CN106289893A - 一种轮盘盘心孔疲劳试验件的制造方法 - Google Patents
一种轮盘盘心孔疲劳试验件的制造方法 Download PDFInfo
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN109489957A (zh) * | 2018-12-10 | 2019-03-19 | 中国航发四川燃气涡轮研究院 | 一种用于轮盘试验的带应力分割槽的转接结构 |
CN111238804A (zh) * | 2018-11-28 | 2020-06-05 | 中国航发商用航空发动机有限责任公司 | 航空发动机转子的超转破裂试验的试验件构型方法 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111238804A (zh) * | 2018-11-28 | 2020-06-05 | 中国航发商用航空发动机有限责任公司 | 航空发动机转子的超转破裂试验的试验件构型方法 |
CN109489957A (zh) * | 2018-12-10 | 2019-03-19 | 中国航发四川燃气涡轮研究院 | 一种用于轮盘试验的带应力分割槽的转接结构 |
CN109489957B (zh) * | 2018-12-10 | 2020-12-15 | 中国航发四川燃气涡轮研究院 | 一种用于轮盘试验的带应力分割槽的转接结构 |
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Address after: Fengcheng Weiyang District ten road 710021 Shaanxi city of Xi'an Province Patentee after: AECC AVIATION POWER CO,LTD. Address before: Fengcheng Weiyang District ten road 710021 Shaanxi city of Xi'an Province Patentee before: AVIC AVIATION ENGINE Corp.,PLC Address after: Fengcheng Weiyang District ten road 710021 Shaanxi city of Xi'an Province Patentee after: AVIC AVIATION ENGINE Corp.,PLC Address before: Fengcheng Weiyang District ten road 710021 Shaanxi city of Xi'an Province Patentee before: XI'AN AVIATION POWER Co.,Ltd. |
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