Abstract: A light shelf for controlling solar radiation that impinges on a building has a panel with a pair of support brackets. The brackets run along tracks secured to the building and engage the tracks to assume a variety of elevations. The brackets can be moved independently, allowing the panel to be tilted and may have pivot joints to facilitate tilting. The panel may be mounted to the brackets in a way that allows the panel to translate horizontally. The panel may have a plurality of elements that can be adjusted to change the surface area and may be automated to respond to ambient conditions.
Abstract: A carrier for connection of a window pane to a window lift of a motor vehicle comprises guiding claws spaced apart from each other in a longitudinal direction of a guide rail of the window lift for guiding the carrier on the guide rail. The carrier includes a window pane holder for connecting the window pane with the carrier and an adjusting device for adjusting the position and/or orientation of the window pane with respect to the guide rail. To ensure an exact bearing of the window pane on an associated sealing contour on a motor vehicle body with simple constructive means, little mounting effort and few components, at least one guiding claw is adjustable in a direction vertical to the longitudinal extension of the guide rail or in longitudinal extension of the guide rail and vertical to the longitudinal extension of the guide rail.
Type:
Application
Filed:
June 25, 2010
Publication date:
December 30, 2010
Inventors:
Klaus Hampel, Juergen Knorr, Erik Langmann, Michael Rattei
Abstract: A hinge unit for hopper/awning window units (1), the window unit comprising a fixed frame (2) and a sash (3) capable of rototranslation about at least a first connecting point (F1) between a window unit (1) closed position and an open position; there being inserted between the fixed frame (2) and the sash (3) on both sides a pair of hinge units (4), each comprising: a supporting and guiding element (5) integral with the fixed frame (2); an arm (6) one end of which pivots at the sash (3); a first slide (7) slidably positioned along the supporting element (5) and forming the first connecting point (F1); connecting rod means (8, 9) connecting the first slide (7) to the arm (6) and designed to allow rototranslation of the arm (6) away from and towards the supporting element (5); a joint rod (10) between the arm (6) and the supporting element (5), its ends respectively pivoting at a distal point of the supporting element (5) and at the arm (6), so as to form a second connecting point (F2); there being adjusting me
Abstract: An structurally simplified actuation mechanism for swinging an aircraft door from a frame on an aircraft fuselage. The actuation mechanism includes a cantilever rotatably mounted to the frame and including a receiving region, a universal joint supported in the receiving region, and an actuation device disposed on the cantilever. The universal joint defines a vertical axis of rotation and is configured to receive a door fitting. The actuation device includes an output drive connected to the universal joint at the vertical axis of rotation.
Type:
Grant
Filed:
February 19, 2003
Date of Patent:
June 1, 2004
Assignee:
Eurocopter Deutschland GmbH
Inventors:
Holger Schreitmueller, Thomas Nickl, Thangaraju Nithyanandam
Abstract: A safety gate assembly includes a generally U-shaped frame (3), which may be secured across a door opening, stairway or the like, and a gate (8), one side of which is connected by one or more pivotal connections (4, 7) to one side of the frame (3) to permit pivotal movement of the gate with respect to the frame about a pivotal axis and the other side of which carries a projecting latch member (9), which cooperates with a latch (1) connected to the other side of the frame. The latch (1) defines an entry (32) for the latch member and a locking position (36), in which pivotal movement of the gate (8) is prevented. The pivotal connections (4, 7) are constructed to permit linear movement of the gate relative to the frame (3) in the direction parallel to the pivotal axis.