Aviation hydraulic oil viscosity attenuation control index test system and test method

A technology of attenuation control and index testing, which can be used in measuring devices, temperature control by electric means, auxiliary controllers with auxiliary heating devices, etc., which can solve the problems of system friction, increased wear, and poor lubrication effect.

Pending Publication Date: 2018-06-22
陕西东方长安航空科技有限公司
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  • Application Information

AI Technical Summary

Problems solved by technology

As the viscosity of the hydraulic oil decreases, the lubricating oil film produced by the hydraulic oil on the working surfaces of the aircraft hydraulic system will gradually become thinner, and the lubricating effect will gradually deteriorate, resulting in increased friction and wear inside the system, resulting in more wear particles.

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  • Aviation hydraulic oil viscosity attenuation control index test system and test method
  • Aviation hydraulic oil viscosity attenuation control index test system and test method
  • Aviation hydraulic oil viscosity attenuation control index test system and test method

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Embodiment Construction

[0062] Such as figure 1 with figure 2 As shown, the aviation hydraulic oil viscosity attenuation control index test device of the present invention includes a monitoring device, a test bench for the tested hydraulic pump 1 to be installed, and a metal element content in the hydraulic oil used to detect the hydraulic pump 1's casing return oil. The oil spectrum analyzer, the test bench includes an oil tank 14 that supplies oil to the hydraulic pump 1 under test, a heating and cooling module that controls the oil return temperature of the hydraulic pump 1 under test, and an oil return module for the hydraulic pump 1 under test. Filter and the filter 13 that is connected with the oil tank 14 and the oil liquid online viscosity sensor 11 that detects the return oil viscosity of the tested hydraulic pump 1, the heating and cooling module includes a water-cooled radiator 17 and is connected with the outlet of the water-cooled radiator 17 The heating package 18, the outlet of the h...

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Abstract

The invention discloses an aviation hydraulic oil viscosity attenuation control index test system and a test method. The test system comprises a monitoring device and a test platform for the mountingof a tested hydraulic pump, and the test platform comprises an oil tank used for supplying oil to the tested hydraulic pump, a heating and cooling module used for controlling the temperature of the return oil of the tested hydraulic pump, a filter used for filtering the return oil of the tested hydraulic pump and connected to the oil tank, and an on-line oil viscosity sensor used for detecting theviscosity of the return oil of the tested hydraulic pump. The test method comprises the following steps: (1) before testing, the tested hydraulic pump is mounted, and whether the tested hydraulic pump is normal or not is judged; (2) a viscosity reference value and a metallic element content reference value are detected; (3) a viscosity attenuation control index is detected. The aviation hydraulicoil viscosity attenuation control index test system has the advantages of simple structure, reasonable design, easiness in use and operation and good use effect, and can easily and quickly carry outthe testing of an aviation hydraulic oil viscosity attenuation control index, and moreover, the testing precision is higher.

Description

technical field [0001] The invention belongs to the technical field of testing the viscosity attenuation control index of aviation hydraulic oil, and in particular relates to a testing device and a testing method for the viscosity attenuation control index of aviation hydraulic oil. Background technique [0002] The aircraft hydraulic system uses aviation hydraulic oil as its working medium. In addition to transmitting hydraulic energy in the aircraft hydraulic system as a working medium, aviation hydraulic oil also lubricates the working surfaces in the aircraft hydraulic system to protect the working surface from oxidation. . With the operation of the aircraft hydraulic system, the relative movement of the internal working surfaces will produce metal particles; various seals will gradually produce non-metallic particles as they age or work, and these particles enter the hydraulic oil and flow downstream with the hydraulic oil , and filtered by oil filter. Therefore, hydr...

Claims

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Application Information

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IPC IPC(8): G01N11/00G01N33/28G01N33/30G05D23/30
CPCG05D23/30G01N11/00G01N33/28G01N33/2805G01N33/2888G01N33/30Y02T50/40
Inventor 李昆侯惠中赵苗李艳波
Owner 陕西东方长安航空科技有限公司
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