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1. 发明申请

WO2012069806A1 MECHANICAL POSITION INDICATOR FOR UN AIRCRAFT LANDING GEAR 审中-公开
标题翻译：联合国飞机起落架机械位置指示器
公开(公告)号：WO2012069806A1
公开(公告)日：2012-05-31
申请号：PCT/GB2011/052182
申请日：2011-11-09
申请人： MESSIER-DOWTY LIMITED , HODGKINSON, Ben , LACY, Stuart , WEBB, Chris , ANSON, Garry
发明人： HODGKINSON, Ben , LACY, Stuart , WEBB, Chris , ANSON, Garry
IPC分类号： B64D45/00 , B64C25/00
CPC分类号： B64D45/0005 , B64C25/00 , B64D2045/008
摘要： A mechanical position indicator (9a) for providing a visual indication that a first part of an aircraft landing gear (1) has assumed a predetermined position relative to a second part, the position indicator (9a) being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element (15a) in a deployed position, the position indicator (9a) being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator (9a) from the first state to a second state in which the indicator element (15a) is displaced from the deployed position, the position indicator (9a) being arranged to inhibit the indicator element (15a) thereafter returning to the deployed position.
摘要翻译：一种用于提供飞行器起落架（1）的第一部分相对于第二部分已经具有预定位置的视觉指示的机械位置指示器（9a），所述位置指示器（9a）被布置成联接到第一部分的第一和第二部分，并且在布置成将展示元件（15a）保持在展开位置的第一状态下，位置指示器（9a）被布置成使得在第一部分相对于第二部分呈现预定位置时，第一和第二部分中的第二部分将位置指示器（9a）从第一状态改变到指示元件（15a）从展开位置移位的第二状态，位置指示器（9a）布置成禁止指示器元件（15a）此后返回到展开位置。

2. 发明申请

WO2011110829A1 AIRCRAFT LANDING GEAR STOP PAD 审中-公开
标题翻译：飞机接地齿轮停止垫
公开(公告)号：WO2011110829A1
公开(公告)日：2011-09-15
申请号：PCT/GB2011/050308
申请日：2011-02-16
申请人： MESSIER-DOWTY LIMITED , DEVILLERS, Christophe , HODGKINSON, Ben
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，所述指示受到对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。

3. 发明申请

WO2014118576A1 PITCH TRIMMER ACTUATOR WITH VARIABLE DAMPING 审中-公开
标题翻译： PITCH TRIMMER执行器与可变阻尼
公开(公告)号：WO2014118576A1
公开(公告)日：2014-08-07
申请号：PCT/GB2014/050303
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 comprises a telescopic pitch trimmer actuator (12) 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 in which the pitch trimmer actuator (12) is not fully retracted and a second damping force greater than the first damping force in a second state in which the pitch trimmer actuator (12) is fully retracted, 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式俯仰微调器致动器（12），其布置成连接在飞行器起落架的第一和第二元件之间，并布置成当处于第一状态时施加第一阻尼力，其中，间距修剪器致动器（12）未完全缩回，并且在俯仰修剪器致动器（12）完全缩回的第二状态下，第二阻尼力大于第一阻尼力，阻尼元件可在第一和第二状态之间切换依赖于第一和第二起落架元件的相对位置。

4. 发明公开

EP2643214A1 MECHANICAL POSITION INDICATOR FOR UN AIRCRAFT LANDING GEAR 有权转让
标题翻译：飞机起落架的机械位置指示器
公开(公告)号：EP2643214A1
公开(公告)日：2013-10-02
申请号：EP11785062.8
申请日：2011-11-09
申请人： Messier-Dowty Limited
发明人： HODGKINSON, Ben , LACY, Stuart , WEBB, Chris , ANSON, Garry
IPC分类号： B64D45/00 , B64C25/00
CPC分类号： B64D45/0005 , B64C25/00 , B64D2045/008
摘要： A mechanical position indicator (9a) for providing a visual indication that a first part of an aircraft landing gear (1) has assumed a predetermined position relative to a second part, the position indicator (9a) being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element (15a) in a deployed position, the position indicator (9a) being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator (9a) from the first state to a second state in which the indicator element (15a) is displaced from the deployed position, the position indicator (9a) being arranged to inhibit the indicator element (15a) thereafter returning to the deployed position.

5. 发明公开

EP2951087A1 PITCH TRIMMER ACTUATOR WITH VARIABLE DAMPING 有权转让
标题翻译：具有可变阻尼的间距调节器执行器
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。

6. 发明公开

EP2544948A1 AIRCRAFT LANDING GEAR STOP PAD 有权转让
标题翻译： STOPPKLOTZFÜRDAS FAHRWERK EINES FLUGZEUGES
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。

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