公开(公告)号：EP3002211A1

公开(公告)日：2016-04-06

申请号：EP14187079.0

申请日：2014-09-30

申请人： Messier-Dowty Limited

发明人： Foster, Nicholas ,  Villain-Chastre, Jean-Philippe ,  Bennett, Ian

IPC分类号： B64C25/10

CPC分类号： B64C25/10

摘要： An aircraft landing gear assembly (10) including structural elements (12, 14) coupled via a coupling including a bearing (22). The bearing is arranged in use to withstand static pressure of at least 300Mpa. At least half the thickness and/or volume of the bearing is formed from a polymer layer.

摘要翻译： 一种包括通过包括轴承（22）的联轴器联接的结构元件（12,14）的飞机起落架组件（10）。 轴承的使用安排是为了承受至少300Mpa的静态压力。 轴承的厚度和/或体积的至少一半由聚合物层形成。

公开(公告)号：EP2951087A1

公开(公告)日：2015-12-09

申请号：EP14704874.8

申请日：2014-02-04

申请人： Messier-Dowty Limited

发明人： HODGKINSON, Ben ,  SCHMIDT, R. Kyle ,  SMART, David

IPC分类号： B64C25/34

CPC分类号： B64C25/60 ,  B64C25/34 ,  F16F9/10 ,  F16F9/34

摘要： A pitch trimmer assembly for an aircraft landing gear having a damping element arranged to be connected between a first and a second element of an aircraft landing gear and arranged to exert a first damping force when in a first state and a second damping force in a second state, the damping element being switchable between the first and second states in dependence on the relative positions of the first and second landing gear elements.

摘要翻译： 一种用于飞机起落架的俯仰修剪器组件，包括伸缩俯仰修剪器致动器（12），其布置成连接在飞机起落架的第一和第二元件之间，并且布置成当处于第一状态 在所述俯仰调节器致动器（12）完全缩回的第二状态下，所述俯仰调节器致动器（12）不完全缩回并且第二阻尼力大于所述第一阻尼力，所述阻尼元件能够在第一状态和第二状态之间切换 依赖于第一起落架元件和第二起落架元件的相对位置。

公开(公告)号：EP2526018B1

公开(公告)日：2015-10-14

申请号：EP11702281.4

申请日：2011-01-19

申请人： Messier-Dowty Limited

发明人： BENNETT, Ian

IPC分类号： B64C25/34 ,  B64C25/50

CPC分类号： B64C25/34 ,  B64C2025/345

公开(公告)号：EP2812243A1

公开(公告)日：2014-12-17

申请号：EP13703863.4

申请日：2013-01-23

申请人： Messier-Dowty Limited

发明人： SIMMONEAUX, Yann ,  HARRIS, Simon D.

IPC分类号： B64C25/32 ,  B64C25/16

CPC分类号： B64C25/16 ,  B64C25/32 ,  B64C2025/003

摘要： An aircraft landing gear including wheels and a fairing arranged to be moveable between a first and a second configuration, wherein in the first configuration the fairing is arranged to shield an element of the landing gear from incident airflow and wherein in the second configuration the fairing is arranged to deflect debris or spray propelled from one or more of the wheels.

摘要翻译： 一种包括轮和整流罩的飞行器起落架，其布置成可在第一和第二构造之间移动，其中在第一构型中，整流罩布置成屏蔽起落架的元件与入射气流，并且其中在第二构造中，整流罩 布置成偏转碎片或从一个或多个轮子推进的喷雾。

公开(公告)号：EP2490938B1

公开(公告)日：2014-05-14

申请号：EP10718675.1

申请日：2010-04-30

申请人： Messier-Dowty Limited

发明人： HILLIARD, Matthew ,  BENNETT, Ian

IPC分类号： B64C25/34

CPC分类号： B64C25/34

公开(公告)号：EP2544948A1

公开(公告)日：2013-01-16

申请号：EP11705238.1

申请日：2011-02-16

申请人： Messier-Dowty Limited

发明人： DEVILLERS, Christophe ,  HODGKINSON, Ben

IPC分类号： B64C25/00

CPC分类号： B64C25/02 ,  B64C25/001 ,  B64C25/34 ,  B64C25/58 ,  B64D2045/008

摘要： A stop pad (11) for an aircraft landing gear arranged to provide protection against impact between first and second elements of the landing gear, the stop pad being arranged to provide an indication that it is been subject to an impact against one of the first or second landing gear elements, the impact having an impact load above a predetermined threshold level.

摘要翻译： 一种用于飞机起落架的止动垫（11），其被布置成提供防止起落架的第一和第二元件之间的冲击的保护，所述止动垫被布置成提供其指示，所述指示受到与所述第一或第 第二起落架元件，所述冲击具有高于预定阈值水平的冲击载荷。

公开(公告)号：EP2534048A1

公开(公告)日：2012-12-19

申请号：EP11703258.1

申请日：2011-02-07

申请人： Messier-Dowty Limited

发明人： BENNETT, Ian

IPC分类号： B64C25/50

CPC分类号： B64C25/50 ,  B64C25/34 ,  B64C2025/345

摘要： A landing gear (10), including an elongate axle (16a) pivotally (18) connected to a bogie beam (14), the landing gear further including a locking device (30) for locking the axle at a substantially fixed orientation with respect to the bogie beam, the locking device including first and second barrier arms (32c, 34c) that are movable between a first configuration, in which they define a barrier so as to maintain the maintain the axle in the substantially fixed orientation with respect to the bogie beam, and a second configuration, in which the axle may pivot about the bogie beam.

摘要翻译： 一种起落架（10），其包括连接到转向架梁（14）的枢转（18）的细长轴（16a），所述起落架还包括锁定装置（30），用于将所述轴锁定在相对于 所述转向架梁包括第一和第二障碍臂（32c，34c），所述第一和第二障碍臂可在第一构造和第二构造之间移动，在所述第一构造中，所述第一和第二障碍臂限定障碍物以维持所述轴相对于所述转向架保持基本固定的取向 以及第二配置，其中轴可以围绕转向架梁枢转。

公开(公告)号：EP2509863A1

公开(公告)日：2012-10-17

申请号：EP10718678.5

申请日：2010-04-30

申请人： Messier-Dowty Limited

发明人： SIMONNEAUX, Yann

IPC分类号： B64C25/00

CPC分类号： B64C25/001 ,  B64C2025/003

摘要： An aircraft landing gear including a fairing (12) arranged to be moveable between first and second configurations, wherein in the first configuration the fairing shields an element of the landing gear from an incident airflow, the fairing being arranged to be in the first configuration when the landing gear is deployed but unloaded, and wherein in the second configuration the fairing exposes the landing gear element to the incident airflow, the fairing being arranged to be in the second configuration when the landing gear is deployed and loaded.

公开(公告)号：EP2470423A2

公开(公告)日：2012-07-04

申请号：EP10747480.1

申请日：2010-08-16

申请人： Messier-Dowty Limited

发明人： BENNETT, Ian

IPC分类号： B64C25/12

CPC分类号： B64C25/14 ,  B64C25/20 ,  B64C25/34 ,  B64C2025/125

摘要： A main landing gear assembly for an aircraft comprising: an elongate beam pivotally coupled about its longitudinal axis to the aircraft such that the axis of rotation of the elongate beam is generally parallel to the longitudinal axis of the aircraft fuselage; a shock strut pivotally coupled at a first end to the elongate beam and coupled at a second end to a wheel assembly; a folding forward stay pivotally coupled at a first end to the elongate beam and pivotally coupled at a second end to the shock strut; and a rigid rear stay pivotally coupled at a first end to the aircraft and pivotally coupled at a second end to the shock strut, the rigid rear stay being arranged to restrain the path of the shock strut when moving between a deployed and a retracted position such that the wheel assembly is located forward and inboard in the retracted position in comparison with its location in the deployed position.

公开(公告)号：EP2470352A1

公开(公告)日：2012-07-04

申请号：EP10750155.3

申请日：2010-08-24

申请人： Messier-Dowty Limited ,  Messier-Dowty SA

发明人： BOND, David ,  TROWBRIDGE, Paul ,  SMITH, Andy ,  MASSON, Richard ,  DUNLEAVY, Patrick

IPC分类号： B29C70/30 ,  B29C70/86 ,  B29C53/58 ,  F16C3/02 ,  F16C7/00

CPC分类号： B29C70/86 ,  B29C53/585 ,  B29C70/30 ,  B29C70/48 ,  B29L2031/75 ,  F16C7/026 ,  Y02T50/43 ,  Y10T29/49826 ,  Y10T403/37 ,  Y10T403/47 ,  Y10T403/475

摘要： An apparatus includes a fitting connected to a body. The fitting has an engagement portion including a channel formed into a peripheral surface of it and an axis. The body includes an axial layer provided around at least some of the peripheral surface of the engagement portion of the end fitting and a hoop layer provided around the axial layer at a location corresponding to at least some of the channel so as to urge at least some of the axial layer into a portion of the channel. The channel is arranged such that at least some of it defines a pathway that is non-orthogonal with respect to the axis of the fitting, such that at least some of the surface area of the channel defines a load bearing surface for the transfer of torque between the fitting and body when a rotational force is applied to one of them.