一种自感知拉索锚具
By using a flanged piezoelectric ceramic sensor to monitor the time difference of flight of ultrasonic waves in cable anchors, the problem of traditional cable anchors being unable to monitor axial force in real time has been solved, enabling real-time safety assessment and early warning of cable structures, and improving the safety and durability of the structures.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- HEFEI VSL ENG CORP ON LIM
- Filing Date
- 2025-07-22
- Publication Date
- 2026-07-17
AI Technical Summary
Traditional cable anchors lack real-time axial force monitoring capabilities, resulting in long detection cycles, low efficiency, and an inability to promptly detect early failure warnings, posing structural safety risks.
By employing a flanged piezoelectric ceramic sensor based on the principle of acoustoelasticity, the sensor transmits and receives ultrasonic waves, records the time difference of flight, and calculates the axial force using calibration coefficients, thereby achieving real-time axial force monitoring and providing timely data support.
It enables real-time status assessment of cable-stayed structures, timely detection of axial force anomalies, prevention of safety accidents, and improvement of structural safety and durability.
Smart Images

Figure CN224514050U_ABST
Abstract
Claims
1. A self-aware guyed anchor comprising an anchor body (1) and a cap (2) located on top of the anchor body (1), characterized in that: The top of the anchor body (1) is provided with a decorative plate (3), the interior of the decorative plate (3) is filled with damping sealant (4), a cap sealing gasket (5) is provided between the top of the decorative plate (3) and the cap (2), a plurality of flanged piezoelectric ceramic sensors (6) are provided in the gap between the anchor body (1) and the decorative plate (3), a connecting wire (7) is fixedly installed on the surface of the plurality of flanged piezoelectric ceramic sensors (6), a connecting wire (8) is fixedly installed at the end of the connecting wire (7) away from the flanged piezoelectric ceramic sensor (6), the connecting wire (8) is located on the outer periphery of the anchor body (1), and a junction box (9) is provided on the outer periphery of the connecting wire (8), the junction box (9) is located on the outer periphery of the anchor body (1).
2. The self-aware guyed cable anchor of claim 1, wherein: There are three flanged piezoelectric ceramic sensors (6), which are arranged in a circle with the center of the decorative plate (3) as the reference.
3. The self-aware guyed cable anchor of claim 1, wherein: The connecting line (7) consists of two parts: a signal line (71) and a return line (72). Both the signal line (71) and the return line (72) are connected to the aircraft plug (8).
4. The self-aware guyed cable anchor of claim 1, wherein: The junction box (9) is fixedly installed with a protective cap (10) and a junction box plug (11) on its side and top, respectively, and the junction box (9) is installed on the outer periphery of the anchor body (1) by fixing screws.
5. The self-aware guyed cable anchor of claim 1, wherein: A fixing bolt (12) is threaded at the edge of the top of the cap (2), and a cap plug (13) is detachably installed at the middle of the top of the fixing bolt (12).
6. The self-aware guyed cable anchor of claim 1, wherein: The anchor body (1) is fixedly installed with a positioning pin (14) on the top. The decorative plate (3) is provided with a positioning hole at the position corresponding to the positioning pin (14). The decorative plate (3) is threaded with a decorative plate fixing screw (15).