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System and method for evaluating high-temperature deposition degradation characteristics of aviation lubricating oil

A technology of aviation lubricating oil and lubricating system, applied in the field of mechanical lubrication

Pending Publication Date: 2022-04-12
孚迪斯石油化工科技(葫芦岛)股份有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the only test method for evaluating the coking performance of aviation lubricating oil is the SH / T 0300 crankcase simulation test method (inclined plate coking). And there is a certain gap with the actual working conditions

Method used

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  • System and method for evaluating high-temperature deposition degradation characteristics of aviation lubricating oil

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Embodiment Construction

[0034] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in further detail below in conjunction with the embodiments and accompanying drawings. Here, the exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not to limit the present invention.

[0035] see figure 1 , an evaluation system for high-temperature deposition and degradation characteristics of air lubricating oil provided by an embodiment of the present invention, comprising: electric spindle 1, bearing tooling 2, test lubrication system 3, accompanying test lubrication system 4, mold temperature controller 5, chiller 6, air Press machine 7 and electric control cabinet 8; Wherein,

[0036] Specifically, such as figure 2As shown, the bearing tooling 2 includes a casing 9, and a test spindle 10 is arranged inside the casing 9, and one end of the test spindle 10 is connected ...

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Abstract

The embodiment of the invention provides a system and a method for evaluating high-temperature deposition and degradation characteristics of aviation lubricating oil. The system comprises an electric spindle, a bearing tool, a test lubricating system, an accompanying test lubricating system, a mold temperature controller, a cooling-water machine, an air compressor and an electric control cabinet, by applying the scheme provided by the embodiment of the invention, the aviation turbine engine lubricating oil is placed in the bearing tool, the test main shaft is driven by the electric main shaft to rotate to simulate high-speed operation of the aviation turbine, the pressure borne by the aviation turbine during operation is simulated through the radial loading device, and the temperature of the aviation turbine during operation is simulated through the heating ring; air pressure in the test cavity is adjusted while sealing airflow is provided through the air compressor, so that an air pressure environment for simulating operation of an aviation turbine is simulated, then comprehensive simulation of actual working conditions is achieved, high-temperature deposition and degradation characteristics of test lubricating oil can be evaluated after the test runs for a certain time, and research and development of oil products are guided.

Description

technical field [0001] The invention relates to the technical field of mechanical lubrication, in particular to a system and method for evaluating high-temperature deposition and degradation characteristics of aviation lubricating oil. Background technique [0002] With the development of aero-engines towards high temperature, high speed, and high thrust-to-weight ratio, the engine's requirements for lubricating oils continue to increase, and aero-engine lubricating oils are urgently required to have better oxidation stability and high temperature resistance. The effective, repeatable and practical evaluation method of high-temperature oxidation and coking performance of aviation lubricating oil has guiding significance for the research and development, oil selection and performance evaluation of aero-engine lubricating oil. [0003] At present, the only test method for evaluating the coking performance of aviation lubricating oil is the SH / T 0300 crankcase simulation test m...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N15/04G01N25/00G01N33/30
CPCY02T90/00
Inventor 杨忠存刘洪亮王思颖刘佳陈磊和玉龙
Owner 孚迪斯石油化工科技(葫芦岛)股份有限公司
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