5 results about "Data processing software" patented technology

A method for constructing artificial pillars in large goaf areas using controlled blasting and slotting includes the following steps: S1. Based on three-dimensional laser scanning and ground pressure monitoring data, a three-dimensional digital model is generated using data processing software to identify potential high ground pressure instability risk areas and determine the location, shape, and size parameters of the artificial pillars; S2. Main blasting holes, cutting holes, and auxiliary holes are arranged in the corresponding area of ​​the goaf roof to form a controlled blasting slotting design; S3. A reinforcing cage is installed at the bottom of the goaf, and the pillar mold is installed and assembled; S4. Using a micro-delay detonation method, the cutting holes, auxiliary holes, and main blasting holes are detonated sequentially, causing the roof rock to directionally collapse and fall into the reinforcing cage directly below, filling and compacting to form a composite artificial pillar; then, the outer mold is removed, completing the construction of the artificial pillar. This invention achieves an integrated and coordinated process of blasting pressure relief, crushed stone utilization, and pillar construction, with advantages of simplified procedures, minimal disturbance, and high stability.

The application designs a three-dimensional flow cytometer and method based on optical detection and ICP-MS combination, relates to the technical field of life analysis scientific detection equipment; first, a three-dimensional flow cytometer is provided, a three-dimensional flow cytometer method based on optical detection and ICP-MS combination is designed based on the analyzer, and the flow cytometer can only perform single-parameter flow cytometer analysis of fluorescence, scattering and mass spectrum or multi-parameter flow cytometer analysis in any combination; the data processing software in the analyzer can provide offline processing of flow cytometer analysis data of fluorescence, side scattering light and mass spectrum, identify, calculate and statistically analyze single-cell pulse signals, especially can provide integration and unification among fluorescence, side scattering and mass spectrum single-cell signals, and obtain three-parameter information of the same cell.

The application discloses a kind of high-speed camera detection multi-machine drive system synchronous phase difference measurement method, it is related to vibrating screen synchronous detection technical field, and the device used includes vibrating screen prototype, high-speed camera, camera support, data processing software and positioning sheet etc..First, high-speed camera is installed with the plane parallel of vibrating screen motor rotor, and image sequence in the rotating process of rotor is collected;Second, the pixel coordinates of positioning sheet and rotating center are obtained by image recognition technology, and relative position vector is constructed. Through interpolation noise reduction processing to vector coordinates, project to preset reference vector, generate projection coordinate-time curve, and extract image phase difference. Finally, according to the rotating direction of motor, image phase difference is converted into motor phase difference using unified formula, and accurate measurement under multiple working conditions is realized. The method solves the industry pain point that positive and negative phase difference measurement standards are not unified, and the measurement precision is high, which can be popularized to multiple working condition detection scenes of multi-machine drive rotating equipment.

The present invention provides a method for processing bitstream data by using code-free reconstruction, and a computing device therefor. A code-free protocol template file is used to define content parameters for each field of bitstream data in a communication protocol. A data parsing and processing method is used to parse a bitstream data frame, and perform forward processing on the bitstream data on the basis of field parameter information in the code-free protocol template, so as to obtain data content information suitable for display and application. An information packaging and processing method is used to perform reverse processing on user-inputted field content information on the basis of the field parameter information in the code-free protocol template, so as to generate bitstream data for communication transmission. The present invention uses different protocol template files to accommodate bitstream data of different protocols. During implementation iterations of engineering projects, a new data protocol can be accommodated merely by editing a code-free protocol template file without the need to modify source code, thereby shortening the development cycle of data processing software, reducing quality risks and management costs, and improving development efficiency.

The application belongs to the technical field of aircraft aerodynamic load design, and is an aerodynamic data processing method for a high-camber wing. Target spanwise position-based spanwise coordinate groups are extracted based on the aircraft body coordinate system, target spanwise data of the wing is input into numerical calculation software or data processing software, external environmental parameters are given, pressure coefficient distribution data of the target spanwise position is calculated and exported; through comparison and judgment with the airfoil leading edge point, coordinate point sets at different positions are obtained, and surface pressure coefficients in different coordinate point sets are extracted respectively, the surface pressure coefficients are sequentially interpolated into chordwise positions required for load calculation, and chordwise position data of the high-camber wing is obtained. The wing surface data is successfully processed through rearrangement of the coordinate points and division of the regions to distinguish the upper and lower surface points by different methods. The influence of the wing camber change is considered, and the design requirements in engineering can be met.