Aircraft door (1) including an opening (4), a frame (3), a hinge structure (5) and a circular translation guide device designed to maintain the orientation of the opening (4) during the opening or closing thereof. The hinge structure (5) is connected to the opening (4) by a lifting arm (8) allowing a lifting movement of the opening (4) relative to the hinge structure (5). The circular translation guide device includes a single link (11) connected to the frame (3) by one of the ends thereof and by the other of the ends thereof to a lever (13) which is attached to the hinge structure (5).

A closure system includes a closure panel assembly and a hinge assembly configured to connect the closure panel assembly to a body. The hinge assembly includes a first hinge and a second hinge configured to be pivotably secured to the body and to the closure panel assembly in parallel, the hinge assembly establishing a four-bar linkage. The closure system includes a hinge cover configured to be fixed to the first hinge and pivotably connected to the closure panel assembly. The closure panel assembly is movable between a closed position and an open position via pivoting of the first hinge and the second hinge. The closure panel assembly at least partially covering an opening in the closed position and at least partially uncovering the opening in the open position. The hinge cover articulated alongside the first hinge and at least partially covers the first hinge in the closed position.

Aspects of the present invention relate to hinge apparatus (3-n) for supporting an aperture closure member (4). The hinge apparatus (3-1, 3-2) (3-n) is configurable in at least first and second configurations. The hinge apparatus (3-1, 3-2) (3-n) includes a first hinge bracket (10) (10) and a second hinge bracket (11) (11). A first hinge linkage member (15) is pivotally mounted to each of the first and second hinge brackets (10, 11) (10, 11). A second hinge linkage member (16) (16) is pivotally mounted to each of the first and second hinge brackets (10, 11) (10, 11). A latching mechanism (25) (25) is provided for selectively latching the hinge apparatus (3-1, 3-2) (3-n). The latching mechanism (25) (25) is operable to inhibit movement of the first and second hinge linkage members (15, 16) (15, 16) relative to each other to latch the hinge apparatus (3-1, 3-2) (3-n). The present invention also relates to a carrier assembly for carrying an aperture closure member (4); and a vehicle (1) having a carrier assembly.

Exemplary closure member systems for motor vehicles may include one or more power hinge assemblies, non-powered hinge assemblies, or both and are configured to displace a closure member to a fully open position of at least 100 degrees relative to its closed position. The hinge assemblies may embody a multi-axis design for moving the closure member between the closed and fully open positions. The closure member systems may be further configured to move the closure member along different swing paths during an opening sequence and a closing sequence.

The present invention is directed to a 4-bar kinematic link component and method for forming the 4-bar kinematic link using a single rotary molding tool. The invention eliminates the need to form individual components of the bracket from several different tools, which will then requires additional assembly steps. The 4-bar kinematic link is formed from two different materials each having a different in mold shrinkage value. This allows for hinge pins to be formed through a base component in a way that will prevent sticking of the components together thereby allowing the parts to have it relative to one another using the hinge pin. The final component is a 4-bar kinematic link that can be used as a 4 bar link mechanism for providing motion.

Aircraft door (1) including an opening (4), a frame (3), a hinge structure (5) and a circular translation guide device designed to maintain the orientation of the opening (4) during the opening or closing thereof. The hinge structure (5) is connected to the opening (4) by a lifting arm (8) allowing a lifting movement of the opening (4) relative to the hinge structure (5). The circular translation guide device includes a single link (11) connected to the frame (3) by one of the ends thereof and by the other of the ends thereof to a lever (13) which is attached to the hinge structure (5).

An opening and closing device includes an upper arm and a lower arm spaced apart in an up-and-down direction and extend between a vehicle door and a vehicle body, a connecting member connecting first end portions of the upper and lower arms, a body-side upper hinge and a body-side lower hinge attached to the vehicle body supporting the connecting member rotatably, a door-side upper hinge attached to the vehicle door to support a second end portion of the upper arm rotatably, a door-side lower hinge attached to the vehicle door to support a second end portion of the lower arm rotatably, and a driving device causing the upper and lower arms to rotate about a first and second rotational axes, and the driving device is attached to the connecting member.

A hinge assembly for a vehicle closure panel includes a body mounting member configured to mount the hinge assembly to a vehicle body, a closure panel mounting member configured to mount the hinge assembly to the vehicle closure panel and a hinge connecting arm pivotally connected by a first pivotal connection at a first end to the body mounting member and pivotally connected by a second pivotal connection at a second end to the closure panel mounting member. A first fastening member is movably received by the closure panel mounting member. A first stop member limits movement of the first fastening member in a first direction toward the closure panel mounting member. A second stop member limits movement of the first fastening member in a second direction away from the closure panel mounting member.

A refuse vehicle includes a body including a cab, a door assembly, and a linkage assembly. The door assembly is coupled to the cab and includes a first door panel and a second door panel. The first door panel is rotatably coupled to the second door panel and has an unfolded position and a folded position. The linkage assembly is configured to reposition the door assembly between a closed position and an open position relative to the cab. In a first state the door assembly is in the closed position the second door panel is in the unfolded position, and in a second state the door assembly is in the open position and the second door panel is in the folded position. The linkage assembly may include a first linkage coupled between the cab and the door assembly and a second linkage coupled between the cab and the door assembly.

A hinge assembly for securing a flap to a vehicle body includes a first hinge part which can be moved between a closed position and an open position for securing to a vehicle body, a second hinge part which can be moved between a closed position and an open position for securing the flap to be mounted relative to the vehicle body, and a deployment securing device for locking the second hinge part relative to the first hinge part. The deployment securing device has a first securing part which is paired with the first hinge part, a second securing part which is paired with the second hinge part, and a locking element and is configured such that the locking element is coupled to the first securing part in the closed position and is locked by the second securing part in a first locking position. The second securing part unlocks the locking element in the course of the movement of the second securing part from the closed position into the open position and thereby releases the locking element. The deployment securing device is configured such that after the locking element is unlocked in the first locking position, the locking element is moved into a second locking position in which the locking element produces a coupling between the first securing part and a third securing part paired with the first hinge part and locks the first securing part and the third securing part in the open position.