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

US20170267357A1 RETRACTABLE AIR GASPER APPARATUS 审中-公开
公开(公告)号：US20170267357A1
公开(公告)日：2017-09-21
申请号：US15504710
申请日：2015-07-28
申请人： BOMBARDIER INC.
发明人： Nikolas BEAUDIN , Bruce MALEK
IPC分类号： B64D13/00
摘要： An air gasper (air) for a vehicle includes an air inlet (26), a first housing (24) disposable through a panel in the vehicle (12), the first housing (24) being connected to the air inlet (26), a second housing (70) disposed within the first housing (24), an air outlet (72) disposed within the second housing (70), downstream of the air inlet (26), and a first mechanism (102, 70) connected between the first housing (24) and the second housing (70). The first mechanism (102, 70) permits the second housing (70) to be stowed within the first housing (24) in a stowed position and also permits the second housing (70) to extend outwardly from the first housing (24) in a deployed position.

2. 发明申请

US20210237844A1 BUFFER ZONE FOR INTERIOR AIRCRAFT FEATURES 有权
公开(公告)号：US20210237844A1
公开(公告)日：2021-08-05
申请号：US17230340
申请日：2021-04-14
申请人： BOMBARDIER INC.
发明人： Bruce MALEK , Stefan HOLOWKA , Nikolas BEAUDIN
IPC分类号： B64C1/06 , B64D11/00 , B64F5/10 , B64C1/10
摘要： Several embodiments of buffer zones are provided that are contemplated to be disposed with respect to two or more adjacent elements on an aircraft. The buffer zones adjust for dynamic spacing between the elements to help control different gapping requirements between the elements installed in the aircraft. Embodiments include an aircraft interior panel configuration, an aircraft interior wall panel configuration, an adjustable width aircraft bulkhead, and an aircraft personal service unit.

3. 发明申请

US20170057639A1 AIRCRAFT ANGLED CONFERENCE TABLE CONFIGURATION 审中-公开
标题翻译：飞机安装会议台配置
公开(公告)号：US20170057639A1
公开(公告)日：2017-03-02
申请号：US15306156
申请日：2015-04-22
申请人： BOMBARDIER INC.
发明人： Seung Joon BANG , Tim Michael FAGAN , Bruce MALEK
IPC分类号： B64D11/06 , A47B13/10 , A47B13/08 , A47B37/00 , A47B5/04 , A47B9/00
CPC分类号： B64D11/0638 , A47B5/04 , A47B9/00 , A47B13/088 , A47B13/10 , A47B37/00 , A47B2200/0079
摘要： An aircraft table configuration includes a first table section and a second table section. The first and second table sections are hingedly connected along a first hinge line so that the second table section is configurable between a deployed, opened position and a folded, closed position. The first table section presents a first angled side and the second table section table presents a second angled side. The first angled side defines a first angle with respect to the first hinge line, and the second angled side defines a second angle with respect to the first hinge line. The first angled side and the second angled side are opposite to one another on either side of the first hinge line, wherein the first and second angled sides are adapted to define an aisle width in the aircraft. The aisle width does not change between the open position and the closed position.
摘要翻译：飞机台配置包括第一台部分和第二台部分。第一和第二台部分沿着第一铰链线铰接连接，使得第二工作台部分可配置在展开的打开位置和折叠的关闭位置之间。第一台部分呈现第一倾斜侧面，第二台部分台呈现第二倾斜侧面。所述第一倾斜侧面相对于所述第一铰链线限定第一角度，并且所述第二倾斜侧面相对于所述第一铰链线限定第二角度。第一成角度侧和第二倾斜侧在第一铰链线的任一侧彼此相对，其中第一和第二倾斜侧适于在飞行器中限定过道宽度。过道宽度在打开位置和关闭位置之间不变。

4. 发明申请

US20170043855A1 BUFFER ZONE FOR INTERIOR AIRCRAFT FEATURES 审中-公开
标题翻译：缓冲区内部飞机特点
公开(公告)号：US20170043855A1
公开(公告)日：2017-02-16
申请号：US15306241
申请日：2015-04-20
申请人： Bombardier Inc.
发明人： Bruce MALEK , Stefan HOLOWKA , Nikolas BEAUDIN
IPC分类号： B64C1/06 , B64D11/00 , B64C1/10
CPC分类号： B64C1/066 , B64C1/10 , B64D11/0023 , B64D2011/0046 , B64F5/10
摘要： Several embodiments of buffer zones are provided that are contemplated to be disposed with respect to two or more adjacent elements on an aircraft. The buffer zones adjust for dynamic spacing between the elements to help control different gapping requirements between the elements installed in the aircraft. Embodiments include an aircraft interior panel configuration, an aircraft interior wall panel configuration, an adjustable width aircraft bulkhead, and an aircraft personal service unit.
摘要翻译：提供缓冲区的几个实施例，其被设想为相对于飞行器上的两个或更多个相邻元件设置。缓冲区可调节元件之间的动态间距，以帮助控制安装在飞机上的元件之间的不同间隙要求。实施例包括飞行器内部面板配置，飞行器内部壁板配置，可调节宽度的飞行器舱壁和飞行器个人服务单元。

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