专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

21. 发明专利

JP5453408B2 Method and apparatus for producing fiber-reinforced thermoplastic composite structure 有权
公开(公告)号：JP5453408B2
公开(公告)日：2014-03-26
申请号：JP2011515608
申请日：2009-06-22
申请人：エアバスオペレーションズリミティド
发明人：インストン，デイビッド
IPC分类号： B29C65/08
CPC分类号： B29C65/08 , B29C35/0261 , B29C35/0266 , B29C35/045 , B29C35/0805 , B29C35/10 , B29C65/081 , B29C65/085 , B29C65/10 , B29C65/16 , B29C65/1612 , B29C65/1658 , B29C65/18 , B29C65/72 , B29C66/0242 , B29C66/1122 , B29C66/43 , B29C66/71 , B29C66/721 , B29C66/731 , B29C66/73117 , B29C66/73921 , B29C66/73941 , B29C66/83411 , B29C66/836 , B29C66/91411 , B29C66/91445 , B29C66/91941 , B29C66/91943 , B29C66/9592 , B29C70/386 , B29C2035/0822 , B29C2035/0838 , B29K2101/10 , B29K2101/12 , B29K2105/06 , B29K2307/00 , B32B37/06 , B32B37/14 , B32B2305/08 , B32B2310/028 , B32B2310/0843 , C08J5/04 , Y02T50/433 , Y10T428/24 , B29K2071/00
摘要： A method of fabricating a fiber reinforced thermoplastic composite structure comprising: placing a first layer of fiber reinforced thermoplastic material on top of a second layer of fiber reinforced thermoplastic material; providing a local heating source and locally heating a portion of at least the upper layer of thermoplastic composite material; and providing an ultrasonic transducer and locally introducing ultrasonic energy waves to the heated portion of the thermoplastic material such that ultrasonic consolidation of the fiber reinforced thermoplastic occurs.

22. 发明专利

JP5416209B2 Angled stiffener apparatus and method for forming an inclined stiffener 有权
公开(公告)号：JP5416209B2
公开(公告)日：2014-02-12
申请号：JP2011518001
申请日：2009-07-14
申请人：エアバスオペレーションズリミティド
发明人：ジョンウィンター，ダレン
IPC分类号： B29C70/52 , B21D5/08 , B29C53/04 , B64C1/06 , B64F5/00
CPC分类号： B64C1/064 , B29C70/504 , B29D99/0007 , B64C3/182 , B64C2001/0072 , Y02T50/433
摘要： A stiffener has an elongate web element and an elongate foot element connected by a curved elbow that has a radius greater over a first portion than over a second portion of the stiffener. The stiffener is formed by feeding an elongate member through a roll forming die having first and second rollers, the first roller having a shaped section arranged to be located within a correspondingly shaped recess in the second roller, the first and second rollers defining a gap there between corresponding to the desired shape to be imparted on the elongate member, the desired shape including a curved elbow between a web and a foot portion, wherein the shapes of the recess and the shaped section vary such that the radius of curvature of the gap between the rollers corresponding to the curved elbow varies between a minimum and a maximum value.

23. 发明专利

JP5336604B2 How to control the center of gravity of the aircraft 有权
公开(公告)号：JP5336604B2
公开(公告)日：2013-11-06
申请号：JP2011538043
申请日：2008-11-25
申请人：エアバスオペレーションズリミティド
发明人：スポッティスウッド，ミシェル , ブルクアール，アントワーヌ , スユンガルゴールド，ペーター
IPC分类号： B64C17/10 , B64D45/00
CPC分类号： B64C17/10 , G01M1/127
摘要： A method of controlling the centre of gravity of an aircraft having a plurality of fuel tanks, the method comprising transferring fuel from one or more of the fuel tanks according to a predetermined sequence, the timing of the sequence being dependent on the decrease in gross weight of the aircraft.

24. 发明专利

JP5336575B2 Slat deployment mechanism 有权
公开(公告)号：JP5336575B2
公开(公告)日：2013-11-06
申请号：JP2011501295
申请日：2009-03-12
申请人：エアバスオペレーションズリミティド
发明人：マン，アラン
IPC分类号： B64C9/24
CPC分类号： B64C9/22 , B64C2009/143
摘要： An aircraft slat deployment mechanism including a first drive member coupled to a slat at a first pivot point and a second drive member coupled to the slat at a second pivot point offset from the first pivot point. A first rack is provided on the first drive member, and a first pinion is carried by the drive shaft. The first pinion is arranged to transmit mechanical power from the drive shaft to the first drive member via the first rack. A second rack is provided on the second drive member, and a second pinion is carried by the drive shaft. The second pinion has a different radius to the first pinion. The second pinion is arranged to transmit mechanical power from the drive shaft to the second drive member via the second rack, such that the first and second drive members move at a different speed.

25. 发明专利

JP5302198B2 Door for opening and closing a door opening in the aircraft 有权
公开(公告)号：JP5302198B2
公开(公告)日：2013-10-02
申请号：JP2009530946
申请日：2007-10-01
申请人：エアバスオペレーションズリミティド
发明人：ジョージシブレイ，マルコム
IPC分类号： B64C1/14
CPC分类号： B64C1/1415 , B64C1/1407 , B64C25/16
摘要： An aircraft door is disclosed comprising a first (301), second (302) and third (303) door members pivotably joined and arranged to move from a closed position in which said members are located in a substantially linear arrangement in the aircraft skin to an open position in which said members are located in a relative folded arrangement with the second and third door members situated substantially above the lowest edge of the first door member.

26. 发明专利

JP2013144809A Method of manufacturing composite material 有权
标题翻译：制造复合材料的方法
公开(公告)号：JP2013144809A
公开(公告)日：2013-07-25
申请号：JP2013068680
申请日：2013-03-28
申请人： Airbus Operations Ltd , エアバスオペレーションズリミティド
发明人： FARMER BENJAMIN LIONEL , JOHNS DANIEL MARK
IPC分类号： C08J5/04 , C08K7/06 , C08L101/00
CPC分类号： C08J7/123 , B29C70/30 , B29C70/62 , B33Y10/00 , B82Y30/00 , C08J5/042
摘要： PROBLEM TO BE SOLVED: To provide a method of manufacturing an excellent composite material.SOLUTION: A method of manufacturing a composite material includes: growing a layer of reinforcement; and impregnating the layer with a matrix. The reinforcement layer may be formed by a chemical vapor deposition process. The method can be used as an additive layer-manufacturing technique to form a component with a desired shape and physical characteristics, or can be used to form a thin sheet material.
摘要翻译：要解决的问题：提供一种制造优异的复合材料的方法。解决方案：复合材料的制造方法包括：生长一层增强材料; 并用基体浸渍该层。加强层可以通过化学气相沉积工艺形成。该方法可以用作添加剂层制造技术以形成具有所需形状和物理特性的组分，或者可以用于形成薄片材料。

27. 发明专利

JP5243424B2 How to stringer of the aircraft wing and forming the same 有权
公开(公告)号：JP5243424B2
公开(公告)日：2013-07-24
申请号：JP2009521347
申请日：2007-07-19
申请人：エアバスオペレーションズリミティド
发明人：チャイルズ，トーマス
IPC分类号： B64C3/18
CPC分类号： B64C3/182 , Y10T29/49622

28. 发明专利

JP5129239B2 Bearing fault indicator 有权
公开(公告)号：JP5129239B2
公开(公告)日：2013-01-30
申请号：JP2009510522
申请日：2007-05-03
申请人：エアバスオペレーションズリミティド
发明人：ブレーズ，ポール , ジョンヘンリーバーネス，リチャード
IPC分类号： F16C19/52 , B64C13/00 , F16C41/00
CPC分类号： G01M13/04 , F16C11/045 , F16C19/38 , F16C19/52 , F16C23/086

29. 发明专利

JP2011529006A How to reinforce the ribs 有权
标题翻译：空值
公开(公告)号：JP2011529006A
公开(公告)日：2011-12-01
申请号：JP2011519242
申请日：2009-07-20
申请人：エアバスオペレーションズリミティド
发明人：ウィリアムズ，スティーブン
IPC分类号： B64C3/18 , B64F5/00
CPC分类号： B64C3/187 , B64F5/10 , Y10T29/49622
摘要：航空機の翼の組立中、リブ（１９、２０）を補強する方法が記載される。スティフナーパネル（４０、４１）がリブ（１９、２０）の表面に取り付けられる。リブはスティフナーパネル（４０、４１）が取り付けられた状態で１以上の翼部品に整列される。ドリルで孔を開けること（１６）のような組立作業が、リブが整列され且つスティフナーパネルが取り付けられた状態で行われる。スティフナーパネル（４０、４１）は組立作業後にリブから取り外される。スティフナーパネルは、パネルの表面上に設置され且つ真空空洞部の外周を形成する弾性の外側シールリングと、外側シールリングによって画成される外周内においてパネル（２０、２１）上に設置され且つ真空空洞部の内周を形成する少なくとも一つの弾性の内側シールリングとを有する。真空クランプ力によって、スティフナーをリブに取り付けることができ、真空は外側シールリング及び内側シールリングによってシールされる。内側シールリングは、リブに存在するいくつかの孔をシールする。スティフナー（４０、４１）は、リブに所要の平面度を与えるべく、整列中、リブ（２０、２１）を支持することができる。
摘要翻译：描述了在飞行器机翼的组装期间加强肋（19,20）的方法。加强板（40,41）附接到肋（19,20）的表面。肋与一个或多个机翼部件对准，并且加强板（40,41）连接在一起。执行诸如钻孔（16）的组装操作，其中肋对准并且加强板连接。在组装操作之后，加强板（40,41）从肋上移除。加强板具有弹性的外部密封环，其安装在面板的表面上并形成真空腔的外周; 以及至少一个弹性内部密封环，其安装在由外部密封环限定的周边内的面板（20,21）上并形成真空腔的内部周边。加强件可以通过真空夹紧力连接到肋上，真空由外部和内部密封环密封。内密封环密封肋中存在的任何孔。加强件（40,41）可以在对准期间支撑肋（20,21），以使其成为所需的平整度。

30. 发明专利

JP2011519046A Ultrasonic inspection method and ultrasonic inspection apparatus 审中-公开
公开(公告)号：JP2011519046A
公开(公告)日：2011-06-30
申请号：JP2011506775
申请日：2009-04-20
申请人：エアバスオペレーションズリミティド
发明人：カズンズ，ジョン
IPC分类号： G01N29/04
CPC分类号： G01N29/28 , G01N29/043
摘要： A method of inspecting a component, the component comprising a hole with an entrance. The method comprises: directing ultrasound into the component via a liquid coupling medium; receiving ultrasound from the component via the liquid coupling medium; and processing the received ultrasound to determine a property of the component. The entrance of the hole is sealed with tape to prevent the liquid coupling medium from flowing into the entrance of the hole. The tape has an acoustic impedance within 40% of the acoustic impedance of the liquid coupling medium. By selecting a tape with an acoustic impedance relatively close to that of the liquid coupling medium (which in most cases will be water) the tape is relatively transparent to ultrasound and thus enables at least the presence or absence of a defect in a wall of the hole to be determined.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式