CN109720544A - 一种大型水上飞机机身垂尾对接结构 - Google Patents
一种大型水上飞机机身垂尾对接结构 Download PDFInfo
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- CN109720544A CN109720544A CN201811342620.8A CN201811342620A CN109720544A CN 109720544 A CN109720544 A CN 109720544A CN 201811342620 A CN201811342620 A CN 201811342620A CN 109720544 A CN109720544 A CN 109720544A
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- fuselage
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- 238000003032 molecular docking Methods 0.000 title claims abstract description 20
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 19
- 230000007704 transition Effects 0.000 claims abstract description 22
- 210000005069 ears Anatomy 0.000 claims abstract description 12
- 230000013011 mating Effects 0.000 claims abstract description 11
- 230000005540 biological transmission Effects 0.000 abstract description 8
- 238000005260 corrosion Methods 0.000 abstract description 6
- 230000007797 corrosion Effects 0.000 abstract description 6
- 230000002180 anti-stress Effects 0.000 abstract description 3
- 238000005516 engineering process Methods 0.000 abstract description 3
- 230000002929 anti-fatigue Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 241000538562 Banjos Species 0.000 description 1
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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CN201811342620.8A CN109720544A (zh) | 2018-11-12 | 2018-11-12 | 一种大型水上飞机机身垂尾对接结构 |
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CN201811342620.8A CN109720544A (zh) | 2018-11-12 | 2018-11-12 | 一种大型水上飞机机身垂尾对接结构 |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110758766A (zh) * | 2019-10-25 | 2020-02-07 | 中航西飞民用飞机有限责任公司 | 一种单耳片接头结构及防止破损的连接方法 |
EP3915871A1 (en) * | 2020-05-27 | 2021-12-01 | The Boeing Company | Aircraft with multi spar box connection to fuselage, and method of attaching a vertical stabilizer |
CN113734418A (zh) * | 2021-10-09 | 2021-12-03 | 贵州贵飞飞机设计研究院有限公司 | 一种避免承受轴向载荷的耳片接头结构 |
CN113830285A (zh) * | 2021-10-25 | 2021-12-24 | 中航通飞华南飞机工业有限公司 | 一种实现破损安全的垂尾主盒段翼梁梢部平垂尾对接接头 |
CN115107986A (zh) * | 2022-07-08 | 2022-09-27 | 白鲸航线(北京)科技有限公司 | 一种翼身连接机身加强框结构 |
US11511846B2 (en) | 2020-05-27 | 2022-11-29 | The Boeing Company | Aircraft with multi spar box connection to fuselage |
US11655019B2 (en) | 2020-05-27 | 2023-05-23 | The Boeing Company | Method and system for coupling a vertical stabilizer to an aircraft fuselage |
US11932398B2 (en) | 2020-08-24 | 2024-03-19 | The Boeing Company | Horizontal stabilizer assembly for an aircraft |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20040023944A (ko) * | 2002-09-12 | 2004-03-20 | 한국항공우주산업 주식회사 | 항공기의 수직미익 장착구조 |
US20110089292A1 (en) * | 2009-01-26 | 2011-04-21 | Airbus Operations Limited | Aircraft joint |
CN102307782A (zh) * | 2008-12-18 | 2012-01-04 | 空客运营有限公司 | 在飞行器的后端中的负载引导区域的结构 |
CN103625631A (zh) * | 2013-08-23 | 2014-03-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种垂尾对接结构设计方法 |
EP3078586A1 (en) * | 2015-04-08 | 2016-10-12 | Airbus Operations S.L. | Aircraft rear structure |
-
2018
- 2018-11-12 CN CN201811342620.8A patent/CN109720544A/zh active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20040023944A (ko) * | 2002-09-12 | 2004-03-20 | 한국항공우주산업 주식회사 | 항공기의 수직미익 장착구조 |
CN102307782A (zh) * | 2008-12-18 | 2012-01-04 | 空客运营有限公司 | 在飞行器的后端中的负载引导区域的结构 |
US20110089292A1 (en) * | 2009-01-26 | 2011-04-21 | Airbus Operations Limited | Aircraft joint |
CN103625631A (zh) * | 2013-08-23 | 2014-03-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种垂尾对接结构设计方法 |
EP3078586A1 (en) * | 2015-04-08 | 2016-10-12 | Airbus Operations S.L. | Aircraft rear structure |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110758766A (zh) * | 2019-10-25 | 2020-02-07 | 中航西飞民用飞机有限责任公司 | 一种单耳片接头结构及防止破损的连接方法 |
CN110758766B (zh) * | 2019-10-25 | 2024-05-24 | 中航西飞民用飞机有限责任公司 | 一种单耳片接头结构及防止破损的连接方法 |
EP3915871A1 (en) * | 2020-05-27 | 2021-12-01 | The Boeing Company | Aircraft with multi spar box connection to fuselage, and method of attaching a vertical stabilizer |
US11370523B2 (en) | 2020-05-27 | 2022-06-28 | The Boeing Company | Aircraft with multi spar box connection to fuselage |
US11511846B2 (en) | 2020-05-27 | 2022-11-29 | The Boeing Company | Aircraft with multi spar box connection to fuselage |
US11655019B2 (en) | 2020-05-27 | 2023-05-23 | The Boeing Company | Method and system for coupling a vertical stabilizer to an aircraft fuselage |
US11932398B2 (en) | 2020-08-24 | 2024-03-19 | The Boeing Company | Horizontal stabilizer assembly for an aircraft |
CN113734418A (zh) * | 2021-10-09 | 2021-12-03 | 贵州贵飞飞机设计研究院有限公司 | 一种避免承受轴向载荷的耳片接头结构 |
CN113830285A (zh) * | 2021-10-25 | 2021-12-24 | 中航通飞华南飞机工业有限公司 | 一种实现破损安全的垂尾主盒段翼梁梢部平垂尾对接接头 |
CN115107986A (zh) * | 2022-07-08 | 2022-09-27 | 白鲸航线(北京)科技有限公司 | 一种翼身连接机身加强框结构 |
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Effective date of registration: 20221024 Address after: 519040 building 201, 999 Jinhai Middle Road, Jinwan District, Zhuhai City, Guangdong Province Applicant after: SOUTH CHINA AIRCRAFT INDUSTRY CO., LTD. OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. Address before: 519040 AVIC Tongfei industrial base, aviation industrial park, Jinwan District, Zhuhai City, Guangdong Province Applicant before: R&D INSTITUTE OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. |
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Application publication date: 20190507 |
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