CN108610078A - 一种航空发动机的主轴承内环 - Google Patents
一种航空发动机的主轴承内环 Download PDFInfo
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Abstract
本发明公开了一种航空发动机的主轴承内环,所述主轴承内环采用如下陶瓷材料加工而成,该陶瓷材料包括以下重量份的组分:碳化铬粉20‑24份,白云石2‑5份,硼砂4‑10份,碳纤维4‑8份,硅藻土5‑7份,乙酸乙酯6‑8份,锰6‑10份,氧化镧4‑6份,二氧化硅10‑20份,玻璃纤维7‑10份,甲基三乙酰氧基硅烷2‑4份,辛基酚聚氧乙烯醚7‑9份,硅烷偶联剂4‑6份,羟乙基纤维素4‑8份,氧化镁8‑11份,氮化硼6‑8份,氮化铝6‑9份,氧化钛4‑5份,氧化铁10‑15份,二氧化锆9‑13份,聚乙二醇5‑10份。本发明强度和硬度好,耐氧化,韧性好;适应性非常广泛。
Description
技术领域
本发明是属于主轴承内环技术领域,具体说是一种航空发动机的主轴承内环。
背景技术
近年来主轴承内环品类繁多,根据需求进行了一次次的改进,现有的主轴承内环具有强度高,往往是单纯追求强度高,而忽略了耐氧化性能和韧性的提高。
发明内容
为解决现有技术中的问题,本发明专利目的是提供一种航空发动机的主轴承内环。
为达到上述目的,本发明采用的技术方案是:
一种航空发动机的主轴承内环,所述主轴承内环采用如下陶瓷材料加工而成,该陶瓷材料包括以下重量份的组分:
碳化铬粉20-24份,白云石2-5份,硼砂4-10份,碳纤维4-8份,硅藻土5-7份,乙酸乙酯6-8份,锰6-10份,氧化镧4-6份,二氧化硅10-20份,玻璃纤维7-10份,甲基三乙酰氧基硅烷2-4份,辛基酚聚氧乙烯醚7-9份,硅烷偶联剂4-6份,羟乙基纤维素4-8份,氧化镁8-11份,氮化硼6-8份,氮化铝6-9份,氧化钛4-5份,氧化铁10-15份,二氧化锆9-13份,聚乙二醇5-10份。本发明具有以下优点:
1、本发明具有极高的强度和硬度,耐氧化,同时具有一定韧性;适应性非常广泛。
具体实施方式
下面结合具体实施例对发明作进一步说明。
实施例1
一种航空发动机的主轴承内环,所述主轴承内环采用如下陶瓷材料加工而成,该陶瓷材料包括以下重量份的组分:
碳化铬粉20-24份,白云石2-5份,硼砂4-10份,碳纤维4-8份,硅藻土5-7份,乙酸乙酯6-8份,锰6-10份,氧化镧4-6份,二氧化硅10-20份,玻璃纤维7-10份,甲基三乙酰氧基硅烷2-4份,辛基酚聚氧乙烯醚7-9份,硅烷偶联剂4-6份,羟乙基纤维素4-8份,氧化镁8-11份,氮化硼6-8份,氮化铝6-9份,氧化钛4-5份,氧化铁10-15份,二氧化锆9-13份,聚乙二醇5-10份。
Claims (1)
1.一种航空发动机的主轴承内环,其特征在于:
所述主轴承内环采用如下陶瓷材料加工而成,该陶瓷材料包括以下重量份的组分:
碳化铬粉20-24份,白云石2-5份,硼砂4-10份,碳纤维4-8份,硅藻土5-7份,乙酸乙酯6-8份,锰6-10份,氧化镧4-6份,二氧化硅10-20份,玻璃纤维7-10份,甲基三乙酰氧基硅烷2-4份,辛基酚聚氧乙烯醚7-9份,硅烷偶联剂4-6份,羟乙基纤维素4-8份,氧化镁8-11份,氮化硼6-8份,氮化铝6-9份,氧化钛4-5份,氧化铁10-15份,二氧化锆9-13份,聚乙二醇5-10份。
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