A split hinge made of a first hinge portion having a first cover that is operatively coupled to two first leaves, and a second hinge portion having a second cover that is operatively coupled to two second leaves. The first leaves, the second leaves, the first cover, and/or the second cover may have the same or different lengths. The first leaves may have first leaf lengths that are greater than or less than the first cover, while the second leaves may have second leaf lengths that are greater than or less than the second cover. The first cover may extend over the first leaves, the second cover may extend over the second leaves, and a portion of the first cover may extend over a portion of the second leaves or a portion of the second cover may extend over a portion of the first leaves to form the split hinge.

A method of attaching and detaching objects allowing for rotation wherein protrusions built in or attached to one object are forced into cavity sockets built in or attached to another by causing force resulting in momentary bending of protrusions or the cavities. The sequential bending causes curvilinear motion allowing protrusions to enter otherwise inaccessible cavity sockets. Once in, the components of the joining mechanism revert to natural position and an equilibrium is reached which keeps the objects attached, yet free to move around an axis. This equilibrium can only be disturbed by causing force at specific points on the mechanism and pulling the objects apart in a curvilinear motion, thereby detaching the objects in one continuous motion with little effort. Objects not permitting momentary bending can be attached with the mechanism housed in a casing. Permitted angles of rotation are controllable and attached objects can be locked in a position.

For a vehicle with at least one removable hardtop roof panel and a fixed hardtop rear rooftop, a hinge is provided that attaches to the removable panel(s) and the rear rooftop. In the case of the Jeep® Freedom Top®, both removable panels are attached to the rear fixed portion of the roof using the hinge, enabling the removable panels to be flipped over the rear of the roof.

An enclosure for protecting a load comprises a truck bed to hold items, a front wall affixed to a proximal end of a width of the truck bed, and a rear wall affixed to a distal end of the width. A main header member runs along the length of the truck bed connecting the rear and front walls to form a central mounting point along a length of the truck bed that is disposed at a maximum height of the rear wall and the front wall. A passenger side gull wing door and a driver side gull wing door are mounted to the main header member by a plurality of hinges affixed to the main header member and which provide a movable joint for the gull wing doors. One or more hydraulic lift cylinders are operative to raise and lower a respective gull wing door.

An aircraft door translation hinge assembly connects a passenger door of an aircraft to the aircraft fuselage structure and enables the passenger door to move through a desired opening motion. The opening motion of the passenger door is controlled by a simplified mechanism that utilizes a pair of linkages connected by a cam surface follower that engages in sliding engagement with a cam surface. The simplified mechanism controls a pivoting movement of the passenger door as the passenger door is first opened, and then controls a translation movement of the passenger door as the passenger door is continued to be opened from a passenger door opening in the aircraft fuselage.

A frame assembly supporting an overhead door has a horizontal header connected to upright columns or posts with splice assemblies. Fasteners mounted on the columns cooperate with retainers on the splice assemblies to position and connect the columns to the header. Hinge assemblies pivotally mount the door on the header for movement between open and closed positions.

Disclosed herein is a continuous hinge. The continuous hinge comprises a first hinge portion comprising a first plurality of knuckles; and a second hinge portion opposing the first hinge portion and comprising a second plurality of knuckles. The second plurality of knuckles is interdigitated with the first plurality of knuckles and pivotally coupled to the first plurality of knuckles. Each knuckle is a separate piece.

The safe door is a releasable door comprising a fire resistant body attached to a door jamb to provide privacy. Safe door comprises a frame less door panel attached to a door jamb by magnets engineered to release when a breakaway force is applied to the door in any direction. Safe door is assembled with welding and adhesive of a foam core, a fire sock and a protective sheet inside a cover of vinyl sheeting. The fire sock and cover are closed to prevent moisture penetration or disassembly to protect people and property. A handle on a handle side and a hinge on a hinge side attach where a traditional door may attach to allow door to move from an open position to a closed position.

The current invention is a set of improved hinges and setup to attach a panel to the hardtop roof of a vehicle. A device that can lock the removable roof or hardtop in an open position. In the preferred embodiment the hinges are comprised of two or more separate hinges with each hinge connected to each panel by one or more flaps. The flaps may be aligned using an alignment bracket. After opening the panels, the panels are folded back on the hinges and can be locked to the roof of the vehicles with one or more locks located on the sides of the roof. The current invention is more flexible and has a better alignment system the back panel being larger than the front panel. The current system has a double hinged system which is an improvement.

The invention relates to an opening system (10) for an auxiliary door (20) of an airplane in a fuselage (30), the door and the fuselage having skins in the extension of one another. In one exemplary embodiment, the system (10) includes a framing lintel (11) integrated into the fuselage, an upper beam (2S) of the door structure arranged opposite the lintel (11), and a set of three lever links (4A, 4B, 4C). Each link is connected, on the one hand, to the lintel (11) by a lever articulation (5a, 6a) fixed relative to the fuselage (30) and, on the other hand, to the upper beam (2S) by a lever articulation (5b, 6b) mobile with the door (20), the articulations (5a, 5b; 6a, 6b) being connected respectively to the lintel (11) and to the upper beam (2S) by fittings (41, 43; 42, 44). The set of links includes two types of link mounted alternately, in which the mobile articulation (5b, 6b) remains positioned respectively close to the fuselage skin (30) and further from this skin (30), the articulations (5a, 5b; 6a, 6b) of two adjacent levers (4A, 4B; 4B, 4C) forming an evolving quadrilateral.