Patent application number | Description | Published |
20100281188 | Methods and Systems for Outlying Peripheral Device Management - Aspects of the present invention comprise systems and methods for detecting and managing peripheral devices that perform outside a given performance envelope. In some aspects, one or more threshold values may be determined prior to or during implementation by heuristic or other methods. These threshold values may then be used to determine device performance. In some aspects, threshold values may relate to performance parameters comprising device failures, consumption levels, output quality and other parameters. In some aspects, multiple threshold values may be used to determine device performance. In an exemplary aspect, a sheet usage threshold, a tone usage threshold and a power usage threshold may be used to determine if a device is an outlying device. In some aspects, performance below an excellence threshold value may indicate that a device has excellent performance. | 11-04-2010 |
20120083934 | MONITORING AND CONTROLLING ENERGY IN AN OFFICE ENVIRONMENT - A method for monitoring and controlling energy usage in an office environment is described. Energy usage information and sensor data are received from a status and control unit for an appliance. An appropriate energy profile for the appliance is determined. The energy profile is customizable by an end user based on preferences and schedules. The energy profile corresponds to appliances within an energy group. A control message is sent to the status and control unit to implement the determined energy profile. | 04-05-2012 |
20120302226 | Workspace energy management using multifactor presence detection and mobile phone identity verification - A workspace energy management method and system control the power state of workspace appliances using multi-factor presence detection and mobile phone identity verification. Multifactor presence detection substantially reduces the risk that workspace appliances will be powered-up in response to erroneous detection of presence at the workspace (e.g., false positive). Mobile phone identity verification, which verifies that the office worker's mobile phone is at the workspace (and thus that the office worker is also likely at the workspace) before workspace appliances are powered-up, prevents workspace appliances from being inadvertently powered-up by personnel other than the office worker, but without compromising worker privacy. | 11-29-2012 |
20130151656 | Globally Assembled, Locally Interpreted Conditional Digital Signage Playlists - Globally assembled, locally interpreted conditional digital signage playlists allow a global administrator with knowledge of content provider intentions but without knowledge of local data collection methods or local customs at digital signage deployments to assemble a conditional playlist on a global basis and be ensured that content items from the playlist will be displayed at all deployments in a manner conformant with content provider intentions, local data collection methods and local customs. | 06-13-2013 |
Patent application number | Description | Published |
20090269996 | REVERSE GATE FOR JET PROPELLED WATERCRAFT - A watercraft has a hull, a deck, an engine, a steering assembly, a jet pump, a venturi, a steering nozzle, and a reverse gate pivotable between a fully stowed position and a fully lowered position. The reverse gate includes a reverse gate body having inner and outer arcuate surfaces, and reverse gate upper and lower edges. First and second side walls are connected to the sides of the reverse gate body. At least one deflector is connected to at least one of the outer arcuate surface, the first side wall, and the second side wall. The at least one deflector is spaced from the outer arcuate surface. A deflector trailing edge is disposed upwardly and rearwardly from a deflector leading edge at least when the reverse gate is in the fully lowered position. Water deflecting surfaces and turning deflectors connected to a reverse gate are also disclosed. | 10-29-2009 |
20090325431 | METHOD OF INDICATING A DECELERATION OF A WATERCRAFT - A method of indicating a deceleration of a watercraft is disclosed. The method comprises creating a spray of water using a reverse gate of the watercraft. The spray of water extends above a water level of a body of water in which the watercraft operates. The spray of water is created when the reverse gate of the watercraft is in a lowered position and the watercraft is decelerating. An alternate method comprises creating a spray of water using a reverse gate of the watercraft only when decelerating the watercraft. A watercraft for carrying out at least one of the methods is also disclosed. | 12-31-2009 |
20100041286 | JET PROPULSION TRIM AND REVERSE SYSTEM - A watercraft has a jet pump and a venturi. A variable trim system (VTS) support and a reverse gate are rotationally mounted relative to the venturi. A steering nozzle is rotationally mounted to the VTS support. A rotary actuator has an output portion operatively connected to at least one of the VTS support and the reverse gate. Rotation of the output portion between a first angle and a second angle causes a rotation of the VTS support while the reverse gate remains in a stowed position relative to the steering nozzle. Rotation of the output portion between the second angle and a third angle causes a rotation of the reverse gate between the stowed position and a second position while the VTS support remains in a fixed position. A jet propulsion system and a method of operating a jet propulsion system are also disclosed. | 02-18-2010 |
20120003886 | DRIVESHAFT SEALING FOR A MARINE PROPULSION SYSTEM - A sealing unit longitudinally comprises first and second sealing sub-units disposed around first and second portions of a driveshaft of a marine propulsion system of a watercraft. The first sealing sub-unit is sealingly connected to a front wall of the hull and the engine casing. The second sealing sub-unit is sealingly connected to the driveshaft and a crankshaft. The second sealing sub-unit is disposed at least partially inside the first sealing sub-unit. An inside of the first sealing sub-unit is in fluid communication with a water intake ramp. An inside of the second sealing sub-unit is in fluid communication with an interior of an engine. The first sealing sub-unit prevents fluid communication between the water intake ramp and a portion of an inside of the hull. The second sealing sub-unit prevents fluid communication between the engine, the inside of the hull, and the water intake ramp. | 01-05-2012 |
Patent application number | Description | Published |
20110290947 | Automatic Method And Device For Aiding The Piloting Of An Airplane - The device ( | 12-01-2011 |
20120022725 | Method And Device For Updating A Target Altitude For An Emergency Descent Of An Aircraft - Method and device for updating a target altitude for an emergency descent of an aircraft. | 01-26-2012 |
20120056760 | Method And Device For Automatically Determining An Erroneous Height Value Of A Radioaltimeter Mounted On An Aircraft - Method and device for automatically determining an erroneous height value of a radio altimeter mounted on an aircraft. The device ( | 03-08-2012 |
20120146816 | Automatic Method And Device For Aiding The Piloting Of An Airplane - The device ( | 06-14-2012 |
20120150367 | Method And Device For Automatically Monitoring The Ability Of An Aircraft To Follow A Flight Trajectory With At Least One Turn - Method and device for automatically monitoring the ability of an aircraft to follow a flight trajectory with at least one turn. | 06-14-2012 |
20120215386 | Method And Device For Aiding The Flight Management Of An Aircraft - Method and device for aiding the flight management of an aircraft.
| 08-23-2012 |
20130103233 | AUTOMATIC LANDING METHOD AND DEVICE FOR AN AIRCRAFT ON A STRONG SLOPE RUNWAY - The device ( | 04-25-2013 |
20130135202 | INTERACTIVE DIALOG DEVICE BETWEEN AN OPERATOR OF AN AIRCRAFT AND A GUIDANCE SYSTEM OF SAID AIRCRAFT - Interactive dialog device between an operator of an aircraft and a guidance system of the aircraft. The dialog device includes an interaction on a screen which represents, on the one hand, a playback element indicating the value of a guidance setpoint of the guidance system of the aircraft, and on the other hand, a control element which can be grasped and moved along a curve by an operator to modify the value of the guidance setpoint. | 05-30-2013 |
20130190949 | VEHICLE ENERGY CONTROL SYSTEM - A system for controlling energy of a vehicle, for example an aircraft, comprising a control interface able to be in at least one first and one second state, the first state being an instruction state in which the interface generates at least a first instruction for speed of variation of a current energy of the vehicle and the second state being a resting state in which it gives no instruction, the interface furthermore being configured to return into the second state after having been brought into the first state. | 07-25-2013 |
20130211635 | INTERACTIVE DIALOG DEVICES AND METHODS FOR AN OPERATOR OF AN AIRCRAFT AND A GUIDANCE SYSTEM OF THE AIRCRAFT - Interactive dialog devices and methods are provided for use by an operator of an aircraft with a guidance system of the aircraft. The dialog devices and methods can include an interaction on a screen that can represent, on the one hand, a playback element indicating the value of a guidance target of the guidance system of the aircraft, and on the other hand, a control element that can be grasped or selected and moved on a display along a path, such as for example a curve, by an operator to modify the value of the guidance target. | 08-15-2013 |
20130215023 | INTERACTIVE DIALOG DEVICES AND METHODS FOR AN OPERATOR OF AN AIRCRAFT AND A GUIDANCE SYSTEM OF THE AIRCRAFT - Interactive dialog devices and methods can be installed on an aircraft for communication between an operator of the aircraft and a guidance system of the aircraft. A dialog device can include a global screen configured for displaying guidance information related to each of a navigation display, a vertical display, and a primary flight display. The global screen can include at least one graphic object which is produced in the form of an interaction element which represents a control feature that can be grasped and moved by an operator to modify a value of at least one guidance target of the guidance system associated with one or more of the navigation display, the vertical display, or the primary flight display. | 08-22-2013 |
20140277857 | METHODS, SYSTEMS AND COMPUTER READABLE MEDIA FOR ARMING AIRCRAFT RUNWAY APPROACH GUIDANCE MODES - Methods, systems, and computer readable media are disclosed for direct arming aircraft runway approach guidance modes, for example and without limitation, for aircraft operational. In some aspects, a method for directly arming a runway approach guidance mode of an aircraft includes displaying on a display unit an airport, selecting the airport and selecting an active runway for final approach, displaying an path toward the selected final approach runway, selecting the final approach runway, displaying on the display unit at least one symbol associated with at least one runway approach guidance mode, and arming at least one of the at least one runway approach guidance mode. | 09-18-2014 |