基于Archard理論的航空發(fā)動機零件磨損研究

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金忠凱1，張銀濤2，王成1，彭莘宇3，王坤1，吳蔚1（ ）

中圖分類號：V232.2 文獻(xiàn)標(biāo)志碼：A doi：10.3969/j.issn.1006-0316.2025.06.002

文章編號：1006-0316（2025）06-0008-07

Research on Wear of Aeroengine Parts Based on Archard Theory

IIN Zhongkai1， ZHANG Yintao2，WANG Cheng1， PENG Shenyu3，WANG Kun1，WU Wei1 （ Chengdu Holy Industry & Commerce （Group） Co.， Ltd.， Chengdu 611937， China; 2.Wuhan Vocational College of Software and Engineering，Wuhan 430205， China; 3. AVIC Chengdu Aircraft Industrial （Group） Co.， Ltd.， Chengdu 610092， China ）

Abstract ：Aiming at solving the problem of large amounts of wear on the rolerand roller shaft parts of the main fuel pump acelerator controller of the aeroengine during use，a relative wear model is established based on Archard wear theory.The MATLAB simulation results are consistent with the experimental results，verifying the accuracy of the wear model.The orthogonal analysis method is used to study the influence of diffrent factors such as diferent initial gaps，relative rotationspeeds and forces on the wear amount of the model，and the lawof wear amount and time changes is analyzed.The research results show that there is a certain amount of wear on the rolers and rolershafts during work.The amount of wear has little todo with the working time，but is mainly related to excessive relative speed， excessive load and excessive initial clearance. Among the wear factors， relative rotational speed has the greatest impact，and initial clearance has the smalest impact.However，when the initial clearance exceeds 0.15mm ，the amount of wear under heavy load and high-speed conditions will increase sharply， so the standard initial clearance should be controlled within 0.15mm

Key words ∵ aeroengine ;wear of parts ; Archard theory ; orthogonal analysis method ; wear pattern

渦扇航空發(fā)動機主燃油泵調(diào)節(jié)器中的加速控制器用于控制發(fā)動機供油量，能根據(jù)發(fā)動機的工作狀態(tài)和飛行條件，自動調(diào)節(jié)燃油泵的輸出壓力和流量，以保證發(fā)動機的穩(wěn)定和高效運行[1]。（剩余6700字）