-
公开(公告)号：EP3069993A1
公开(公告)日：2016-09-21
申请号：EP15160005.3
申请日：2015-03-20
发明人： SCHMIDT, Robert Kyle
IPC分类号： B64C25/58
摘要： An aircraft landing gear assembly (10) includes a fibre composite leaf spring (30) arranged as a down lock spring to make the lock link (14).
摘要翻译： 一种飞机起落架组件（10）包括布置成锁定弹簧以形成锁定连杆（14）的纤维复合板簧（30）。
-
公开(公告)号：EP3069991A1
公开(公告)日：2016-09-21
申请号：EP15160002.0
申请日：2015-03-20
发明人： Schmidt, Robert Kyle
IPC分类号： B64C25/26
摘要： An aircraft landing gear assembly (10) includes a bi-stable, split line tube (22) biased to assume a tubular condition to serve in place of a lock link or side stay and an actuator (24) configured to radially enlarge the tube at a region for folding.
摘要翻译： 一种飞机起落架组件（10）包括偏置成呈现管状状态以代替锁定连杆或侧支架的双稳态分裂管线管（22），以及致动器（24），所述致动器（24） 一个折叠区域。
-
公开(公告)号：EP2534048B1
公开(公告)日：2016-04-20
申请号：EP11703258.1
申请日：2011-02-07
发明人： BENNETT, Ian
CPC分类号： B64C25/50 , B64C25/34 , B64C2025/345
-
公开(公告)号：EP2989005A1
公开(公告)日：2016-03-02
申请号：EP14720213.9
申请日：2014-04-24
CPC分类号： F15B15/1457 , B64C25/60 , F15B11/123 , F15B15/1409 , F15B15/1438 , F16F9/063 , F16F9/486
摘要： An actuator arranged to be movable between an extended condition and a compressed condition and being biased to an intermediate condition between and distinct from the extended condition and the compressed condition. The actuator includes a damping device arranged to define the damping coefficient of the actuator. The damping device is arranged to provide a relatively low damping coefficient when the actuator is in a first condition distinct from the intermediate condition, and a relatively high damping coefficient when the actuator is in a second condition, the second condition being distinct from the first condition and being equal or adjacent to the intermediate condition
摘要翻译： 致动器（10）被布置成可在延伸状态和压缩状态之间移动并被偏置到介于延伸状态和压缩状态之间的中间状态。 致动器包括布置成限定致动器的阻尼系数的阻尼装置（40）。 当致动器处于不同于中间状态的第一状态时，阻尼装置被设置成提供相对低的阻尼系数，并且当致动器处于第二状态时，阻尼装置具有相对高的阻尼系数，第二状态不同于第一状态 并等于或接近中间条件。
-
公开(公告)号：EP2776734A1
公开(公告)日：2014-09-17
申请号：EP12790941.4
申请日：2012-11-01
发明人： SCHMIDT, Kyle
摘要： An oleo-pneumatic shock absorber having a casing, a rod slidably mounted in the casing, first and second fluids in the casing, and a gauge. The gauge has a substrate positioned on the shock absorber. The substrate has a first region with a slot sized to fit an ultrasonic transducer arranged to encompass a range of possible oil levels within the shock absorber, a second region corresponding to a range of possible extension states of the shock absorber and a third region comprising one or more traces. Each trace corresponds to a temperature value and is indicative of an optimum relationship between the oil levels and the range of extension states at the respective temperature value associated with the trace.
摘要翻译： 用于指示油气减震器中的油位是否需要修改的量表。 该量规包括用于相对于油气缓冲器定位的基板。 衬底具有第一区域和第二区域，第一区域布置成包围减震器内的可能油位的范围，第二区域对应于减震器的可能延伸状态的范围，第三区域包括一个或多个迹线。 每条迹线对应于一个温度值，并表示油位与与迹线相关的相应温度值处的延伸状态范围之间的最佳关系。
-
公开(公告)号：EP2490937B1
公开(公告)日：2014-02-19
申请号：EP10718674.4
申请日：2010-04-30
发明人： SIMONNEAUX, Yann
IPC分类号： B64C25/02
CPC分类号： B64C25/02
-
公开(公告)号：EP2248720B1
公开(公告)日：2013-04-17
申请号：EP10174045.4
申请日：2006-08-04
发明人： Bennett, Ian , Lang, Richard , Menezes, Robert
-
公开(公告)号：EP2576341A1
公开(公告)日：2013-04-10
申请号：EP11722147.3
申请日：2011-05-19
CPC分类号： B64C25/50 , B64C25/34 , B64C2025/345
摘要： A landing gear (10), including: a bogie beam (12); an axle (14) pivotally connected to the bogie beam (12); a locking member (40) coupled to the axle (14) such that movement of the axle (14) invokes movement of the locking member (40), said movement of the locking member (40) defining a swept volume; and a locking mechanism (60) coupled to the bogie beam (12) and including first (65a) and second glide members, (65a, 65b) the locking mechanism (60) being arranged to move the glide members (65a, 65b) between locking positions, where glide members (65a, 65b) are within the swept volume on opposing sides of the locking member (40) and in which position the locking mechanism (60) is arranged to lock the locking member (40) in a predetermined position, and non- locking positions, where the locking mechanism (60) is arranged permit movement of the locking member (40).
摘要翻译： 一种起落架（10），包括：转向架梁（12）; 枢轴地连接到所述转向架梁（12）的轴（14）; （14）上的锁定构件（40），使得所述轴（14）的移动引起所述锁定构件（40）的移动，所述锁定构件（40）的所述移动限定了扫掠体积; 和联接到所述转向架梁（12）并且包括第一滑动构件（65a）和第二滑行构件（65a，65b）的锁定机构（60），所述锁定机构（60）布置成使所述滑动构件（65a，65b） 锁定位置，其中滑动构件（65a，65b）位于锁定构件（40）的相对侧上的扫掠体积内，并且锁定机构（60）布置成在该位置将锁定构件（40）锁定在预定位置 和非锁定位置，其中锁定机构（60）被布置为允许锁定构件（40）的移动。
-
公开(公告)号：EP2490938A1
公开(公告)日：2012-08-29
申请号：EP10718675.1
申请日：2010-04-30
发明人： HILLIARD, Matthew , BENNETT, Ian
IPC分类号： B64C25/34
CPC分类号： B64C25/34
摘要： An aircraft landing gear assembly including a bogie beam, a landing gear strut (1) having a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam (3), and a stop (13) arranged to limit pivotal movement of the bogie beam relative to the landing gear strut, wherein the stop comprises at least one elongate member arranged to be deflectable in bending when the bogie beam reaches a pivotal limit.
-
公开(公告)号：EP2490937A1
公开(公告)日：2012-08-29
申请号：EP10718674.4
申请日：2010-04-30
发明人： SIMONNEAUX, Yann
IPC分类号： B64C25/02
CPC分类号： B64C25/02
摘要： Aircraft landing gear including at least one load bearing longitudinal structural element (116) wherein said longitudinal structural element is hollow and is arranged to have at least one non-structural element (118) located inside.
-
-
-
-
-
-
-
-
-
搜索结果
73 条记录 (耗时 0.018 秒)
