AIRFLOW DIVERTER FOR AIRCRAFT AND METHOD OF USE

    公开(公告)号:US20240083585A1

    公开(公告)日:2024-03-14

    申请号:US18515251

    申请日:2023-11-20

    CPC classification number: B64D13/06 F24F13/065 B64D2013/003

    Abstract: Disclosed is a stowable airflow diverter for removable attachment to a floor vent of a turbine aircraft. The air diverter comprises vertical ducting extending from a base. A flexible gasket and magnets are attached to the base for engagement with the floor vent. A nozzle attached to the vertical ducting redirects the airflow emanating from the floor vent from horizontal to vertical in order to direct air conditioned air into the cock pit of the aircraft. In an alternate embodiment, the nozzle is rotatable with respect to the vertical axis of the duct. In another alternate embodiment, the nozzle and vertical duct comprise telescoping segments such that the device can be collapsed into the floor vent.

    Air Treatment Module
    2.
    发明申请

    公开(公告)号:US20170283075A1

    公开(公告)日:2017-10-05

    申请号:US15478790

    申请日:2017-04-04

    Abstract: In an illustrative embodiment, an apparatus for treating air discharged to a passenger suite of an aircraft includes an enclosure that houses components for treating air passing through the enclosure and a detachable cover connected to the enclosure that provides access to the components. Air treatment components associated with air treatment flow paths within the enclosure include a blower with a fan that draws air through an air intake on the enclosure. An air duct is affixed to a discharge of the blower and directs the air discharged from the blower through an air treatment flow path that includes a scented cartridge with a scented medium that is absorbed into the air passing through the air duct. An air exhaust port is attached at a discharge end of the air duct that discharges the air conditioned by the scented cartridge through an air exhaust vent on the enclosure.

    Passenger service unit and related systems
    3.
    发明授权
    Passenger service unit and related systems 有权
    乘客服务单位及相关制度

    公开(公告)号:US09487296B2

    公开(公告)日:2016-11-08

    申请号:US14464893

    申请日:2014-08-21

    Abstract: A passenger service unit (PSU) for a transport vessel has a unitary chassis with a plurality of apertures extending therethrough. Each one of the apertures is independently sized to receive at least one of a plurality of different modules. Each one of the modules includes one or more PSU fixtures having components different from other ones of the plurality of modules. A representative vessel is a passenger aircraft. Representative modules include vent and passenger reading light module, speaker module, passenger oxygen supply module and display module.

    Abstract translation: 用于运输船的乘客服务单元(PSU)具有单个底盘,其具有延伸穿过其中的多个孔。 孔中的每一个独立地大小以便接收多个不同模块中的至少一个。 每个模块包括具有与多个模块中的其它模块不同的组件的一个或多个PSU固定装置。 代表船是客机。 代表性模块包括通风和乘客阅读灯模块,扬声器模块,乘客氧气供应模块和显示模块。

    SPLIT VENTILATION SYSTEM
    4.
    发明申请
    SPLIT VENTILATION SYSTEM 审中-公开
    分体通风系统

    公开(公告)号:US20160046380A1

    公开(公告)日:2016-02-18

    申请号:US14457178

    申请日:2014-08-12

    CPC classification number: B64D13/02 B64D11/02 B64D11/04 B64D13/00 B64D2013/003

    Abstract: A ventilation system, aircraft, and method. The ventilation system includes a first conduit in fluid communication with a first air source in the aircraft to direct a fluid flow from the first air source. The ventilation system also includes a first branch in fluid communication with the first conduit and a first outflow point, the first branch including an active air mover to move the fluid flow toward the first outflow point. The ventilation system further includes a second branch that is separate from the first branch and in fluid communication with the first conduit and a second outflow point, the second branch including a passive air mover to move the fluid flow to toward the second outflow point.

    Abstract translation: 通风系统,飞机和方法。 通风系统包括与飞行器中的第一空气源流体连通以引导来自第一空气源的流体流的第一导管。 所述通风系统还包括与所述第一管道流体连通的第一分支和第一流出点,所述第一分支包括主动式空气推动器,以将流体流动朝向所述第一流出点移动。 所述通风系统还包括与所述第一分支分离并与所述第一管道流体连通的第二分支和第二流出点,所述第二分支包括被动式空气推动器,以将所述流体流动移向所述第二流出点。

    REMOTE CONTROLLED AIR NOZZLES AND METHODS OF ASSEMBLING THE SAME
    6.
    发明申请
    REMOTE CONTROLLED AIR NOZZLES AND METHODS OF ASSEMBLING THE SAME 审中-公开
    远程控制空气喷嘴及其组装方法

    公开(公告)号:US20150210397A1

    公开(公告)日:2015-07-30

    申请号:US14166249

    申请日:2014-01-28

    CPC classification number: B64D13/00 B64D2013/003 Y10T29/49826

    Abstract: An aircraft includes a plurality of seats and an input device coupled to each of the plurality of seats. The aircraft also includes a remotely controlled nozzle positioned proximate each seat of the plurality of seats. Each nozzle includes an actuator assembly including at least one actuator and an actuator shaft. The at least one actuator is configured to move the actuator shaft between an open position and a closed position to control an airflow through the nozzle in response to a signal received from a respective input device of the input devices, wherein the signal represents a position of the actuator shaft.

    Abstract translation: 一种飞行器包括多个座和耦合到多个座中的每一个的输入装置。 飞机还包括位于多个座椅的每个座位附近的远程控制的喷嘴。 每个喷嘴包括致动器组件,其包括至少一个致动器和致动器轴。 所述至少一个致动器构造成在所述致动器轴在打开位置和关闭位置之间移动以响应于从所述输入装置的相应输入装置接收到的信号来控制通过所述喷嘴的气流,其中所述信号表示 执行器轴。

    Diversion directional nozzle
    7.
    发明授权
    Diversion directional nozzle 有权
    转向定向喷嘴

    公开(公告)号:US09011216B1

    公开(公告)日:2015-04-21

    申请号:US12477100

    申请日:2009-06-02

    CPC classification number: B64D13/00 B64D2013/003

    Abstract: An elongated nozzle for distributing airflow in varying directions may include at least one set of channels. Each set may include a plurality of groups of channels. Each set may further include spaced-apart opposed dividers extending lengthwise along an elongated length of the nozzle, and spaced-apart channel side-walls extending between the spaced-apart opposed dividers. The opposed dividers and the spaced-apart channel side-walls may form the channels of each set. At least one of the spaced-apart opposed dividers of each set may be oriented at a first angle which is non-parallel to an imaginary vertical plane extending along the elongated length of the nozzle. Within each set, the spaced-apart channel side-walls of each group of channels may be oriented at different second angles, relative to an imaginary vertical plane extending along a width of the nozzle, than the spaced-apart channel side-walls of other groups of channels.

    Abstract translation: 用于在不同方向上分配气流的细长喷嘴可以包括至少一组通道。 每组可以包括多组通道组。 每个组件还可以包括沿着喷嘴的细长长度方向延伸的间隔开的相对的分隔件,以及在间隔开的相对分隔件之间延伸的间隔开的通道侧壁。 相对的分隔件和间隔开的通道侧壁可以形成每组的通道。 每组的间隔开的相对分隔件中的至少一个可以以不同于沿着喷嘴的细长长度延伸的假想垂直平面的第一角度定向。 在每组中,每组通道的间隔开的通道侧壁可以相对于沿着喷嘴的宽度延伸的假想垂直平面相对于其它的间隔开的通道侧壁以不同的第二角度定向 频道组。

Patent Agency Ranking