A family of airfoils suitable for 5-10 MW wind turbine blades
A wind turbine blade and airfoil technology, which is applied in the field of blade airfoil design, can solve the problems of inapplicability to multi-megawatt large wind turbine blades, low design Reynolds number, etc., and achieves low roughness sensitivity and high lift-to-drag ratio. Effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
experiment example 1
[0097]The inventor calculated the aerodynamic performance of the NPU-MWA airfoil family of the present invention using the Reynolds-averaged Navier-Stokes method (RANS), respectively adopted the free transition calculation and the full turbulence calculation, and the calculation results are shown in Table 10. The design of the airfoil The lift coefficients are all over 1.2. The section moments of inertia in Table 10 are calculated under the assumption that the airfoil chord length is 1m.
[0098] Table 10 Main aerodynamic characteristics of NPU-MWA multi-megawatt wind turbine airfoil family
[0099]
experiment example 2
[0101] This experimental example is used to compare the difference in aerodynamic performance between the NPU-MWA-180 airfoil and the similar comparison airfoil.
[0102] Specifically, the NPU-MWA-180 airfoil disclosed by the present invention is used as the design airfoil, and the NPU-WA airfoil and DU airfoil with the same relative thickness are used as the comparison airfoil, namely: DU96-W-180 airfoil and NPU -WA-180 airfoil is a comparative airfoil. Among them, the DU96-W-180 airfoil is an airfoil with a relative thickness of 0.18 designed by Delft University in the Netherlands; the reference "Design of Airfoils for Wind Turbine Blades", the link is https: / / gcep.stanford.edu / pdfs / energy_workshops_04_04 / wind_van_rooij.pdf ; The NPU-WA-180 airfoil is an airfoil with a relative thickness of 0.18 disclosed by the patent application number CN201110023215.1.
[0103] The inventor used airfoil aerodynamic analysis software to compare and calculate the aerodynamic performanc...
experiment example 3
[0105] This experimental example is used to compare the difference in aerodynamic performance between the NPU-MWA-210 airfoil and the similar comparison airfoil.
[0106] Specifically, the NPU-MWA-210 airfoil disclosed by the present invention is used as the design airfoil, and the NPU-WA airfoil and DU airfoil with the same relative thickness are used as the comparison airfoil, namely: DU93-W-210 airfoil and NPU -WA-210 airfoil is a comparative airfoil. Among them, the DU93-W-210 airfoil is an airfoil with a relative thickness of 0.21 designed by Delft University in the Netherlands; the reference is Denmark "Wind Turbine Airfoil Catalogue" published by the National Laboratory in 2001, the link is http: / / orbit.dtu.dk / files / 7728949 / ris_r_1280.pdf ; The NPU-WA-210 airfoil is an airfoil with a relative thickness of 0.21 disclosed in the invention patent with the patent application number CN201110023215.1.
[0107] The inventor used airfoil aerodynamic analysis software to ...
PUM
Property | Measurement | Unit |
---|---|---|
Reynolds number | aaaaa | aaaaa |
lift coefficient | aaaaa | aaaaa |
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