Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

37results about How to "Simplify the troubleshooting process" patented technology

Method and device for diagnosing automotive electronic control unit faults based on semi-physical simulation

The invention relates to a method and a device for diagnosing automotive electronic control unit faults based on semi-physical simulation. The method comprises the steps that (1) a personal computer (PC) and a control system send standard input information to an electronic control unit to be detected and send standard output response information to a fault diagnosis and display module; (2) the electronic control unit to be detected processes and sends out the output response information; (3) the fault diagnosis and display module compares the standard output response information with output response information of electronic control unit (ECU) to be detected to draw a conclusion whether the electronic control unit to be detected breaks down; and (4) changing some input information, and diagnosing fault properties of the electronic control unit to be detected. The device comprises the PC, the control system and a simulation controller. Compared with the prior art, by means of the method and the device for diagnosing the automotive electronic control unit faults based on the semi-physical simulation, the fault clearing flow of an automotive electronic control is greatly simplified, the fault clearing range is narrowed, the fault diagnosis rate is further improved, maintenance workload result from diagnosis of replacement parts and fund employment amount of stock parts are effectively reduced, thus the maintenance cost is greatly reduced.
Owner:SHANGHAI UNIV OF ENG SCI +1

Diagnostic determination method for spacecraft control system under influence of noise

The invention provides a diagnostic determination method for a spacecraft control system under influence of noise. First, a multivariate probability distribution statistic model of the spacecraft control system is built through a standard model and an equivalent space method; then a detectability index is obtained; and fault detectability is determined; finally, an isolability index is obtained, and the fault isolability is determined. According to the diagnostic determination method, influence of process noise, observation noise and other interference factors on diagnostic performance are fully taken into consideration, fault diagnosis algorithms are not required to be designed, and the fault detectability and the isolability can be determined according to system information including kinetics, kinematics, a controller model and the like of the spacecraft control system and the configuration and installation condition of a sensor and an actuator, the fault diagnosis process of the spacecraft control system is simplified, meanwhile, a theoretical basis can be provided for design of a diagnosis algorithm, the design method of the spacecraft control system is optimized, and the controllability of the spacecraft control system is improved.
Owner:BEIJING INST OF CONTROL ENG

Method for performing cross-platform unified management on users of cluster storage system

The invention specially relates to a method for performing cross-platform unified management on users of a cluster storage system. The method for performing the cross-platform unified management on the users of the cluster storage system includes: uniformly storing all the cluster storage users on an external AD (active directory) domain controller, and simultaneously using SAMBA software to add cluster storage nodes in a Windows AD domain, wherein a storage node SAMBA server is used as a member of the Windows AD domain, and an AD domain controller node provides SAMBA user unified management services to the cluster storage system. According to the method for performing the cross-platform unified management on the users of the cluster storage system, all user management operations are completed through the AD domain controller, unified authentication of the cross-platform users, Windows users and Linux users is achieved, and simultaneously user information is stored on an AD domain service node except the nodes of the cluster storage system, influences of breakdowns of the cluster storage nodes on user access are further avoided, and furthermore not only is the unified management of the cross-platform users achieved, but also an elimination process of system breakdowns is greatly simplified.
Owner:INSPUR GROUP CO LTD

Superconductive magnetic suspension supporting arrangement

The invention provides a superconductive magnetic suspension supporting arrangement, and six support modules (10) are symmetrically distributed on a reference axis of orthogonal coordinate system whose original point is the center of a rotor chamber (8). A heating power supply (18) is powered on, and a superconductive switch (16) is disconnected, and a superconductive power supply (19) is used for excitation of a superconducting coil (11). A magnetic field generated by the superconducting coil (11) enters from a middle aperture of the superconducting coil (11) to a middle aperture of the superconductive shaping block (12), and then returns from a gap from the superconductive shaping block (12) and the superconducting ring (13) as well as the lower part of the superconducting coil (11) to the middle aperture of the superconducting coil (11) for forming a closed magnetic circuit. The superconductive rotor (9) is suspended by a magnetic repulsion generated by the superconducting coil (11). After excitation of the superconducting coil (11), the heating power supply (18) is closed and the superconductive switch (16) is connected, and then the superconductive power supply (19) is disconnected, and the current of the superconducting coil (11) can provide a stable suspension magnetic field for the superconductive rotor (9).
Owner:INST OF ELECTRICAL ENG CHINESE ACAD OF SCI

High-altitude flame-projecting barrier-removing robot

The invention discloses a high-altitude flame-projecting barrier-removing robot, including a multi-shaft aircraft two-stage telescoping mechanism and a flame projecting system. The flame projecting system includes a pressurization fuel oil storage tank, a nozzle and a high-pressure igniter, after being atomized through the nozzle, pressurized fuel oil in the pressurization fuel oil storage tank can be ignited by the high-pressure igniter, the two-stage telescoping mechanism includes a first-stage sliding block, a first-stage guide rail, a second-stage sliding block, a second-stage guide rail, an extension rod and a driving device, the first-stage sliding block is slidably arranged on the first-stage guide rail and is fixedly arranged on a main rack of the flame projecting system, and the second-stage sliding block is slidably arranged on the second-stage guide rail; while driving the second-stage sliding block to slide relative to the second-stage guide rail, the driving device drives the first-stage guide rail to slide relative to the first-stage sliding block in the same direction synchronously; and the extension rod is fixedly connected to the second-stage sliding block, and the nozzle and the high-pressure igniter are mounted on the extension rod. The high-altitude flame-projecting barrier-removing robot provided by the invention adopts a remote control flight flame-projecting scheme, and a power supply does not need to be cut off in the barrier removing process, thereby simplifying a barrier removing operation process, lightening the burden of operating personnel, improving the barrier removing efficiency, and ensuring the safety of workers.
Owner:昆山市工业技术研究院有限责任公司

Method for investigating indoor and outdoor communication fault points of VRV (Vacuum Reducer Valve) multi-connected air-condition unit

The invention discloses a method for investigating indoor and outdoor communication fault points of a VRV (Vacuum Reducer Valve) multi-connected air-condition unit. The method comprises the following steps: when indoor and outdoor communication fault occurs, firstly checking and determining whether the communication between an outdoor machine and a first indoor machine is normal; if so, determining whether the fault is caused by address conflict of the first category of indoor machines; if so, carrying out fault clearance, if not, determining that the fault is caused by the problem of the second category of hardware, and going to the next investigating step at the time; investigating the fault caused by the problem of the second category of hardware: judging the communication connection problem of one indoor machine or several indoor machines by using a dichotomy; checking according to several fault causes after the communication problem of the indoor machine is investigated by using the dichotomy; and then removing the fault to ensure that the communication between the outdoor machine and the indoor machine gets right. The invention has the advantages of simplicity and convenience, reliability, quick investigating speed and high working efficiency.
Owner:NINGBO AUX ELECTRIC

A method for determining the diagnosability of spacecraft control systems under the influence of noise

The invention provides a diagnostic determination method for a spacecraft control system under influence of noise. First, a multivariate probability distribution statistic model of the spacecraft control system is built through a standard model and an equivalent space method; then a detectability index is obtained; and fault detectability is determined; finally, an isolability index is obtained, and the fault isolability is determined. According to the diagnostic determination method, influence of process noise, observation noise and other interference factors on diagnostic performance are fully taken into consideration, fault diagnosis algorithms are not required to be designed, and the fault detectability and the isolability can be determined according to system information including kinetics, kinematics, a controller model and the like of the spacecraft control system and the configuration and installation condition of a sensor and an actuator, the fault diagnosis process of the spacecraft control system is simplified, meanwhile, a theoretical basis can be provided for design of a diagnosis algorithm, the design method of the spacecraft control system is optimized, and the controllability of the spacecraft control system is improved.
Owner:BEIJING INST OF CONTROL ENG

Method and device for diagnosing automotive electronic control unit faults based on semi-physical simulation

The invention relates to a method and a device for diagnosing automotive electronic control unit faults based on semi-physical simulation. The method comprises the steps that (1) a personal computer (PC) and a control system send standard input information to an electronic control unit to be detected and send standard output response information to a fault diagnosis and display module; (2) the electronic control unit to be detected processes and sends out the output response information; (3) the fault diagnosis and display module compares the standard output response information with output response information of electronic control unit (ECU) to be detected to draw a conclusion whether the electronic control unit to be detected breaks down; and (4) changing some input information, and diagnosing fault properties of the electronic control unit to be detected. The device comprises the PC, the control system and a simulation controller. Compared with the prior art, by means of the method and the device for diagnosing the automotive electronic control unit faults based on the semi-physical simulation, the fault clearing flow of an automotive electronic control is greatly simplified, the fault clearing range is narrowed, the fault diagnosis rate is further improved, maintenance workload result from diagnosis of replacement parts and fund employment amount of stock parts are effectively reduced, thus the maintenance cost is greatly reduced.
Owner:SHANGHAI UNIV OF ENG SCI +1

Superconductive magnetic suspension supporting arrangement

The invention provides a superconductive magnetic suspension supporting arrangement, and six support modules (10) are symmetrically distributed on a reference axis of orthogonal coordinate system whose original point is the center of a rotor chamber (8). A heating power supply (18) is powered on, and a superconductive switch (16) is disconnected, and a superconductive power supply (19) is used for excitation of a superconducting coil (11). A magnetic field generated by the superconducting coil (11) enters from a middle aperture of the superconducting coil (11) to a middle aperture of the superconductive shaping block (12), and then returns from a gap from the superconductive shaping block (12) and the superconducting ring (13) as well as the lower part of the superconducting coil (11) to the middle aperture of the superconducting coil (11) for forming a closed magnetic circuit. The superconductive rotor (9) is suspended by a magnetic repulsion generated by the superconducting coil (11). After excitation of the superconducting coil (11), the heating power supply (18) is closed and the superconductive switch (16) is connected, and then the superconductive power supply (19) is disconnected, and the current of the superconducting coil (11) can provide a stable suspension magnetic field for the superconductive rotor (9).
Owner:INST OF ELECTRICAL ENG CHINESE ACAD OF SCI

High-altitude fire-breathing obstacle removal robot

The invention discloses a high-altitude flame-projecting barrier-removing robot, including a multi-shaft aircraft two-stage telescoping mechanism and a flame projecting system. The flame projecting system includes a pressurization fuel oil storage tank, a nozzle and a high-pressure igniter, after being atomized through the nozzle, pressurized fuel oil in the pressurization fuel oil storage tank can be ignited by the high-pressure igniter, the two-stage telescoping mechanism includes a first-stage sliding block, a first-stage guide rail, a second-stage sliding block, a second-stage guide rail, an extension rod and a driving device, the first-stage sliding block is slidably arranged on the first-stage guide rail and is fixedly arranged on a main rack of the flame projecting system, and the second-stage sliding block is slidably arranged on the second-stage guide rail; while driving the second-stage sliding block to slide relative to the second-stage guide rail, the driving device drives the first-stage guide rail to slide relative to the first-stage sliding block in the same direction synchronously; and the extension rod is fixedly connected to the second-stage sliding block, and the nozzle and the high-pressure igniter are mounted on the extension rod. The high-altitude flame-projecting barrier-removing robot provided by the invention adopts a remote control flight flame-projecting scheme, and a power supply does not need to be cut off in the barrier removing process, thereby simplifying a barrier removing operation process, lightening the burden of operating personnel, improving the barrier removing efficiency, and ensuring the safety of workers.
Owner:昆山市工业技术研究院有限责任公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products