Vertical torsion two-degree-of-freedom segment model wind tunnel test system
A technology of wind tunnel test and degree of freedom, which is applied in aerodynamic test, machine/structural component test, measuring device, etc. It can solve the non-linear enhancement, shedding and weakening of the aeroelastic effect of long-span bridges to realize different test environments etc. to reduce the sources of complex nonlinear damping and improve reliability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment
[0036] Such as figure 1 and figure 2 As shown, the present invention discloses a segmental model wind tunnel test system with two degrees of freedom in vertical torsion, including two sets of suspension support devices with the same structure, and the two sets of suspension support devices are respectively connected to the two ends of the segmental test model 13 , and arranged symmetrically with each other, each group of suspension support devices respectively includes a rigid support 1, a wind attack angle adjustment plate 2, a support frame 3, a vertical flutter measurement component and a torsional flutter measurement component, the rigid support 1 stands on the ground, and the wind attack The angle adjustment plate 2 is installed on the rigid support 1, the support frame 3 is installed on the wind attack angle adjustment plate 2 through the vertical flutter measurement assembly, and can move in the vertical direction, and the torsional flutter measurement assembly is inst...
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