Abstract: Methods and systems are described for binding attributes between visual components. A first visual component, including a first presentation space for presenting first data by an operating first application, is detected. Binding information, for the first application, is identified that specifies a mapping between a first visual attribute of the first visual component and a second visual attribute of a second visual component including a second presentation space for presenting second data by a second application. A change to the first visual attribute is detected. In response to the detection of the change, change information is automatically sent to change the second visual attribute according to the mapping.

Abstract: Methods and systems are described for managing operation of an automotive vehicle. Vehicle information, about an automotive vehicle, is received. The automotive vehicle has a current operational configuration for constraining an operation of the automotive vehicle. Device information, about a portable electronic device, is received. A detection is made, based on the vehicle information and the device information, that an operator of the automotive vehicle is a device user of the portable electronic device. In response to the detection, change information is sent to change the current operational configuration to alter a constraint on the operation of the automotive vehicle.

Abstract: Methods and systems are described for selecting a resource based on a measure of a processing cost. Resource information is received identifying a first resource and a second resource for processing by a program component. One or more of a first measure of a specified processing cost for the processing of the first resource and a second measure of the processing cost for the processing of the second resource is determined. One of the first resource and the second resource is selected based on at least one of the first measure and the second measure. The selected one of the first resource and the second resource is identified to the program component for processing.

Abstract: The invention essentially concerns an aircraft seat (1), comprising control units (17.2, 22.2, 27), at least one node (11-15) to execute a particular action or function, and a display (22.1) for viewing video data. Said node (11-15) and said display (22.1) are capable of being actuated by the control units (17.2, 22.2, 27). A keyboard (17.1) for transmitting a command signal addressed to the control units (17.2, 22.2, 27) is connected to said control units (17.2, 22.2, 27). The control units are shared between the display (22.1), the key board (17.1) and the node (11-15).

Abstract: Methods and systems are described for providing steering-control feedback to an operator of an automotive vehicle. First attribute information is received that identifies a first attribute of a first operator coupling of an operator, of an automotive vehicle, to a steering-control mechanism of the automotive vehicle. A specified steering-control criterion is detected as met based on the first attribute. Feedback information is identified based on the steering-control criterion. In response to the detecting, the feedback information is sent to present, via an output device, a feedback indicator to the operator.

Abstract: Methods and systems are described for navigating between visual components. A first visual component, of a first operating application in a plurality of operating applications, is detected in a first application region of a presentation space of a display device. A first navigation control is presented, in a first navigation region determined based on the first application region, for navigating to a second visual component, of a second application in the plurality, in a second application region in the presentation space. A user input corresponding to the first navigation control is detected. In response to the detected user input, navigation information is sent to navigate to the second visual component.

Abstract: The invention essentially concerns an aircraft seat (1), comprising control units (17.2, 22.2, 27), at least one node (11-15) to execute a particular action or function, and a display (22.1) for viewing video data. Said node (11-15) and said display (22.1) are capable of being actuated by the control units (17.2, 22.2, 27). A keyboard (17.1) for transmitting a command signal addressed to the control units (17.2, 22.2, 27) is connected to said control units (17.2, 22.2, 27). The control units are shared between the display (22.1), the keyboard (17.1) and the node (11-15).

Abstract: This invention relates to a control and safety circuit (1) for gas delivery valves, comprising an actuator (50) opening the gas delivery valve; a control unit (100) intended to emit a command signal (V2) to activate the actuator and switch on the valve, and a clock signal (CK); and a memory (5) placed between the control unit (100) and the actuator (50). The memory is capable of receiving the command signal (V2) and the clock signal (CK) as inputs, and at the same time emits an output signal (V3) which is a function of the input command signal (V2) and a clock signal (CK). The output signal (V3) is sent to the actuator (50) to command the same to open the valve.

Abstract: A method is provided for controlling the feed of a combustible gas by a valve device placed in a feed pipe which has a gas inlet section and a gas outlet section. The device includes a valve seat in the pipe associated with a membrane-operated plug and a device for returning the plug to a position in which the valve seat is shut off. The method includes the steps of creating a pressure difference in a section of the pipe downstream of the plug with respect to the direction of flow, by a constriction in the pipe having a predetermined cross section, the pressure difference being defined by a first pressure upstream of the constriction and a second pressure downstream of the constriction; collecting the signal formed by the second pressure downstream of the constriction and making the second pressure act on the side of the membrane opposite that on which the first pressure acts; and generating a regulatable load on the membrane of the membrane operating system.

Abstract: The invention essentially concerns an aircraft seat (1), comprising control units (17.2, 22.2, 27), at least one node (11-15) to execute a particular action or function, and a display (22.1) for viewing video data. Said node (11-15) and said display (22.1) are capable of being actuated by the control units (17.2, 22.2, 27). A keyboard (17.1) for transmitting a command signal addressed to the control units (17.2, 22.2, 27) is connected to said control units (17.2, 22.2, 27). The control units are shared between the display (22.1), the key board (17.1) and the node (11-15).

Abstract: A device for controlling a combustible gas supply to a burner is provided, which includes first and second servovalves, having respective valve seats associated with a corresponding shut-off mechanism, which include respective first and second control solenoid valves with an electromagnetic operating device that controls the opening/closing of the corresponding servovalve. The solenoid valves act to indirectly control the corresponding servovalve's respective shut-off mechanism. The pipes of the control are in communication with the main pipe through an auxiliary bleed pipe. A pilot pipe is branched from the auxiliary pipe to supply a pilot burner, and a thermoelectric magnetic unit with a knob is provided on the auxiliary pipe, which allows gas to flow towards the pilot burner when the unit is activated, while simultaneously shutting off the flow of gas towards the servovalve control circuit. The device includes a control mechanism, controlled by the knob, which controls gas flow.

Abstract: The invention essentially concerns an aircraft seat (1), comprising control units (17.2, 22.2, 27), at least one node (11-15) to execute a particular action or function, and a display (22.1) for viewing video data. Said node (11-15) and said display (22.1) are capable of being actuated by the control units (17.2, 22.2, 27). A keyboard (17.1) for transmitting a command signal addressed to the control units (17.2, 22.2, 27) is connected to said control units (17.2, 22.2, 27). The control units are shared between the display (22.1), the key board (17.1) and the node (11-15).

Abstract: The invention relates to a network of switched optical fiber for airplane seats. The network connects the screens of the seats to each other and to a server via an optical fiber. The network includes optical switches of the MEMS type including mirrors, said switches being provided perpendicular to each seat. Each switch delivers the light beam in the optical fiber to the screen with which it is connected and re-amplifies it in the optical fiber when it is powered, while the switch directly delivers the light beam to the following seat when it is not powered.

Abstract: A flame atmosphere analyzer is described, for operation with combustible gases, including a tube in which an intake and air and gas mixing chamber is formed, a first gas supply nozzle and means for supplying primary combustion air opening into said intake chamber, and a flame burner in fluid communication with the intake and mixing chamber for supplying an air and gas mixture, formed in the chamber, to the burner. The analyzer includes a second gas supply nozzle, which is slidably guided in the tube, and an actuator provided on the tube and operable from outside the tube, for moving the second nozzle between an inoperative first position, in which the gas is supplied through the first nozzle, and an operational second position, in which the gas is supplied through the second nozzle, the first nozzle having no effect on the supply of the gas in the second position.

Abstract: The invention essentially concerns an aircraft seat, comprising control units, at least one node to execute a particular action or function, and a display for viewing video data. The node and the display are capable of being actuated by the control units. A keyboard for transmitting a command signal addressed to the control units is connected to the control units. The control units are shared between the display, the keyboard and the node.

Abstract: The invention essentially concerns an aircraft seat, comprising control units, at least one node to execute a particular action or function, and a display for viewing video data. The node and the display are capable of being actuated by the control units. A keyboard for transmitting a command signal addressed to the control units is connected to the control units. The control units are shared between the display, the keyboard and the node.

Abstract: A fireplace is provided, in which a flame can be lit. The fireplace including a warning system, which includes a proximity sensor to detect the presence of object within an active volume, the volume surrounds at least a portion of the fireplace. The system also includes an alarm device to emit an alarm signal, a clock to calculate a time elapsed since the switching off of the fireplace, and a processing unit receiving as input data from the clock and the proximity sensor, and outputting command signals to the alarm device. The alarm device is activated by the processing unit to generate an alarm signal when an object is detected by the proximity sensor as entering the active volume and the fireplace has been switched off since no later than a first pre-defined time interval. Also provided is a method for warning when an object enters the active volume of a fireplace.

Abstract: A device for controlling a gas supply to a burner includes a main duct, which is provided with at least one main valve including a valve seat and associated shutter with a control for opening the seat in opposition to a resilient recall member. A pilot duct leads from the main duct to supply a pilot burner, the main duct includes a magnetic thermoelectric safety unit which is manually or automatically armed, acting on the pilot duct to enable gas to flow to the pilot burner when armed. The pilot duct includes a pressure regulator having a shutter with a membrane control, the membrane subject to pressure regulated by the regulator and to a calibration pressure determined in a calibration chamber of the regulator. The device includes a fluid connector between the calibration chamber and the main valve to provide a pressure signal correlated with the gas supply pressure.

Abstract: A valve unit for controlling the delivery of a combustible gas, in particular for delivery via a gas metering apparatus including a main gas through-flow pipe (2), the unit comprising a servovalve with a first valve seat (3) provided on the pipe and associated with a respective first shutter (6) with diaphragm control (7) for the opening of the seat (3) in opposition to a first return spring (22), an operating chamber (10) for controlling the servovalve, the chamber being in communication with an inlet section (4) of the main pipe (2), upstream of the first valve seat (3), one side (7a) of the diaphragm (7) being subjected to the pressure prevailing in the chamber (10), the other side (7b) being subjected to the pressure prevailing downstream of the first valve seat, in the region of an outlet section (5) of the pipe (2), the operating chamber (10) being in communication with the outlet section (5) via a second valve seat (9) co-operating with a second shutter (8).

Abstract: A device is provided for controlling a gas supply to a burner, having a draft shut-off device and includes a main gas supply pipe with first and second servovalves therein, which include respective valve seats associated with corresponding shut-off members with diaphragm control for opening the seats in opposition to a resilient return member. A pilot pipe branched from the main pipe supplies a pilot burner. A thermoelectric magnetic safety unit is provided on the main pipe, acting to allow gas to flow towards the pilot burner when the unit is activated. The draft shut-off device includes a corresponding shut-off member movable from and towards a position in which an exhaust pipe is shut off, and a diaphragm-controlled pneumatic actuator of the shut-off member, the diaphragm forming a corresponding control chamber of the shut-off member which is in fluid communication with an auxiliary pipe section branched from the main pipe.