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204results about How to "Error prone" patented technology

Method of batching and analyzing of data from computerized process and control systems

The present invention is a solution for problems associated with batching, analyzing and viewing data from computerized and process control systems used in the manufacture of pharmaceutical products. Utilizing the hardware and software networking standards already implemented by a corporate IS/IT group as a platform, the present invention automatically captures (via 3rd party software), processes, archives, reports on and distributes data for any computerized equipment at a facility. Data formats for all equipment regardless of manufacturer, plant location, or hardware/software platform used, are standardized. A single data repository is provide so that any authorized user connected to the company/facility network will have the ability to query this secure data and can generate any number of different reports. Once data is collected, it is batched or grouped according to user defined rules. A batch is given a distinct number, which will then be used to identify the data. Within seconds of batching, data is automatically analyzed using process macro code. This code can be simple or complex as needed to provide only the most important details about a batch. Such analyzation eliminates the manual processing of data, which is usually complex, time-consuming and prone to error. Via the Intranet or Internet, authorized users can view or trend data and access reports including adding electronic signatures. Additional process information such as standard operating procedures, and cycle descriptions may be uploaded and attached to a batch. Any action a user performs that creates, modifies or deletes data in the data repository will be audited.
Owner:TINSETH LANCE DAVID

Dynamic checking method of intelligent substation IED (intelligent electronic device) model configuration correctness based on SCD (security coding device) files

The invention discloses a dynamic checking method of intelligent substation IED (intelligent electronic device) model configuration correctness based on SCD (security coding device) files. The dynamic checking method is adaptable to a digital substation or an intelligent substation communicated under IEC61850. The dynamic checking method includes firstly extracting relative IED model information to be detected from the SCD files, then mapping the relative IED model information to be detected into MMS (multimedia messaging service) named variables, and storing the MMS named variables as a data file 1; then communicating with the IED to be detected in a client terminal mode, reading information of each layer of the IED to be detected online through ACSI (abstract communication service interface) model reading service, and storing the information as a data file 2; and finally comparing the model information of the data file 1 to that of the data file 2 to determine whether the model information is identical or not. The dynamic checking method has the advantages that downloaded CID (character identifier) files in the intelligent substation IED and the SCD file information are checked automatically to determine whether the information is identical or not.
Owner:STATE GRID CORP OF CHINA +2

Fuselage variant type vertical take off and landing aircraft

The invention relates to a new concept aircraft, which is capable of vertically taking off and landing, and flying with a high speed. The profile of a fuselage is similar with the profile of a common fixed wing airplane, the rear part of the fuselage is composed of 2-4 turnable bearing structures, the turnable bearing structures and a longitudinal shaft of front fuselages (which comprises left and right fuselages with a double fuselage layout) are combined as one body on a coaxial line when in a level flight state, the aircraft is transferred to a vertical state while landing, the bearing structure of the rear part of the fuselage enables vertical turnover along a direction perpendicular to the longitudinal shaft, then the airplane is taken off in a tailstock mode, meanwhile the supporting structures of the main wing outer ends at two sides of the airplane can contact to a group/warship surface, a rear fuselage bearing structure tail and the landing plane/warship surface form a large contact/support plane basically perpendicular to the longitudinal shaft of the fuselage, thereby a plurality of supporting structures can support the vertical front fuselage on each direction on a horizontal plane during the tailstock of the aircraft; and the process is opposite during the taking off of the aircraft. In a figure, the dotted line expresses the rear fuselage while stopping.
Owner:江闻杰
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