Abstract:
A horizontally sliding door or some other type of translating door includes a chain, cable, or some other elongate member for moving a door panel across a doorway, and the door also includes a sensor that monitors the tension or slackness of the elongate member to determine whether the door panel encounters an obstruction in the doorway. In some embodiments, a proximity sensor detects slackness in the elongate member by sensing when the member droops away from or toward the sensor. The elongate member can have some sections that are more elastic than others to increase the drooping action.
Abstract:
This invention relates to a procedure for hardening the bearing surfaces (H1,H2,H3,H4) of a shaft or axle, in particular a crankshaft (2) or camshaft, in which the bearing surfaces (H1-H4) to be hardened are hardened sequentially with the shaft or axle turning around their longitudinal axis (L) by means of a heating and quenching device (3), in which the distortion of the shaft or axle that arises in the area of the respective bearing surface (H1) during the course of hardening is determined, in which the shaft or axle is supported by at least one supporting device (9) during hardening of a bearing surface (H1-H6), which is placed against a previously hardened bearing surface (H1), and in which the setting of the supporting device (9) is regulated taking into account the distortion determined for the bearing surface (H1), against which the supporting device (9) is placed, and a device which enables hardening of crankshafts with a minimal distortion.
Abstract:
A generally horizontally sliding door includes a sliding or otherwise translating door panel with a full-perimeter seal that engages sealing surfaces upon closing and at least partially disengages the surfaces upon opening. The door panel travels along an overhead track that is slightly inclined to lower the panel's upper and lower edge seals into engagement with sealing surfaces as the door closes. To provide a substantially full-perimeter seal, a leading edge seal and a trailing edge seal engage sealing surfaces as well. Some of the edge seals are joined to create corner seals. The seals are adapted for single panel sliding doors, bi-parting doors, multi-panel doors, and various combinations thereof.
Abstract:
In a switch, particularly a window lifter switch, with a housing, a switching rocker which is mounted in the housing and is associated with electrical contacts, and with a button which is likewise mounted in the housing, the button is acted upon elastically so that it is mounted free from play in the housing.
Abstract:
A resilient, insulated door panel for a sliding door includes a resilient core protected by a compliant outer covering with a seal disposed about the perimeter of the panel. The panel has sufficient resilience to recover from an impact that temporarily deforms it, yet has sufficient rigidity to transmit a compressive force needed for effectively setting the seals. Much of the core is filled with air to not only provide effective insulation and resilience, but to also provide an extremely lightweight door panel that can be operated to travel rapidly along an overhead track. Some embodiments include relatively rigid backup plates that provide a solid foundation to which the perimeter seals can be attached. The backup plates are segmented so as not to completely restrict the flexibility of the door panel.
Abstract:
In a process and an apparatus for the avoidance of airplane collisions in which at least one light source of a light flash warning apparatus on an airplane generates light flashes at periodic intervals, light flashes with a constant frequency are emitted from a first light source and light flashes with a variable frequency are emitted from a second light source, thereby increasing the warning effectiveness, localizing capability and, thereby, safety during operation of the airplane.
Abstract:
An inductor is provided for the simultaneous inductive heating of two tracks or ways which are formed next to one another on a metallic workpiece, having a first segment which is associated with the first track or way and a second segment which is associated with the second track or way, and having two supply arms via which the segments can be connected to a power supply. To enable two tracks or ways to be heated simultaneously to the hardening temperature without heating the material portion situated between the tracks or ways the segments of the inductor and the supply arms are connected together in an inductor in such a way that the fields travelling at right angles to the longitudinal extent of the tracks or ways neutralize each other in the region of the material portion which separates the tracks or ways from one another.
Abstract:
A method for simultaneously hardening a group of cams on a camshaft comprises first heating the group of cams at low power for at least one heating interval, then pausing the heating for a pause interval during which no power is applied to the group of cams, and then subsequently heating the group of cams at high power for one heating interval. The pause intervals, during which no power is applied to the group of cams, are sufficient as to allow heat stored in the cams to distribute uniformly throughout the cams. Each group of cams is hardened by a linear inductor and the regions of the camshafts that are not to be hardened are shielded by a cooling device.
Abstract:
The degradation of harmful substances in water by compounds, such as hydrogen peroxide, which form hydroxyl radicals under UV irradiation in continuous reactors is improved when the irradiation is carried out in a reactor with a specific reactor volume of at least 10 liters per kW of the UV radiator or radiators, and if the amount of water to be treated is 0.25 to 25 times the amount of the intrinsic volume of the reactor flows through the reactor per hour. It is particularly preferred that the water volume per hour to be treated is 0.25 to 10 times the intrinsic reactor volume.
Abstract:
In a process and an apparatus for the avoidance of bird impacts on airplanes by means of at least one light-flashes generating light source on an airplane, for which the frequency of the generated light flashes is varied through at least one cycle, the flash frequency is varied dependent upon the speed and/or the altitude and/or the acceleration of the airplane in order to provide an optimal flash frequency range for all take-off and landing phases and at the same time to be independent of a load and the type of airplane.