CN206270295U - 航空发动机涡轮叶片涡流探伤试块夹具 - Google Patents
航空发动机涡轮叶片涡流探伤试块夹具 Download PDFInfo
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- CN206270295U CN206270295U CN201620289692.0U CN201620289692U CN206270295U CN 206270295 U CN206270295 U CN 206270295U CN 201620289692 U CN201620289692 U CN 201620289692U CN 206270295 U CN206270295 U CN 206270295U
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- 238000012360 testing method Methods 0.000 title claims abstract description 12
- 238000007689 inspection Methods 0.000 title claims abstract description 11
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 18
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- 238000007781 pre-processing Methods 0.000 claims description 6
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- 238000002474 experimental method Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
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CN201620289692.0U CN206270295U (zh) | 2016-04-08 | 2016-04-08 | 航空发动机涡轮叶片涡流探伤试块夹具 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107271541A (zh) * | 2016-04-08 | 2017-10-20 | 贵州黎阳航空动力有限公司 | 一种涡轮叶片涡流探伤对比试块加工夹具及其制作方法 |
CN109341507A (zh) * | 2018-11-20 | 2019-02-15 | 中国航发贵州黎阳航空动力有限公司 | 一种涡流测厚校准对比装置 |
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2016
- 2016-04-08 CN CN201620289692.0U patent/CN206270295U/zh not_active Withdrawn - After Issue
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107271541A (zh) * | 2016-04-08 | 2017-10-20 | 贵州黎阳航空动力有限公司 | 一种涡轮叶片涡流探伤对比试块加工夹具及其制作方法 |
CN107271541B (zh) * | 2016-04-08 | 2024-02-02 | 中国航发贵州黎阳航空动力有限公司 | 一种涡轮叶片涡流探伤对比试块加工夹具及其制作方法 |
CN109341507A (zh) * | 2018-11-20 | 2019-02-15 | 中国航发贵州黎阳航空动力有限公司 | 一种涡流测厚校准对比装置 |
CN109341507B (zh) * | 2018-11-20 | 2020-09-29 | 中国航发贵州黎阳航空动力有限公司 | 一种涡流测厚校准对比装置 |
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Address after: 550000 No. 1111 Liyang Road, Baiyun District, Guiyang City, Guizhou Province Patentee after: AIR CHINA FA GUIZHOU LIYANG AVIATION POWER Co.,Ltd. Address before: Mailbox No.5, Pingba County, Anshun City, Guizhou Province Patentee before: GUIZHOU LIYANG AVIATION POWER Co.,Ltd. |
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