专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2014184627A1 EXIT ROW TABLE FOR AN AIRCRAFT 审中-公开
公开(公告)号：WO2014184627A1
公开(公告)日：2014-11-20
申请号：PCT/IB2014/000637
申请日：2014-04-29
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： GAGNON, Pierre , ROY, Jordan , DEKA, Tom , MAGEAU, Christian , MONARDO, Michele , HUBER, Stefan , HASELBERGER, Christoph
IPC分类号： B64D11/06
CPC分类号： B64D11/0638 , B64D11/06 , B64D11/0605
摘要： A table (30) for an aircraft includes a table surface (56) deployable between a retracted position and a deployed position, an arm (50) having a first end and a second end, the arm (50) supporting the table (66) surface at the first end, a support connected to the arm (50) at the second end, the support connecting the arm to a structure interior to the aircraft, a sensor (136) within the aircraft to detect if a seat adjacent to the table surface is occupied, and a mechanism (120) for retracting the table surface to the retracted position if the sensor (136) detects at least one of that the seat is not occupied and that the aircraft flight mode meets predetermined criteria.
摘要翻译：一种用于飞行器的工作台（30）包括可在缩回位置和展开位置之间展开的台面（56），具有第一端和第二端的臂（50），支撑台（66）的臂（50）在第一端处的表面，在第二端处连接到臂（50）的支撑件，支撑件将臂连接到飞行器内部的结构，飞行器内的传感器（136），以检测邻近桌子的座椅如果所述传感器（136）检测到所述座椅未被占用和所述飞行器飞行模式满足预定标准中的至少一个，则将所述台面缩回到所述缩回位置的机构（120）。

2. 发明公开

EP2996940A1 EXIT ROW TABLE FOR AN AIRCRAFT 审中-公开
标题翻译： NOTAUSGANGSREIHENTISCHFÜREIN FLUGZEUG
公开(公告)号：EP2996940A1
公开(公告)日：2016-03-23
申请号：EP14726008.7
申请日：2014-04-29
申请人： Bombardier Inc. , Short Brothers Plc
发明人： GAGNON, Pierre , ROY, Jordan , DEKA, Tom , MAGEAU, Christian , MONARDO, Michele , HUBER, Stefan , HASELBERGER, Christoph
IPC分类号： B64D11/06
摘要： A table (30) for an aircraft includes a table surface (56) deployable between a retracted position and a deployed position, an arm (50) having a first end and a second end, the arm (50) supporting the table (66) surface at the first end, a support connected to the arm (50) at the second end, the support connecting the arm to a structure interior to the aircraft, a sensor (136) within the aircraft to detect if a seat adjacent to the table surface is occupied, and a mechanism (120) for retracting the table surface to the retracted position if the sensor (136) detects at least one of that the seat is not occupied and that the aircraft flight mode meets predetermined criteria.
摘要翻译：一种用于飞行器的工作台（30）包括可在缩回位置和展开位置之间展开的台面（56），具有第一端和第二端的臂（50），支撑台（66）的臂（50）在第一端处的表面，在第二端处连接到臂（50）的支撑件，支撑件将臂连接到飞行器内部的结构，飞行器内的传感器（136），以检测邻近桌子的座椅如果所述传感器（136）检测到所述座椅未被占用和所述飞行器飞行模式满足预定标准中的至少一个，则将所述台面缩回到所述缩回位置的机构（120）。

3. 发明授权

EP2996940B1 EXIT ROW TABLE FOR AN AIRCRAFT 有权
公开(公告)号：EP2996940B1
公开(公告)日：2020-09-16
申请号：EP14726008.7
申请日：2014-04-29
申请人： Bombardier Inc. , Short Brothers Plc
发明人： GAGNON, Pierre , ROY, Jordan , DEKA, Tom , MAGEAU, Christian , MONARDO, Michele , HUBER, Stefan , HASELBERGER, Christoph
IPC分类号： B64D11/06

4. 发明申请

WO2014051638A1 AIRCRAFT SIDEBOARD 审中-公开
标题翻译：飞机侧栏
公开(公告)号：WO2014051638A1
公开(公告)日：2014-04-03
申请号：PCT/US2012/059188
申请日：2012-10-08
申请人： BOMBARDIER INC. , LEARJET INC. , GAGNON, Pierre , DEKA, Tom , FAHMY, Patrick , MONARDO, Michele
发明人： GAGNON, Pierre , DEKA, Tom , FAHMY, Patrick , MONARDO, Michele
IPC分类号： B64D11/00 , B64D11/06
CPC分类号： B64D11/0638 , B64D11/0007 , B64D11/0015 , B64D11/0604 , B64D11/0624 , B64D11/0636
摘要： An aircraft sideboard (10) includes a first portion (26) with a first top surface (32) and a first panel (62). The first top surface (32) is disposed substantially horizontally at a first height and the first panel (62) is disposed substantially vertically adjacent to the first top surface (32). A second portion (28) is disposed adjacent to the first portion (26) at a first end of the first portion. The second portion (28) includes a second top surface (34) and a second panel (64). The second top surface (34) is disposed substantially horizontally at a second height and the second panel (64) is disposed substantially vertically adjacent to the second top surface (43). A table (76) is stowed interiorly to the first portion (26). The table (76) extends from the first portion when deployed. The first top surface (32) is immovable. The table (76) deploys by tilting the first panel (62) along a pivot axis defined adjacent to a bottom end thereof. The first height is greater than the second height.
摘要翻译：飞机侧板（10）包括具有第一顶表面（32）和第一面板（62）的第一部分（26）。第一顶表面（32）基本上水平地设置在第一高度处，并且第一面板（62）基本上垂直地布置成与第一顶表面（32）相邻。第二部分（28）在第一部分的第一端处邻近第一部分（26）设置。第二部分（28）包括第二顶表面（34）和第二面板（64）。第二顶表面（34）基本上水平地设置在第二高度处，并且第二面板（64）基本上垂直地布置成与第二顶表面（43）相邻。桌子（76）内部收纳在第一部分（26）上。当展开时，桌子（76）从第一部分延伸。第一顶面（32）是不可移动的。桌子（76）通过沿着与其底端相邻限定的枢转轴线倾斜第一面板（62）来部署。第一个高度大于第二个高度。

5. 发明公开

EP2900552A1 AIRCRAFT SIDEBOARD 有权
标题翻译： FLUGZEUG-ABLAGESCHRANK
公开(公告)号：EP2900552A1
公开(公告)日：2015-08-05
申请号：EP12780963.0
申请日：2012-10-08
申请人： Bombardier Inc. , Learjet Inc.
发明人： GAGNON, Pierre , DEKA, Tom , FAHMY, Patrick , MONARDO, Michele
IPC分类号： B64D11/00 , B64D11/06
CPC分类号： B64D11/0638 , B64D11/0007 , B64D11/0015 , B64D11/0604 , B64D11/0624 , B64D11/0636
摘要： An aircraft sideboard includes a first portion with a first top surface and a first panel. The first top surface is disposed substantially horizontally at a first height and the first panel is disposed substantially vertically adjacent to the first top surface. A second portion is disposed adjacent to the first portion at a first end of the first portion. The second portion includes a second top surface and a second panel. The second top surface is disposed substantially horizontally at a second height and the second panel is disposed substantially vertically adjacent to the second top surface. A table is stowed interiorly to the first portion. The table extends from the first portion when deployed. The first top surface is immovable. The table deploys by tilting the first panel along a pivot axis defined adjacent to a bottom end thereof. The first height is greater than the second height.
摘要翻译：飞机侧板包括具有第一顶表面和第一面板的第一部分。第一顶表面基本上水平设置在第一高度处，并且第一面板基本上垂直地布置成与第一顶表面相邻。第二部分在第一部分的第一端处邻近第一部分设置。第二部分包括第二顶表面和第二面板。第二顶表面基本上水平地设置在第二高度处，并且第二面板基本上垂直地设置成与第二顶表面相邻。一个桌子在内部被收存在第一部分。部署时，表从第一部分延伸。第一个顶面是不可移动的。桌子通过沿着与其底端相邻限定的枢转轴线倾斜第一面板来展开。第一个高度大于第二个高度。

6. 发明授权

EP2900552B1 AIRCRAFT SIDEBOARD 有权
标题翻译：飞机侧板
公开(公告)号：EP2900552B1
公开(公告)日：2017-07-19
申请号：EP12780963.0
申请日：2012-10-08
申请人： Bombardier Inc. , Learjet Inc.
发明人： GAGNON, Pierre , DEKA, Tom , FAHMY, Patrick , MONARDO, Michele
IPC分类号： B64D11/00 , B64D11/06
CPC分类号： B64D11/0638 , B64D11/0007 , B64D11/0015 , B64D11/0604 , B64D11/0624 , B64D11/0636
摘要： An aircraft sideboard includes a first portion with a first top surface and a first panel. The first top surface is disposed substantially horizontally at a first height and the first panel is disposed substantially vertically adjacent to the first top surface. A second portion is disposed adjacent to the first portion at a first end of the first portion. The second portion includes a second top surface and a second panel. The second top surface is disposed substantially horizontally at a second height and the second panel is disposed substantially vertically adjacent to the second top surface. A table is stowed interiorly to the first portion. The table extends from the first portion when deployed. The first top surface is immovable. The table deploys by tilting the first panel along a pivot axis defined adjacent to a bottom end thereof. The first height is greater than the second height.
摘要翻译：飞机餐具柜包括具有第一顶面和第一面板的第一部分。第一顶部表面基本水平地设置在第一高度处，并且第一面板基本垂直设置在第一顶部表面附近。第二部分在第一部分的第一端处邻近第一部分布置。第二部分包括第二顶面和第二面板。第二顶面基本水平地设置在第二高度处，并且第二面板基本垂直设置在第二顶面附近。一张桌子被收藏在第一部分的内部。桌子在展开时从第一部分延伸。第一个顶面是不动的。通过沿着邻近其底端限定的枢转轴线倾斜第一面板来展开桌子。第一个高度大于第二个高度。

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