2022
DOI: 10.1016/j.measurement.2022.112050
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Online monitoring of oil film thickness of journal bearing in aviation fuel gear pump

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Cited by 20 publications
(18 citation statements)
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“…When interference factors significantly impact the measurement results, higher-precision measurement results can Temperature Spring model, resonant model (Jia et al, 2021;Jia et al, 2022) Multifaceted temperature compensation for density, sound velocity and reference signal Resonant model (Wei and Wang et al, 2022) Calibration in the temperature range of 24-90°C with 0.2 °C intervals…”
Section: Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…When interference factors significantly impact the measurement results, higher-precision measurement results can Temperature Spring model, resonant model (Jia et al, 2021;Jia et al, 2022) Multifaceted temperature compensation for density, sound velocity and reference signal Resonant model (Wei and Wang et al, 2022) Calibration in the temperature range of 24-90°C with 0.2 °C intervals…”
Section: Discussionmentioning
confidence: 99%
“…Sliding Bearings (Wei et al, 2022) Uses complex modal and resonance modes for online monitoring of the oil film the presence of incident angles. The accuracy and applicable models of oil film thickness measurement results under different influencing factors shown in Table 4.…”
Section: Resonance Modelmentioning
confidence: 99%
“…Due to its simple structure, small size, and low sensitivity to oil contamination, gear pumps are widely used in lubrication systems and fuel systems of aviation aircraft [1] . As the power source of the lubrication system, gear pumps provide lubricant and coolant that effectively reduce part wear and carry away heat generated by gears and bearings during transmission, which can ensure aircraft flight safety.…”
Section: Introductionmentioning
confidence: 99%
“…With the continuous improvement of aircraft performance, more stringent requirements have been placed on overall weight and internal space of aircraft, necessitating the miniaturization and lightweight design of components [2] . There are mainly two ways to achieve miniaturization and lightweight design of aviation gear pumps [3][4] : (1) Increasing speed can reduce pump displacement and achieve miniaturization and lightweight design of gears and other components under rated flow rate; (2) Gear pitch circle diameter, and pump body thickness, overall miniaturization and lightweight design can be realized by reducing shaft diameter. However, as gear pump speed increases and dimensions decrease, problems such as intensified oil entrainment, decreased component strength, and increased wear may occur, which lead to premature damage to the transmission system and engine of aviation aircraft during service [5][6] .…”
Section: Introductionmentioning
confidence: 99%
“…Thereby, the initial mode may even become the primary mode of the final failure [1]. Therefore, predicting the lifespan of aero engine bearings is crucial for effectively implementing 'on-condition maintenance' of an aero engine [2]. As fault diagnosis theory and equipment testing technology improve in quality, the resulting research findings are being applied to several aspects of mechanical engineering practice [3].…”
Section: Introductionmentioning
confidence: 99%