CN102581620B - Method for turning and milling to realize typical characteristics of aircraft landing gear - Google Patents
Method for turning and milling to realize typical characteristics of aircraft landing gear Download PDFInfo
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- CN102581620B CN102581620B CN 201210066834 CN201210066834A CN102581620B CN 102581620 B CN102581620 B CN 102581620B CN 201210066834 CN201210066834 CN 201210066834 CN 201210066834 A CN201210066834 A CN 201210066834A CN 102581620 B CN102581620 B CN 102581620B
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- 238000003801 milling Methods 0.000 title claims abstract description 80
- 238000000034 method Methods 0.000 title claims abstract description 14
- 238000007514 turning Methods 0.000 title abstract description 6
- 238000005520 cutting process Methods 0.000 claims description 53
- 210000003454 tympanic membrane Anatomy 0.000 claims description 12
- 241000220317 Rosa Species 0.000 claims description 7
- 238000003672 processing method Methods 0.000 claims description 6
- 210000000883 ear external Anatomy 0.000 claims description 3
- 238000009499 grossing Methods 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 238000003754 machining Methods 0.000 abstract description 22
- 238000009966 trimming Methods 0.000 abstract 2
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 210000003128 head Anatomy 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 1
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CN 201210066834 CN102581620B (en) | 2012-03-14 | 2012-03-14 | Method for turning and milling to realize typical characteristics of aircraft landing gear |
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CN 201210066834 CN102581620B (en) | 2012-03-14 | 2012-03-14 | Method for turning and milling to realize typical characteristics of aircraft landing gear |
Publications (2)
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CN102581620A CN102581620A (en) | 2012-07-18 |
CN102581620B true CN102581620B (en) | 2013-11-06 |
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CN 201210066834 Expired - Fee Related CN102581620B (en) | 2012-03-14 | 2012-03-14 | Method for turning and milling to realize typical characteristics of aircraft landing gear |
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Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103273124B (en) * | 2013-05-29 | 2015-06-17 | 广东鸿图南通压铸有限公司 | Manufacturing method for rapidly forming camshaft bracket |
CN104015015B (en) * | 2014-06-23 | 2016-04-06 | 四川明日宇航工业有限责任公司 | Aircraft main landing gear urceolus part by numerical control integrated manufacturing method |
CN104526030B (en) * | 2014-12-08 | 2016-08-24 | 湖南南方宇航工业有限公司 | A kind of processing method of T-shaped thin-walled parts |
CN105499909B (en) * | 2016-01-20 | 2017-09-15 | 哈尔滨飞机工业集团有限责任公司 | A kind of short support arm processing method of helicopter landing gear inner cylinder |
CN106077775B (en) * | 2016-08-04 | 2018-05-08 | 成都航飞航空机械设备制造有限公司 | A kind of processing method of three axis machine tooling back-off class workpiece |
CN106825702B (en) * | 2016-12-15 | 2018-10-19 | 湖北三江航天红阳机电有限公司 | A kind of nose cone hat shape whole glass steel bay section machining process of the end face with angle |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101524776A (en) * | 2008-03-04 | 2009-09-09 | 冯付良 | Orthogonal turn-milling method for rotary part |
CN101670462A (en) * | 2009-09-29 | 2010-03-17 | 江西洪都航空工业集团有限责任公司 | Wall plate processing technology for hyperboloid thin wall |
JP4587623B2 (en) * | 2001-09-26 | 2010-11-24 | コマツ工機株式会社 | Crankshaft machining line machining method |
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2012
- 2012-03-14 CN CN 201210066834 patent/CN102581620B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4587623B2 (en) * | 2001-09-26 | 2010-11-24 | コマツ工機株式会社 | Crankshaft machining line machining method |
CN101524776A (en) * | 2008-03-04 | 2009-09-09 | 冯付良 | Orthogonal turn-milling method for rotary part |
CN101670462A (en) * | 2009-09-29 | 2010-03-17 | 江西洪都航空工业集团有限责任公司 | Wall plate processing technology for hyperboloid thin wall |
Non-Patent Citations (6)
Title |
---|
刘强.大型飞机制造中的关键数控技术及装备.《航空制造技术》.2008,(第5期), |
刘达有.浅谈飞机起落架外筒零件的数控加工.《科技资讯》.2009,(第33期),82. |
大型飞机制造中的关键数控技术及装备;刘强;《航空制造技术》;20080331(第5期);40-43 * |
大型飞机起落架制造技术;李铭;《航空制造技术》;20081231(第21期);68-71 * |
李铭.大型飞机起落架制造技术.《航空制造技术》.2008,(第21期),68-71. |
浅谈飞机起落架外筒零件的数控加工;刘达有;《科技资讯》;20091130(第33期);82 * |
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CN102581620A (en) | 2012-07-18 |
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Legal Events
Date | Code | Title | Description |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
ASS | Succession or assignment of patent right |
Owner name: AVIC LANDING GEAR ADVANCED MANUFACTURING CORP. Effective date: 20121214 |
|
C41 | Transfer of patent application or patent right or utility model | ||
C53 | Correction of patent for invention or patent application | ||
CB03 | Change of inventor or designer information |
Inventor after: Yuan Songmei Inventor after: Zhang Li Inventor after: Zhang Zhigang Inventor before: Yuan Songmei Inventor before: Zhang Li |
|
COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: YUAN SONGMEI ZHANG CHONG TO: YUAN SONGMEI ZHANG CHONG ZHANG ZHIGANG |
|
TA01 | Transfer of patent application right |
Effective date of registration: 20121214 Address after: 100191 Haidian District, Xueyuan Road, No. 37, Applicant after: Beihang University Applicant after: AVIC Landing Gear Advanced Manufacturing Corp. Address before: 100191 Haidian District, Xueyuan Road, No. 37, Applicant before: Beihang University |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131106 Termination date: 20190314 |
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CF01 | Termination of patent right due to non-payment of annual fee |