An Analysis Method for the Effect of Rotor-side Control Parameters on Torsional Vibration of Doubly-fed Fan Shafting
A technology for controlling parameters and doubly-fed fans, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as heavy workload and complex models, and achieve the goal of simplifying secondary links, realizing search, and reducing risks Effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0030] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application.
[0031] The present invention provides an analysis method for the influence of rotor-side control parameters on the torsional vibration of the DFIG shaft system, which includes quickly obtaining the torsional vibration critical point of the DFIG shaft system based on the simplified model of the DFIG, and then performing torsional vibration analysis on it. analysis of vibration effects; Figure 4 The power system structure diagram based on the simplified model of doubly-fed wind turbines is shown. The doubly-fed wind farms are respectively connected to two infinite power systems through transmission lines. A series compensation capacitor is set on one transmission line, and the series compensation capacitor can be adjusted at a specific moment. Bypass, and a three-phase ground...
PUM

Abstract
Description
Claims
Application Information

- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com