171 results about "Hinge line" patented technology

A cast or support for use in limiting movement of the anatomy to promote healing of an injured body part includes initially flexible and subsequently rigid double-knit material, or other casting blanks. There is a water-hardenable material impregnated into the casting blank. Certain areas of the blank have significantly reduced or no hardenable material. This construction may provide at least one hinge line which extends substantially across the double-knit material or other casting blank where the upper and lower layers are held in engagement with each other. The cast or support may be folded open along the hinge line to permit washing, inspection, or treatment of the portion of the anatomy to which the cast or support is applied or as one step in the preparation of a mold of a portion of the anatomy. More than one hinge line may be provided. Overlapping edges of the blank may also be of reduced thickness and with reduced hardening material to provide a smooth overlap to secure the cast or support in place.

An apparatus for deploying an air bag through an automotive dash panel (12) includes an air bag door (16) integrally formed in the panel and defined by a door perimeter including a frangible edge (18) of reduced cross section. A dispenser (20) supports the air bag (24) behind the door. A metal reaction plate (28) is positioned between the air bag (24) and the door (16). When the air bag inflates, it forces the reaction plate (28) to bend around a horizontal hinge line (36). As the reaction, plate pivots it concentrates inflation force along a lower portion of the frangible door edge. This helps to predictably separate the door from the dash panel by tearing along the lower door edge and allowing the tear to propagate up two side edges. In one embodiment, the tear also propagates across an upper edge to completely separate the door from the panel. At least one, and preferably two or three tethers (50) limit how far the door can travel during air bag inflation. A stop member may be included to limit reaction plate bending. After deployment, the reaction plate remains in a position that prevents the door from returning to its original position. A retaining structure may be included to preclude at least a portion of the air bag door from tearing free of the vehicle panel. A hinge (44) may be embedded in the panel in a position spanning a portion of the door perimeter. A hollow channel may be formed into the panel along the frangible marginal edge to create a substantial strength differential with the door perimeter to promote bending along the hinge and/or to help confine tearing to the frangible marginal edge during air bag deployment.

A flexible armor system includes a rigid panel of a stiffness calculated to resist penetration by a known ballistic object, made from multiple layers of Ultra High Molecular Weight Poly-Ethylene fibers or other high tenacity fibers, which is then pre-flexed beyond its elastic bending limit to create a distributed pattern of surface buckling, with localized areas of interior delamination, which together function as bending or hinge lines to provide flexibility to the otherwise rigid panel and thereby lower its overall stiffness to less than that calculated for the rigid panel to resist the ballistic object. The areas of delamination have a width of less than one half the diameter of the ballistic object.

A panel assembly for an aircraft including a panel having an upper aerodynamic surface and a leading edge, and a hinge fitting connected to an underside of the panel, defining a hinge line for the direction of rotation of the panel. The upper surface of the leading edge has an arcuate portion centered about the hinge line, and has an upturned portion forward of the arcuate portion. The panel assembly is pivotally connected to its hinge fitting to the trailing edge of the fixed wing portion and rotatable between a first position wherein the upper surfaces of the fixed wing portion and the panel are substantially flush, and a second position wherein the panel is rotated downwardly from the first position. A seal member attached to the trailing edge of the fixed wing portion, has a lower surface which seals against the upper surface of the panel during its movement.

A hinge lid container for smoking articles having a front wall, a rear wall and opposed side walls extending therebetween comprises: a box portion; and a lid portion hinged to the box portion along a hinge line extending across a rear wall of the container. At each side wall of the container, the angle □ between the front edge of the side wall of the lid portion and the lower edge thereof is greater than the angle □ defined between the rear edge of the side wall and a straight line extending between a first point (A) where the hinge line meets the side wall and a second point (B) where the upper edge of a front wall of the box portion meets the side wall.

A ramp assembly is suitable for use with a vehicle having a floor. The ramp assembly includes a ramp rotatably coupled within the vehicle, and a moving floor having an inboard panel and an outboard panel. The outboard panel has an outboard end hingedly coupled to the inboard end of the ramp to define an outboard hinge line that moves between a raised position when the ramp is in a stowed position and a lowered position when the ramp is in a deployed position. An outboard end of the inboard panel is hingedly coupled to an inboard end of the outboard panel. A reciprocating mechanism reciprocates an inboard end of the inboard panel between a lowered position and a raised position.

A fan variable area nozzle (FVAN) includes a flap assembly which varies a fan nozzle exit area. An actuator system drives a sliding drive ring relative a multitude of slider tracks mounted to a fan nacelle to adjust each flap of the flap assembly through the flap linkage to pitch the flap assembly about a circumferential hinge line to vary the diameter of the annular fan nozzle exit area between the fan nacelle and the core nacelle. The FVAN may be separated into a multiple of drive ring sectors which are each independently adjustable by an associated actuator of the actuator system to provide a low profile drag asymmetrical fan nozzle exit area.

A door seal system is provided for forming a seal between a closed door and its door frame. The system includes a unitary co-extruded seal member having first and second legs connected by a flexible hinge. A traditional flexible seal is formed along one leg and, preferably, a strip of intumescent material is formed along the other leg. The member can be folded flat along the hinge line for rolling into a compact storage and shipping configuration. For installation, a length is pulled from the roll, cut off, bent into a right angle along the hinge, and fixed to the door frame with one leg extending along the jamb and the other extending along the stop. The flexible seal bears and seals against the outside face of a closed door and the intumescent strip is positioned in the gaps between the door edges and the door frame.

A nacelle for an engine has outer and inner cowl doors that are independently rotatable about offset hinge lines. A connection device is provided for selectively connecting the outer and inner cowl doors so as to cause them to open simultaneously. The inner cowl door is arranged to rotate by a greater angle than the outer cowl door so as to improve access to the engine for maintenance purposes.

A flexible space structure such as a solar array is composed of multiple solar cell modules (SCMs) each supporting an arrangement of solar cells on a frontside layer and incorporating a backside layer with a surface opposite from the frontside layer having a conductive coating. A selected portion of the SCMs have structural ground extension harnesses intermediate the frontside layer and backside layer. Conductive tapes secure vertically adjacent SCMs by attachment to the conductive coating and electrical jumpers interconnect the structural ground extension harnesses across gapped hinge lines of laterally adjacent SCMs.

A fairing assembly is suitable for use with a heavy duty vehicle having a cab mounted to a frame, wherein relative motion occurs between the cab and the frame during vehicle operation. The fairing assembly extending downwardly from a lower portion of the cab and includes a fairing panel and a hinge for hingedly connecting an upper portion of the fairing panel to a lower portion of the cab. The hinge defines a hinge line extending in a generally longitudinal direction. The fairing assembly further includes a link having a first end rotatably connected to a lower portion of the fairing panel and a second end rotatably connected to the frame. The link substantially limits rotation of the fairing panel about the hinge line and rotates relative to the fairing panel to allow for relative motion between the frame and the cab.

A nacelle assembly provides thrust reverser doors and core cowl doors with separate thrust reverser door hinge lines and core cowl doors hinge lines for independent operation to eliminate the requirement of a lower bi-fi splitter. The removal of the lower Bi-Fi splitter provides improved aerodynamic packaging with improved performance by reducing drag in the bypass fan stream.

A ramp for directing the deployment of an expanding air bag may be formed to extend from a surface of a trim panel. The ramp may comprise one or more projections having a hinge or fold line. After molding of the trim panel, the projection may be folded along the hinge line towards the surface of the panel to form a ramp structure to promote the emergence, direction and/or placement of an expanding air bag. The ramp structure may be formed on any surface of trim panels lying adjacent or over an air bag system.

An attached lid container has lids that are hinged to the top edges of the side walls of the container. When the lids are closed, the free edges of the lids engage one another to form a joint that interlocks the lids together. The lids are attached to the container at the hinge joints after the molding of the container and lids, while the molded parts are still in the mold press. Specifically, the lids are molded next to the container and then moved laterally to be aligned with the hinge line of the container after the mold cavity is withdrawn. Then, the ejectors push the lids out toward the container. The force of the outward movement causes the hinge parts of the lids and container to snap together. Subsequently a robot arm removes the container from the mold press with the hinged lids assembled on the container.

This invention is a servo mounting system, which allows a servo with a rotating output shaft to directly power an aircraft control surface. A specially designed servo mount securely positions the servo with the central axis of its rotational output shaft on, and axially aligned with, the hinge line of the control surface it drives. The servo shaft and servo body are directly connected to the airframe and control surface, thereby conserving rotational motion while driving control movement. Electronic means are then used to control the neutral point and the limit of travel of the servo. The system eliminates lost motion without generating adverse linear loads within the drive assembly.

In a fabric enclosure such as a tent wall there is provided an opening in the fabric panel with a fabric closure panel for closing the opening having a hinge line along one side connecting the closure panel to the wall panel. The opening and the closure panel each define an edge thereof opposite to the hinge line which is curved from an end at the hinge line around to an opposite end at the hinge line with the edge of the closure panel overlapping the edge of the opening for closure thereon and a flexible bowing strip attached to the edge of the closure panel which is forced into a bowed shape to apply tension to the closure panel tending to maintain the panel flat.