Static index testing platform and method for industrial robot joint decelerator
A joint reducer, industrial robot technology, applied in the direction of machine gear/transmission mechanism testing, etc., can solve the problems of large fluctuations in test results, manual loading, poor loading accuracy, etc., to improve test efficiency, reduce test errors, The effect of improving test accuracy
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2016-03-30
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention belongs to the technical field of industrial robots, and in particular relates to a static index test platform and a test method for joint reducers of industrial robots. Background technique
[0002] As an important carrier of automation, industrial robots have become an important symbol to measure a country's manufacturing level and technological level. The joint reducer is the core component of an industrial robot, and its cost accounts for about 30% of the cost of the entire industrial robot. Joint reducers for industrial robots require high rigidity, high motion precision, high transmission efficiency, small hysteresis, and stable load. Among them, the static performance indicators of the reducer include bending moment rigidity, torsional rigidity, backlash and backlash. These static indicators play a decisive role in the position accuracy, operation stability, working capacity and life of the industrial robot's mechanical arm. [0...
Examples
Embodiment Construction
[0027] The present invention will be described in detail below in conjunction with the accompanying drawings.
[0028] Such as figure 1 As shown, an industrial robot joint reducer static index test platform of the present invention includes a first tension pressure sensor 3, a first coupling shaft 4, a moment arm 5, a second coupling shaft 6, a second tension pressure sensor 7, and a second tension pressure sensor 7. Automatic loading device 8, reducer pallet 17 and fuselage base 1, the structure of the second automatic loading device 8 and the first automatic loading device 2 is identical; Fuselage base 1 is provided with reducer pallet 17 and the first automatic loading device 2, And the first automatic loading device 2 is fixed on the fuselage base 1 .
[0029] see figure 2, the first automatic loading device 2 includes a thin cylinder 29 and a screw jack 22, the output screw 21 of the screw jack 22 is used as the execution output end of the automatic loading device, the...