Wind tunnel balance and method of use
US-2018335364-A1 · Nov 22, 2018 · US
US11754464B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11754464-B2 |
| Application number | US-202017624353-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 31, 2020 |
| Priority date | Feb 6, 2020 |
| Publication date | Sep 12, 2023 |
| Grant date | Sep 12, 2023 |
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A wind tunnel test equipment using wind force integration includes: a structural model whose interior is empty; an internal support disposed inside the structural model; and load sensors disposed outside the internal support and coming into close contact with the inner surfaces of the structural model to measure aerodynamic forces applied to the structural model.
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The invention claimed is: 1. Wind tunnel test equipment using wind force integration, comprising: a structural model ( 2 ) whose interior is empty; an internal support ( 3 ) disposed inside the structural model ( 2 ); and load sensors ( 4 ) disposed outside the internal support ( 3 ) and coming into close contact with the inner surfaces of the structural model ( 2 ) to directly measure aerodynamic forces applied to the structural model ( 2 ) as reaction forces. 2. The wind tunnel test equipment according to claim 1 , wherein the structural model ( 2 ) has a plurality of segments ( 21 ) formed dividedly on the external walls thereof. 3. The wind tunnel test equipment according to claim 2 , wherein the neighboring segments ( 21 ) have a sealing material ( 22 ) disposed therebetween. 4. The wind tunnel test equipment according to claim 1 , wherein the internal support ( 3 ) is a rigid core. 5. The wind tunnel test equipment according to claim 1 , wherein the internal support ( 3 ) is an equivalent dynamic model of a structural system of a structure.
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