E05D2011/0072

ASSEMBLY COMPRISING A FURNITURE HINGE AND A COVERING
20220307302 · 2022-09-29 ·

An assembly including a furniture hinge having a first fitting portion configured to be fixed to a first furniture part, a second fitting portion configured to be fixed to a second furniture part, and a hinge axis hingedly connecting the first fitting portion and the second fitting portion to one another, and at least one cover configured to at least partially cover a gap formed between the first fitting portion and the second fitting portion. A fastening device for fixing the cover to the furniture hinge is provided, and the fastening device includes an arresting device for fixing the fastening device on different positions of the cover in a longitudinal direction of the cover.

MULTI-JOINT LINK HINGE AND REFRIGERATOR INCLUDING THE SAME
20220034577 · 2022-02-03 ·

A multi-joint link hinge includes a hinge bracket, a plurality of links axially coupled to the hinge bracket, and a door bracket coupled to the plurality of links. The hinge bracket includes a base portion that defines a plurality of screw coupling holes at a vertical surface thereof, a plurality of side portions that extend from the base portion in a horizontal direction and are spaced apart from each other in a vertical direction, and a side surface portion that extends from the base portion in the vertical direction and defines a fixing groove. The plurality of links are coupled between the plurality of side portions along an axis that extends in the vertical direction. The multi-joint link hinge is used for a home appliance including refrigerators.

JOINT STRUCTURE FOR BATHROOM DOOR BODY OF AIRPLANE BATHROOM DOOR
20210387714 · 2021-12-16 ·

A joining structure of a door panel for a lavatory of an aircraft lavatory unit is provided. A plurality of pairs of end surfaces of a structural frame side hinge portion end surface and a door panel side hinge portion end surface facing each other in the vertical direction are alternately provided at intervals in the vertical direction. Bearing members each formed in a cylindrical shape and including a shaft insertion hole are disposed between at least two pairs of end surfaces adjacent to each other in the vertical direction, of the plurality of pairs of end surfaces. Both surfaces of the bearing member are in contact with each of the two pairs of end surfaces.

Safety guard for door gaps
11199047 · 2021-12-14 ·

A safety guard for door gaps preferably includes a telescoping tube cover, a compression spring, a top bushing, a top hinge tube and a bottom pin bushing. The telescoping tube cover includes a first tube and a second tube. The compression spring is inserted into first tube and the second tube is inserted into the first tube. The top bushing is inserted into a top of the second tube. The second bottom bushing is inserted into a bottom of the first tube. A second embodiment of the safety guard includes the telescoping tube cover, the top bushing, the top hinge tube, the bottom pin bushing and a fastener. A third embodiment of the door safety guard preferably includes a safety tube, a top pin bushing, the bottom pin bushing and an extra length hinge pin.

AIRCRAFT HINGE ASSEMBLY

A hinge assembly 8a for an aircraft component comprises first and second hinge plates 9, 10, each hinge plate including a plurality of fingers 13 to 17. The fingers of the first and second hinge plates are interleaved. A seal assembly 28 to 32 is provided between at least some of the fingers. The provision of a hinge including interposed fingers allows for a hinge assembly having a complex aerodynamic profile to be made, while the sealing function is performed by the seals filling the gaps between the fingers.

AIRCRAFT HINGE ASSEMBLY

A hinge assembly 8a for an aircraft component including first and second hinge plates 9, 10, having an aerodynamic surface. A first seal assembly 28 to 32 is provided and arranged to seal between the aerodynamic surfaces of the hinge plates. A second seal assembly 38 to 42 is arranged to seal between the undersides of the hinge plates in order to reduce pressure leakage between voids under the hinge. The provision of two seal assemblies, each having a dedicated function, addresses the competing demands made on the sealing arrangement of an aircraft hinge assembly in use.

Ligature-resistant hinge cap

A ligature-resistant hinge cap configured for use with a door hinge and generally including a body portion configured for mounting to the hinge, a flange extending rearward from the body portion, a rear side defined by the flange, and a front side opposite the rear side. The body portion includes a downwardly-extending stem configured to extend into a connecting portion of the hinge, and the front side is sloped.

Hinge stile gap blocking apparatus
11346151 · 2022-05-31 ·

This invention relates to a hinge stile gap blocking apparatus and to a method designed to prevent hand and finger injuries resulting from inadvertent door closures. The apparatus includes a pair of joined elongate members, each elongate member is joined to the other by an elastic band which extends through the opening of a door frame hinge stile gap with each joined elongate member residing on opposite sides of the hinge stile gap. The elongate members move when the door is pivoted, but are sufficiently tensioned against the hinge stile such that hands and fingers cannot be placed in the hinge stile gap when the door is open.

MANDREL FLEX CIRCUIT ROUTING

Cable assemblies for providing electrical communication between hinged sections of an electronic device are described. The cable assemblies can include a cover that covers one or more cables that run through a hinge region of the electronic device. The cable and cover can be drawn over a mandrel of the hinge region. The cover and the portions of the mandrel can be visible to a user at the hinge region of the electronic device. The cover can be sufficiently rigid to guide a path of the cable and protect the cable from bending beyond a prescribed angle during rotation of the electronic device at the hinge region. The cover can also be sufficiently rigid to prevent ceasing or folding of the cover and the cable during rotation of the electronic device at the hinge region.

Joint structure for bathroom door body of airplane bathroom unit
11718383 · 2023-08-08 · ·

A joining structure of a door panel for a lavatory of an aircraft lavatory unit is provided. A plurality of pairs of end surfaces of a structural frame side hinge portion end surface and a door panel side hinge portion end surface facing each other in the vertical direction are alternately provided at intervals in the vertical direction. Bearing members each formed in a cylindrical shape and including a shaft insertion hole are disposed between at least two pairs of end surfaces adjacent to each other in the vertical direction, of the plurality of pairs of end surfaces. Both surfaces of the bearing member are in contact with each of the two pairs of end surfaces.