145results about How to "Quick restart" patented technology

When an engine restart request is given in an engine stopping period which begins at a point of fuel supply interruption and ends at a point of complete engine stop, an engine starting system judges whether TDC engine speed detected immediately before is equal to or lower than a specific value “A”, the counted number of reverse running motions of the engine is 0, and a piston in an expansion stroke cylinder is relatively close to TDC. If the judgment result is in the affirmative with all these conditions satisfied, the engine starting system injects fuel into the expansion stroke cylinder and then ignites and combusts a mixture produced therein. The engine starting system also injects the fuel into a compression stroke cylinder and then ignites and combusts a mixture produced therein when a piston in the compression stroke cylinder has gone beyond TDC.

The invention discloses a wireless illumination control system which comprises a remote controller, a system manager, a plurality of dimmers, a plurality of drivers and a plurality of lamps, wherein the remote controller is in coupling connection with the system manager; the system manager is in coupling connection with each dimmer; commands are sent to the system manager by the remote controller; the system manager is used for converting the commands into control signals and sending the control signals to the corresponding dimmer; the dimmers are used for converting the control signals into dimming control signals and transmitting the dimming control signals onto the corresponding drivers; each driver is used for ensuring the corresponding lamp to emit light on the corresponding brightness level according to the corresponding dimming control signal; a plurality of lamps can be divided into a plurality of groups; a plurality of groups of lamps correspond to the setting of G keys on the remote controller; and the setting of one group of G keys can be named one scene S. According to the invention, 50 or more dimmers can be conveniently controlled, a range of 50 meters can be covered and the energy consumption of the remote controller is obviously reduced.

Various systems and methods are described for controlling an engine in a vehicle, the engine being coupled to a transmission. One example method comprises, under selected braking conditions, shutting-off the engine and spinning-down the engine to rest while the vehicle is traveling, and in response to a foot-off-brake event, restarting the engine by at least partially engaging the transmission to assist in spinning-up of the engine from rest while the vehicle is traveling.

An abnormality diagnosis method for a gas concentration measuring device, includes electrically shutting off measurement means from an oxygen concentration detecting cell and an oxygen pump cell of a gas sensor when a voltage at one of electrical connection points through which the measurement means is electrically connected to the oxygen concentration detecting cell and the oxygen pump cell becomes equal to a predetermined abnormal voltage value, and thereafter, electrically connecting the measurement means to the oxygen concentration detecting cell and the oxygen pump cell of the gas sensor to perform an abnormality diagnosis of the gas sensor. An abnormality diagnosis apparatus for a gas concentration measuring device is also provided.

An internal-combustion-engine automatic stop and restart system according to the present invention is provided with a restarting control unit that performs restarting control of the internal combustion engine by making the pinion pushing unit push out the pinion gear so as to engage the pinion gear with the ring gear, when the restarting condition is satisfied in a time period from a time instant when the automatic stopping condition is satisfied to a time instant when the rotation of the internal combustion engine stops; and a throttle valve control unit that opens the throttle valve even when the restarting condition has not been satisfied and stops control of the throttle valve in a time period from a time instant when the rotation of the internal combustion engine stops to a time instant when the restarting condition is satisfied, when the rotation speed of the internal combustion engine becomes lower than a predetermined value in a time period from a time instant when the automatic stopping condition is satisfied to a time instant when the rotation of the internal combustion engine stops.

The invention relates to an architecture of a propulsion system of a multi-engine helicopter, comprising turboshaft engines (1, 2) that are connected to a power transmission gearbox (3), and comprising a low DC voltage onboard network (7) for supplying helicopter equipment during flight, characterised in that it comprises: a hybrid turboshaft engine (1) that is capable of operating in at least one standby mode during a stable flight of the helicopter; an electrotechnical pack (20) for quickly restarting said hybrid turboshaft engine in order to bring said engine out of said standby mode and to reach a mode in which it provides mechanical power, said restart pack (20) being connected to said onboard network (7); and at least two sources (4, 16, 18) of electrical power for said onboard network (7).

Provided are a multi-level converter having more than one converter arm in which a plurality of sub-modules are connected in series, multi-level converter comprising, a first bypass circuit connected in parallel to at least one sub-module included in more than one converter arm on a first side and including a first switching device, a second bypass circuit connected in parallel to more than one converter arm on a second side and including a diode, a second switching device included in more than one converter arm and having a first end connected in series to at least one sub-module and a second end connected to a first end of first bypass circuit at a single node and a third switching device included in more than one converter arm and having a first end connected in series to at least one sub-module and a second end connected to a first end of second bypass circuit at a single node.

A multidisk storage system (SD) equipped with a redundancy mechanism comprises at least two disk units (UND1-UND3), at least one redundancy control unit (UNC1-UNC2), a power distribution point (P), and a control unit (EG1-EG5), located in proximity to the point (P), for triggering the opening of the corresponding line (LI1-LI5) in case of an electrical fault in the associated unit and in the line itself. This system therefore ensures an optimal protection against electrical faults and ensures an optimal availability of the data.

A code generator and method for generating an orthogonal code for use in the baseband part of a transmitter or transceiver of a telecommunication system. An index conversion unit converts an index (k) into a modified index (j) associated with a corresponding code having a spreading factor greater than one and less than or equal to a maximum spreading factor. A logic unit performs logic operations on bits of the modified index (j) and a counter value (i) to generate a code bit of the orthogonal code. A number of parallel code generators may generate a number of orthogonal codes having respective spreading factors and indices.

In a fuel cell system in which load electric power is supplied from a fuel cell and a secondary battery, intermittent operation is performed, that is, operation of the fuel cell is stopped and the load electric power is supplied from the secondary battery in a low load region. At this time, a threshold value for stopping and starting the operation of the fuel cell is adjusted according to open circuit voltage. Thus, it is possible to prevent fuel from being unnecessarily consumed in order to maintain the open circuit voltage at a predetermined value when the operation of the fuel cell is stopped, and to improve response of the fuel cell when the operation of the fuel cell is restarted after the open circuit voltage has decreased in the fuel cell that has stopped generating electric power.

The invention relates to an architecture of a propulsion system of a multi-engine helicopter comprising turboshaft engines connected to a power transmission gearbox, characterised in that it comprises: at least one hybrid turboshaft engine (20) capable of operating in at least one standby mode during a stable cruise flight of the helicopter; at least two systems (30; 40) for controlling each hybrid turboshaft engine (20), each system (30; 40) comprising an electric machine (31; 41) connected to the hybrid turboshaft engine (20) and suitable for rotating the gas generator thereof, and at least one source (33; 43) of electrical power for said electric machine (31; 41), each reactivation system (30; 40) being configured such that it can drive said turboshaft engine (20) in at least one operating mode among a plurality of predetermined modes.

A system and method for fast restart of user apps on a user device. A host system hosts classes and resources of the user app, and a service app host application on the host system deploys an initial instance of the user app on the user device that includes additional instrumentation for enabling the user app to be quickly restarted on the user device with a set of changed classes and/or changed resources that comprise the latest version of the user app during development of the user app. This can significantly reduce the typically long turnaround time when developing and testing user apps as compared to current systems and methods. In a preferred embodiment, the system enables a fast restart of user apps running on Android user devices.

A hot standby power supply for a variable frequency drive of a floating vessel is provided. The variable frequency drive may power an electric motor of the floating vessel. The hot standby power supply includes a power input for receiving electric power from a main power supply of the floating vessel. The hot standby power supply also includes a first electric connection configured to supply electric power at a first voltage level to a converter power input of the variable frequency drive, and a second electric connection configured to supply electric power at a second voltage level to control power input of the variable frequency drive. The first voltage level is higher than the second voltage level. A transformer is further provided for transforming received electric power to the first voltage level or to the second voltage level.

A disaster recovery technology capable of achieving the high-speed FO and correctly reading the logs even if the unit of logs written in the main site is large is provided. In the disaster recovery system comprising a main site and a sub-site, when the writing in units of a log block consisting of a plurality of log records is performed in the main site and the logs are applied in the sub-site, the log blocks are read from the sub-storage to verify the consistency, and it is determined whether the reading process conflicts with the writing process through the remote copy operation when reading the logs. Then, only the log blocks in which the reading process does not conflict with the writing process as a result of the determination are applied to the database. Thereby, the logs are applied in the sub-site independently to recover the database.

Method for installing (or replacing) a unit on the tower of an offshore wind turbine, which unit comprises a rotor including a hub and one or two rotor blades, and a nacelle receiving a gearbox and a generator. The method is characterized by pre-assembling the substantially functional unit ashore or on a platform, placing the functional unit on a watercraft in such a manner that the center of gravitation of the unit lies in the region of the longitudinal axis of the watercraft and the rotor blades extend in the longitudinal direction of the watercraft, transporting the functional unit to the site of the offshore wind turbine, lifting the functional unit from the watercraft using a crane aboard the watercraft, placing the functional unit on the tower of the offshore wind turbine, and fastening the functional unit on the tower of the offshore wind turbine.

When a crank angle CAa of a specific cylinder, which was expected to stop in a fuel injection stop range over an intake stroke to a compression stroke at a full stop of an engine and received fuel injection, actually exceeds the fuel injection stop range and reaches a preset reference angle CA4, engine stop-state ignition control of the invention ignites the air-fuel mixture in the specific cylinder receiving the fuel injection at a moment of reaching the preset reference angle CA4 (step S260) and simultaneously injects the fuel into a certain cylinder that is in the intake stroke at the moment of the ignition (step S270). When the crank angle CAa of the specific cylinder receiving the fuel injection does not reach the preset reference angle CA4 but exceeds a preset reference angle CA3 that is smaller than the preset reference angle CA4, the engine stop-state ignition control of the invention ignites the air-fuel mixture in the specific cylinder upon a preset wait time elapsed after the full stop of the engine (step S295). This arrangement of the invention effectively restrains direct discharge of the uncombusted fuel at a restart of the engine to prevent the poor emission, while ensuring quiet combustion to reduce the potential vibrations due to the explosive combustion.