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公开(公告)号：EP3383738B1
公开(公告)日：2019-11-20
申请号：EP16871470.7
申请日：2016-12-01
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公开(公告)号：EP3383738A1
公开(公告)日：2018-10-10
申请号：EP16871470.7
申请日：2016-12-01
摘要： According to one or more aspects, a control system for managing operational limits associated with two or more actuators includes a controller. The controller may continually monitor a first operational limit associated with a first actuator and a first operational limit associated with a second actuator. The controller may determine a first overall distributed control system operating limit based on the first operational limit associated with the first actuator, the first operational limit associated with the second actuator, and a type of operational limit associated with both operational limits.
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公开(公告)号：EP2920067B1
公开(公告)日：2018-05-30
申请号：EP13850470.9
申请日：2013-09-30
CPC分类号： B64C1/1438 , B64D11/0023
摘要： A door assembly for an aircraft includes a partition panel disposed laterally within a fuselage of the aircraft and a descender panel moveably secured to a lower end of the partition panel for selectively closing an aisle opening defined below the partition panel. The door assembly further includes a handle disposed on the partition panel that is operatively connected to the descender panel through a link mechanism such that rotation of the handle is translated into movement of the descender panel to move the descender panel between a retracted position and a deployed position.
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公开(公告)号：EP2996938A2
公开(公告)日：2016-03-23
申请号：EP14797229.3
申请日：2014-05-14
发明人： FUJINO, Michimasa , HOMMA, Yasuhiro
CPC分类号： B64C1/1484 , B64C1/1492 , B64D11/02
摘要： An aircraft includes a fuselage including a plurality of frame members disposed at predetermined intervals in a longitudinal direction of the fuselage and a plurality of stringers extending substantially linearly in the longitudinal direction. The fuselage defines an aircraft interior. A compartment is located in the interior of the fuselage. The compartment defines an interior area. A first one window assembly is mounted to an upper portion of the fuselage for introducing daylight into the interior area. The first window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers. The first window assembly includes a window pane, an inner cover and a retainer. The inner cover introduces daylight from the window pane into the interior area. The retainer secures the window pane and the inner cover to the fuselage.
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公开(公告)号：EP2994356A1
公开(公告)日：2016-03-16
申请号：EP14826438.5
申请日：2014-07-16
IPC分类号： B60T8/42
CPC分类号： B60T11/046 , B60T7/101 , B60T13/662 , B64C13/04 , B64C25/001 , B64C25/44
摘要： An aircraft emergency brake system includes a modulating emergency/parking brake valve in fluid communication with and disposed between a pressure source and a wheel brake and a lever assembly operatively connected with the brake valve. The emergency brake system is operative in first and second stages. The lever assembly includes a handle, a lock mechanism and an unlock mechanism. The handle is movable between a non-actuated position and a fully-actuated position. The brake pressure provided to the wheel brake through the brake valve depends on a position of the handle. The lock mechanism is operatively connected with the handle to obstruct the handle from moving from the first stage to the second stage. The unlock mechanism is disposed on the handle to unlock the lock mechanism allowing movement of the handle to the second stage position from the first stage position.
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6.发明公开AIRCRAFT DOOR MECHANISM WITH HANDLE ACTUATED DESCENDER 有权FLUGZEUGTÜRMECHANISMUSMIT EINER DURCH EINEN GRIFF ZUBETÄTIGENDENTREPPE
公开(公告)号：EP2920067A1
公开(公告)日：2015-09-23
申请号：EP13850470.9
申请日：2013-09-30
IPC分类号： B64C1/14
CPC分类号： B64C1/1438 , B64D11/0023
摘要： A door assembly for an aircraft includes a partition panel disposed laterally within a fuselage of the aircraft and a descender panel moveably secured to a lower end of the partition panel for selectively closing an aisle opening defined below the partition panel. The door assembly further includes a handle disposed on the partition panel that is operatively connected to the descender panel through a link mechanism such that rotation of the handle is translated into movement of the descender panel to move the descender panel between a retracted position and a deployed position.
摘要翻译： 用于飞行器的门组件包括横向设置在飞行器的机身内的分隔板和可移动地固定到分隔板的下端的下降板，用于选择性地关闭限定在分隔板下方的通道开口。 门组件还包括设置在分隔板上的手柄，其通过连杆机构可操作地连接到下降板，使得手柄的旋转被转换成下降板的运动，以使下降板在缩回位置和展开的位置之间移动 位置。
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公开(公告)号：EP2877400A1
公开(公告)日：2015-06-03
申请号：EP13823807.6
申请日：2013-07-09
发明人： GOTO, Kenichi
IPC分类号： B64D37/02
CPC分类号： B64D37/28 , Y10T137/7303
摘要： A fuel transfer system for an aircraft includes an upper tank, a lower tank, a fuel transfer line connecting the upper tank to the lower tank, an upper fuel transfer line outlet in the lower tank, a lower fuel transfer line outlet in the lower tank, an upper float valve associated with the upper fuel transfer line outlet, and a lower float valve associated with the lower fuel transfer line outlet. The upper fuel transfer line outlet, which is in the lower tank, is in fluid communication with the upper tank. The lower fuel transfer line outlet, which is located in the lower tank, is in fluid communication with the upper tank.
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公开(公告)号：EP2259966B1
公开(公告)日：2012-09-12
申请号：EP09727634.9
申请日：2009-03-31
发明人： OYAMA, Hiroki
IPC分类号： B64C9/32
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公开(公告)号：EP3383741A1
公开(公告)日：2018-10-10
申请号：EP16871462.4
申请日：2016-12-01
IPC分类号： B64D31/10
CPC分类号： B64D31/10 , B64C13/16 , B64C13/503 , G05D1/0808
摘要： A rudder bias system for an aircraft with a right engine and a left engine includes a component determining a left and right primary and secondary thrust estimates. The system includes a left engine thrust estimate selector determining a left selected estimate based on the left thrust estimates and a right engine thrust estimate selector determining a right selected estimate based on the right thrust estimates. The system includes an enable and mode component determining one or more corresponding validities for the thrust estimates. The system includes a control component generating an engage command based on a thrust differential between the right engine and the left engine, calculated from the left selected estimate and the right selected estimate and a torque command based on an equivalent pedal force assistance calculated as a difference between the thrust differential and an activation threshold.
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公开(公告)号：EP3003855B1
公开(公告)日：2018-07-11
申请号：EP14807595.5
申请日：2014-05-29
发明人： KONDO, Junichi
CPC分类号： B64C1/1492 , B63B19/02 , B63B2019/0038 , B64C1/1484 , B64G1/22 , B64G1/60 , F16B5/02 , F16B19/02
摘要： A fastening assembly for a window of a pressurized fuselage of an aircraft includes a fastener received through a mounting hole defined in the window, an edge attachment member fixing the window to the fuselage, and a bushing assembly embedded in the mounting hole. The bushing assembly includes an inner sleeve bushing radially interposed between the fastener and the window and an outer sleeve bushing radially interposed between the inner sleeve bushing and the window. The inner sleeve bushing is formed from relatively less rigid metal compared with metal of the fastener and the outer sleeve bushing is formed from relatively rigid metal compared with material of the window and the metal of the inner sleeve bushing.
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