A structural member for a window comprising two extrusions spaced apart and coupled to each other using an insulating coupler extending at least 40 mm apart to form the structural member and hinder thermal bridging. A stiffener extends inside the structural member between the extrusions to stiffen the structural member and comprises two spaced apart ends engaged with the two extrusions, respectively. The two ends are coupled to each other using an insulating stiffener coupler to support the stiffener and hinder thermal bridging. A method of forming a thermally broken structural member.

An arrangement for spreading apart at least two door leaves which are part of an item of furniture and are hingedly interconnected, from a folded position into a spread-apart position, includes an energy accumulator and a spreading element impinged by the energy accumulator. The spreading element comprises a pivotally supported lever arm with a free end, and a control contour is provided for controlling movement of the spreading element.

A stiffener for, and a method of, stiffening a structural member of a window are disclosed. The structural member has first and second ends thermally separated from each other. The stiffener comprises a first stiffener end configured to engage with the first end and spaced apart from the second end, and a second stiffener end configured to engage with the second end and spaced apart from the first end. An insulating stiffener coupler couples the first stiffener end to the second stiffener end to hinder thermal bridging of the first stiffener end and the second stiffener end. The method includes engaging frictionally the first extrusion with a first stiffener structure, engaging frictionally the second extrusion with a second stiffener structure, and coupling the first stiffener structure and the second stiffener structure to each other using an insulating stiffener.

A cover device which covers an upper part of a mounting work space of a component mounting machine includes: an openable/closable cover including a first cover portion swingable around a first swinging shaft line and a second cover portion attached to a free end of the first cover portion to be swingable around a second swinging shaft line; and a guiding device which stably holds the openable/closable cover in a half-opened state and in an entirely opened state. To hold the half-opened state of the openable/closable cover, a guide rail is provided with a downwardly curved portion at an intermediate portion of the guide rail, and a flip-up type guide provided above the curved portion.

A swinging-sliding door module for a rail vehicle is provided, the swinging-sliding door module including a door leaf and a rotatably mounted rotary pillar coupled to the door leaf. Furthermore, the swinging-sliding door module includes a support which is oriented longitudinally in the sliding direction of the door leaf and is mounted so as to be displaceable transversely with respect to the longitudinal extent thereof in the horizontal direction in relation to the rotary pillar and in which the door leaf is mounted displaceably. A first over-center locking brings about the deployment movement of the support. Furthermore, the coupling between rotary pillar and door leaf includes a second over-center locking which acts in the deployment direction of the door leaf.

A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.

In a preferred embodiment, a telescoping panel door for an aircraft compartment includes a first panel configured for hinged connection to a surface of a door frame, a second panel, and a linkage fixing a distance that the second panel can extend from the door frame, where the second panel is configured for connection to the door frame via the linkage. The door operates such that, in a closed position, the second panel is extended from an interior of the first panel, the first and second panels cooperate to completely cover an opening defined by the door frame, and the linkage is generally parallel to the plane defined by the door frame. In an open position, the second panel is retracted into the interior of the first panel by operation of the linkage and the first and second panels are nested to reduce a distanced spanned by the panels.

In a preferred embodiment, a telescoping panel door for an aircraft compartment includes a first panel configured for hinged connection to a surface of a door frame, a second panel, and a linkage fixing a distance that the second panel can extend from the door frame, where the second panel is configured for connection to the door frame via the linkage. The door operates such that, in a closed position, the second panel is extended from an interior of the first panel, the first and second panels cooperate to completely cover an opening defined by the door frame, and the linkage is generally parallel to the plane defined by the door frame. In an open position, the second panel is retracted into the interior of the first panel by operation of the linkage and the first and second panels are nested to reduce a distanced spanned by the panels.

A vertical door system includes: a door having a door frame, the door frame having at least one frame section; an operator; two vertical supports configured to: (a) be installable on opposite sides of the door opening and (b) support the vertical door, at least one of the vertical supports having: a guide track on a surface of the vertical support facing toward the door opening; and a drive system having: an elongated threaded rod drivable by the operator via a gearing arranged between the operator and the threaded rod; and one or more blocks, each block comprising a guide track connecting portion that connects to a guide track so the connected block is freely movable along the guide track, each block having a through-bore for accepting the threaded rod so that the block is positioned on the threaded rod and is movable along the threaded rod.

In a preferred embodiment, a telescoping panel door for an aircraft compartment includes a first panel configured for hinged connection to a surface of a door frame, a second panel, and a linkage fixing a distance that the second panel can extend from the door frame, where the second panel is configured for connection to the door frame via the linkage. The door operates such that, in a closed position, the second panel is extended from an interior of the first panel, the first and second panels cooperate to completely cover an opening defined by the door frame, and the linkage is generally parallel to the plane defined by the door frame. In an open position, the second panel is retracted into the interior of the first panel by operation of the linkage and the first and second panels are nested to reduce a distanced spanned by the panels.