the first operative position.
Abstract:
A high R-rating window assembly storing multiple, reciprocating reflective flexible film layers defined by one or more parallel, displaced films or looped films define the layers. The layers are contained in a sealed housing between rigid transparent (e.g. glazed) layers. The glazed layers are separated on the order of 3 to 5-inches and are secured to low thermal conductivity framework pieces. The framework is capped with a motorized roller and film housing and the assembly is evacuated and filled with a desiccated, inert dry gas. Several plastic, reflective coated films are supported under tension in planar parallel relation between the glazing layers from the motorized roller and several guide rollers and guide tracks. Location sensors responsive to indicia on the films identify film position. Temperature sensors monitor ambient, internal and user set thermal conditions to control film exposure. The films are operable via a room control system and window controllers to define open, closed and partial exposure conditions. Alternative control functions may control film exposure in relation to room occupancy.
Abstract:
A method is provided for making a composite laminate aircraft skin for a fuselage in multiple composite panels. A resin-impregnated composite tape is placed on a lay-up surface of a mandrel tool to form the composite laminate aircraft skin as a barrel that is substantially the shape of a fuselage section. The barrel is cut into a plurality of panels on the mandrel tool, and at least one panel of the plurality of panels is transferred, individually and independently of all other of the plurality of panels, from the lay-up surface of the mandrel tool to a first cure tool of a plurality of cure tools having an aero surface tooled to an outer mold line. The at least one of the panels is cured on the first cure tool to form a cured composite panel. The first cure tool defines and controls the outer mold line of the at least one panel. The cured composite panel is removed from the first cure tool.
Abstract:
An anti-sag management assembly includes a cross member operatively coupled at opposed first and second ends to brackets that are adapted for movable engagement with stationary portions of first and second telescoping slide assemblies. A slider movably engages the cross member. A first arm is operatively coupled to an arm bracket that is adapted for connection to a movable portion of the first telescoping slide assembly and to the slider. A second arm operatively coupled to a second arm bracket that is adapted for connection to the stationary portion of the first telescoping slide assembly and to the slider. Upon extension of the movable portion of the telescoping slide rail assemblies the slider is moved from a first operative position adjacent the second member bracket to a second operative position adjacent the first member bracket and upon retraction of the device the slider is moved from the second operative position to the first operative position.
Abstract:
There is described a focusing apparatus having a deformable membrane that at least partially defines a cavity and an optical fluid disposed in the cavity. An actuator assembly can be provided for imparting a force to the deformable membrane. In one embodiment, the actuator assembly can include a piezoelectric actuator.
Abstract:
A connection system for connecting two or more marine propulsion devices together provides a coupler that can be rotated in place, without detachment from other components, to adjust the distances between the tie bar arms. In addition, the use of various clevis ends and pairs of attachment plates on the components significantly reduces the possibility of creating moments when forces and their reactions occur between the various components.
Abstract:
A jack plate is configured to allow removal of hydraulic components from a fixed portion of the jack plate without having to remove an outboard motor from the jack plate. A mechanical stop device is provided which supports a movable member of the jack plate relative to a stationary member of the jack plate and, as a result, supports the outboard motor even as the hydraulic components are removed from the jack plate. This allows the hydraulic cylinder, hydraulic pump, and motor to be removed from the jack plate by loosening and then detaching a removable bracket member from the jack plate. As a result, the hydraulic system can be inspected, maintained, or replaced without having to remove the outboard motor from the jack plate.
Abstract:
An apparatus and method for forming a composite workpiece are provided. An electromagnetic field generator induces a current in a susceptor, thereby heating the workpiece in a die cavity. An elastomeric bladder in the cavity is inflated and urges the workpiece against a contour surface corresponding to a desired configuration of the workpiece. Coolant fluid can also be circulated through the die cavity to cool the workpiece. Thus, the workpiece can be heated, formed, and cooled quickly and without substantial heating of other components, thereby reducing the time and energy relative to conventional forming methods.