CN112623187A - 一种翼型的可拆卸替换后缘装置及其制作方法 - Google Patents
一种翼型的可拆卸替换后缘装置及其制作方法 Download PDFInfo
- Publication number
- CN112623187A CN112623187A CN202011611236.0A CN202011611236A CN112623187A CN 112623187 A CN112623187 A CN 112623187A CN 202011611236 A CN202011611236 A CN 202011611236A CN 112623187 A CN112623187 A CN 112623187A
- Authority
- CN
- China
- Prior art keywords
- airfoil
- trailing edge
- wing
- block
- positioning
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Abstract
Description
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011611236.0A CN112623187B (zh) | 2020-12-30 | 2020-12-30 | 一种翼型的可拆卸替换后缘装置及其制作方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011611236.0A CN112623187B (zh) | 2020-12-30 | 2020-12-30 | 一种翼型的可拆卸替换后缘装置及其制作方法 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN112623187A true CN112623187A (zh) | 2021-04-09 |
CN112623187B CN112623187B (zh) | 2022-11-29 |
Family
ID=75286660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011611236.0A Active CN112623187B (zh) | 2020-12-30 | 2020-12-30 | 一种翼型的可拆卸替换后缘装置及其制作方法 |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN112623187B (zh) |
Citations (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5226618A (en) * | 1992-01-30 | 1993-07-13 | The United States Of America As Represented By The Secretary Of The Navy | Lift enhancement device |
WO1998017529A1 (en) * | 1996-10-22 | 1998-04-30 | The Boeing Company | Airplane with unswept slotted cruise wing airfoil |
US20020005461A1 (en) * | 2000-02-14 | 2002-01-17 | Nettle James E. | Method for reducing fuel consumption in aircraft |
US20050118028A1 (en) * | 2003-06-25 | 2005-06-02 | Paul Matheny | Detachable leading edge for airfoils |
US20060060721A1 (en) * | 2004-03-30 | 2006-03-23 | Phillip Watts | Scalloped leading edge advancements |
WO2008012569A2 (en) * | 2006-07-28 | 2008-01-31 | Airbus Uk Limited | Aircrat wing box and manufacture thereof |
US20090277996A1 (en) * | 2008-05-06 | 2009-11-12 | Alenia Aeronautica S.P.A. | Wing and empennage leading edge structure made of thermoplastic material with a stiffened double shell configuration |
US20100148010A1 (en) * | 2006-08-25 | 2010-06-17 | A Partnership Of Jim Langley And Courtney Hunter | Aircraft wing modification and related methods |
CN202320772U (zh) * | 2011-09-02 | 2012-07-11 | 北京航空航天大学 | 一种双通道大型客机的高升力装置 |
US20130289766A1 (en) * | 2010-01-19 | 2013-10-31 | The Boeing Company | Apparatus for Automated Maintenance of Aircraft Structural Elements |
CN105253305A (zh) * | 2015-10-10 | 2016-01-20 | 南京航空航天大学 | 一种基于压电除冰系统的前缘可拆卸式的实验机翼结构 |
CN106005368A (zh) * | 2016-05-16 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种可变后缘的柔性机翼颤振模型 |
CN106005367A (zh) * | 2016-05-16 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种具有主动柔性前缘的颤振模型 |
CN107023515A (zh) * | 2017-06-16 | 2017-08-08 | 吉林大学 | 一种低噪声轴流风机复合仿生翼型叶片 |
CN108100218A (zh) * | 2017-11-16 | 2018-06-01 | 中国航空工业集团公司西安飞机设计研究所 | 一种带翼型的可拆卸雷达罩支撑结构 |
CN208181397U (zh) * | 2018-01-30 | 2018-12-04 | 彩虹无人机科技有限公司 | 一种机翼前缘轻质支架 |
EP3421355A1 (en) * | 2017-06-29 | 2019-01-02 | Airbus Operations GmbH | Aerofoil structure and method of assembly |
CN110015401A (zh) * | 2017-12-13 | 2019-07-16 | 空中客车营运有限公司 | 零件套件、翼型结构和用于组装翼型结构的方法 |
CN209496410U (zh) * | 2017-12-20 | 2019-10-15 | 卢森堡斯耐尔责任有限公司 | 生成表示建筑物中的人运输工具的实际外形的点云的装置 |
CN110550216A (zh) * | 2019-09-24 | 2019-12-10 | 中国人民解放军陆军军事交通学院镇江校区 | 一种动力提升地效飞行器 |
CN111003209A (zh) * | 2019-12-26 | 2020-04-14 | 中国航空工业集团公司西安飞机设计研究所 | 大型尾翼除冰风洞试验装置和方法 |
CN111186593A (zh) * | 2020-01-15 | 2020-05-22 | 通航国际(西安)飞机技术有限公司 | 一种飞机机翼的安装方法 |
-
2020
- 2020-12-30 CN CN202011611236.0A patent/CN112623187B/zh active Active
Patent Citations (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5226618A (en) * | 1992-01-30 | 1993-07-13 | The United States Of America As Represented By The Secretary Of The Navy | Lift enhancement device |
WO1998017529A1 (en) * | 1996-10-22 | 1998-04-30 | The Boeing Company | Airplane with unswept slotted cruise wing airfoil |
US20020005461A1 (en) * | 2000-02-14 | 2002-01-17 | Nettle James E. | Method for reducing fuel consumption in aircraft |
US20050118028A1 (en) * | 2003-06-25 | 2005-06-02 | Paul Matheny | Detachable leading edge for airfoils |
US20060060721A1 (en) * | 2004-03-30 | 2006-03-23 | Phillip Watts | Scalloped leading edge advancements |
WO2008012569A2 (en) * | 2006-07-28 | 2008-01-31 | Airbus Uk Limited | Aircrat wing box and manufacture thereof |
US20100148010A1 (en) * | 2006-08-25 | 2010-06-17 | A Partnership Of Jim Langley And Courtney Hunter | Aircraft wing modification and related methods |
US20090277996A1 (en) * | 2008-05-06 | 2009-11-12 | Alenia Aeronautica S.P.A. | Wing and empennage leading edge structure made of thermoplastic material with a stiffened double shell configuration |
US20130289766A1 (en) * | 2010-01-19 | 2013-10-31 | The Boeing Company | Apparatus for Automated Maintenance of Aircraft Structural Elements |
CN202320772U (zh) * | 2011-09-02 | 2012-07-11 | 北京航空航天大学 | 一种双通道大型客机的高升力装置 |
CN105253305A (zh) * | 2015-10-10 | 2016-01-20 | 南京航空航天大学 | 一种基于压电除冰系统的前缘可拆卸式的实验机翼结构 |
CN106005368A (zh) * | 2016-05-16 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种可变后缘的柔性机翼颤振模型 |
CN106005367A (zh) * | 2016-05-16 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种具有主动柔性前缘的颤振模型 |
CN107023515A (zh) * | 2017-06-16 | 2017-08-08 | 吉林大学 | 一种低噪声轴流风机复合仿生翼型叶片 |
EP3421355A1 (en) * | 2017-06-29 | 2019-01-02 | Airbus Operations GmbH | Aerofoil structure and method of assembly |
CN109204781A (zh) * | 2017-06-29 | 2019-01-15 | 空中客车德国运营有限责任公司 | 翼型结构用结构组件、翼型结构和其组装方法以及飞行器 |
CN108100218A (zh) * | 2017-11-16 | 2018-06-01 | 中国航空工业集团公司西安飞机设计研究所 | 一种带翼型的可拆卸雷达罩支撑结构 |
CN110015401A (zh) * | 2017-12-13 | 2019-07-16 | 空中客车营运有限公司 | 零件套件、翼型结构和用于组装翼型结构的方法 |
CN209496410U (zh) * | 2017-12-20 | 2019-10-15 | 卢森堡斯耐尔责任有限公司 | 生成表示建筑物中的人运输工具的实际外形的点云的装置 |
CN208181397U (zh) * | 2018-01-30 | 2018-12-04 | 彩虹无人机科技有限公司 | 一种机翼前缘轻质支架 |
CN110550216A (zh) * | 2019-09-24 | 2019-12-10 | 中国人民解放军陆军军事交通学院镇江校区 | 一种动力提升地效飞行器 |
CN111003209A (zh) * | 2019-12-26 | 2020-04-14 | 中国航空工业集团公司西安飞机设计研究所 | 大型尾翼除冰风洞试验装置和方法 |
CN111186593A (zh) * | 2020-01-15 | 2020-05-22 | 通航国际(西安)飞机技术有限公司 | 一种飞机机翼的安装方法 |
Non-Patent Citations (4)
Title |
---|
吕强等: "充气结构机翼的设计和试验研究", 《飞行力学》 * |
石磊: "NACA0018翼型模型的仿生降噪", 《吉林大学学报》 * |
石磊等: "NACA0018翼型模型的仿生降噪", 《吉林大学学报(工学版)》 * |
程颖颐等: "基于仿生学结构的翼型降噪实验研究", 《工程热物理学报》 * |
Also Published As
Publication number | Publication date |
---|---|
CN112623187B (zh) | 2022-11-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US9377005B2 (en) | Airfoil modifiers for wind turbine rotor blades | |
CN201771673U (zh) | 风电叶片表面之涡流发生器 | |
CN102465828B (zh) | 用于风力涡轮机中转子叶片的降噪装置 | |
US7980515B2 (en) | Aircraft wing modification and related methods | |
US5711653A (en) | Air lifted airfoil | |
CN104704233B (zh) | 燕尾型翼 | |
LORBER et al. | A comprehensive hover test of the airloads and airflow of an extensively instrumented model helicopter rotor | |
DK2942521T3 (en) | WORTEX GENERATOR REPAIR PROCEDURE AND A BUILDING SET THEREOF | |
DE602006004461D1 (de) | Anordnung für ein flugzeug mit einem flügelsystemelement und einem befestigungsmast | |
ATE496826T1 (de) | Schlitzflügel für flugzeug | |
DE112005000443T5 (de) | Vorderkantenvorrichtungssystem für Luftfahrzeuge und entsprechende Dimensionierungsverfahren | |
CN106289680B (zh) | 用于风洞静气弹试验的试验装置 | |
CN1867771A (zh) | 用于风力设备的转子叶片 | |
DE102008002930A1 (de) | Rotorflügel-Spitzenwirbelbrecher | |
CN105863955A (zh) | 用于转子叶片的涡流发生器 | |
DE102010026588A1 (de) | Windenergieanlagenrotorblatt mit optimierter Hinterkante | |
CN112623187B (zh) | 一种翼型的可拆卸替换后缘装置及其制作方法 | |
BR102013023117A2 (pt) | Conjunto de armação para um molde de pá do rotor, molde para formar uma pá do rotor e método para formar uma pá do rotor | |
RU2008138594A (ru) | Крыло летательного аппарата (варианты), отклоняемый предкрылок и летательный аппарат | |
EP2951445A1 (en) | Fluid flow modification apparatus | |
CN209192179U (zh) | 一种尾舵及包含该尾舵的水上装置 | |
CN100497090C (zh) | 一种适用于平流层低雷诺数、高效三叶螺旋桨 | |
CN207550540U (zh) | 颤振模型 | |
CN208828131U (zh) | 一种飞机侧翼的保养设备 | |
CN212090886U (zh) | 一种航空模型无动力滑翔结构 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
CB03 | Change of inventor or designer information | ||
CB03 | Change of inventor or designer information |
Inventor after: Zhang Yingchao Inventor after: Zhang Chengchun Inventor after: Han Zhiwu Inventor after: Wang Zhongjian Inventor after: Jiang Qingwen Inventor after: Liu Tao Inventor after: Xu Jincheng Inventor after: Yu Xin Inventor after: Tong Zhongqing Inventor after: Shen Chun Inventor after: Wang Guohua Inventor before: Zhang Yingchao Inventor before: Wang Zhongjian Inventor before: Jiang Qingwen Inventor before: Liu Tao Inventor before: Xu Jincheng Inventor before: Yu Xin Inventor before: Tong Zhongqing Inventor before: Shen Chun Inventor before: Wang Guohua |
|
GR01 | Patent grant | ||
GR01 | Patent grant |