Double-lug double-shaft tension-torsion fatigue test loading device

By designing a biaxial tensile-torsional fatigue test loading device with double lugs, the problem of fatigue characteristic evaluation of double lug structures under biaxial loads was solved, reliable design data was provided, and high-precision fatigue performance evaluation and failure mode analysis were achieved.

CN224163508UActive Publication Date: 2026-04-24CHINA HELICOPTER RES & DEV INST
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Patent Information

Application Number
CN202520622907.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-04-03
Publication Date
2026-04-24
Estimated Expiration
2035-04-03

AI Technical Summary

Technical Problem

Existing technologies are insufficient to effectively assess the fatigue characteristics and failure modes of double-eared structures under the coupled effects of axial tensile and compressive loads and rotational loads around the bolt hole axis, resulting in a lack of reliable data support for fatigue strength design.

Method used

A dual-ear biaxial tensile-torsional fatigue test loading device was designed. Axial tensile and compressive loads are applied by an actuator, and rotational loads around the bolt hole axis are achieved by a lateral loading adapter plate and a spherical bearing. Combined with displacement and angle sensors for monitoring, the fatigue performance of the dual-ear plates under biaxial loads is simulated.

Benefits of technology

It enables accurate evaluation of the fatigue performance and failure mode of the double-ear structure under biaxial tensile and torsional loads, provides reliable design data support, and the device has a simple structure, low cost, high stability of loading waveform, and an error of less than 3%.

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Abstract

The utility model belongs to the technical field of helicopter fatigue tests, and particularly relates to a double-lug double-shaft tension-torsion fatigue test loading device. Comprising an actuator, a switching assembly, a fixed loading frame, a torsion frame and a vertical loading fork lug, a groove is formed in the middle of the torsion frame, two ends of the torsion frame are respectively provided with a lug, and the lug plane is perpendicular to the groove plane; a single plate below the double-lug piece is inserted into a groove of the torsion frame, and double lugs above the double-lug piece are hinged with a vertical loading fork lug through a joint bearing; a rolling bearing for torsion is embedded in each of two lugs above the torsion frame, and a torsion pin shaft penetrates through the rolling bearings for torsion to be connected with the fixed loading frame; the actuator is connected with the torsion frame through the switching assembly.
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