WO2020024336A1 - 民用飞机客舱内的安装结构 - Google Patents

民用飞机客舱内的安装结构 Download PDF

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Publication number
WO2020024336A1
WO2020024336A1 PCT/CN2018/100862 CN2018100862W WO2020024336A1 WO 2020024336 A1 WO2020024336 A1 WO 2020024336A1 CN 2018100862 W CN2018100862 W CN 2018100862W WO 2020024336 A1 WO2020024336 A1 WO 2020024336A1
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WO
WIPO (PCT)
Prior art keywords
passenger
power supply
supply device
usb interface
passenger service
Prior art date
Application number
PCT/CN2018/100862
Other languages
English (en)
French (fr)
Inventor
李宗谕
肖�琳
Original Assignee
李宗谕
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 李宗谕 filed Critical 李宗谕
Publication of WO2020024336A1 publication Critical patent/WO2020024336A1/zh

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for

Definitions

  • the utility model belongs to the technical field of aircraft, and particularly relates to a mounting structure in a passenger cabin of a civil aircraft.
  • the main purpose of the utility model is to propose a mounting structure in the cabin of a civil aircraft, which aims to solve the technical problem of low utilization rate of the internal space of the cabin caused by the USB interface provided on both sides of the passenger seat in the prior art. To improve economic efficiency.
  • the installation structure in the cabin of a civil aircraft of the present utility model includes a power supply device and a passage assembly provided in the cabin of the aircraft.
  • the passage assembly is provided with a first passenger service module, a second passenger service module, and A partition plate between the first passenger service component and the second passenger service component, the power supply device is built into a cavity sealed by the partition plate, and a first passenger service component is provided with a first A USB interface, the first USB interface is connected to the power supply device.
  • it further comprises a wire, and the power supply device is connected to the first USB interface through the wire.
  • the first passenger service component is provided with an air-conditioning blowing structure and a call button.
  • it further comprises a storage bin for storing a traveler's backpack, and the storage bin is arranged on the aisle assembly.
  • a second USB interface is provided on the second passenger component, and the second USB interface is connected to a power supply device.
  • a power supply device is built in a space enclosed by a partition plate, and a first USB service interface is provided on a first passenger service component, so that electronic equipment required by passengers can be serviced by the first passenger.
  • the first USB interface on the module is used for power supply, and the power supply device is built in the cavity enclosed by the partition board, which does not occupy the passenger seat space, so the utilization rate of the internal space of the cabin is improved, and more passenger seats can be arranged, of which
  • the power supply device is built into the cavity enclosed by the partition plate. Maintenance personnel can complete the maintenance operation by replacing the power supply device. Compared with the traditional need to perform maintenance operations on the power supply system on the passenger seat, the maintenance is convenient and fast. Produce greater economic benefits.
  • FIG. 1 is a schematic structural diagram of a cabin of a civil aircraft of the present invention
  • FIG. 2 is a partially enlarged schematic diagram of a region B in FIG. 1;
  • FIG. 2 is a partially enlarged schematic diagram of a region B in FIG. 1;
  • FIG. 3 is a partially enlarged schematic diagram of FIG. 2;
  • FIG. 4 is a schematic structural diagram of an intermediate structure of a mounting structure in a passenger cabin of a civil aircraft of the present invention.
  • first may be referred to as a second component
  • second component may similarly be referred to as a first component.
  • the term "and / or” refers to a combination of any one or more of related items and descriptive items.
  • FIG. 1 is a schematic structural diagram of a civil aircraft cabin of the utility model
  • FIG. 2 is a partially enlarged schematic diagram of a region B in FIG. 1
  • FIG. 4 is a mounting structure of a civil aircraft cabin of the utility model. Schematic diagram of the structure of the intermediate partition.
  • the installation structure in the cabin of a civil aircraft of the present utility model includes a power supply device 31 and a passage assembly 88 provided in the cabin 99 of the aircraft.
  • the passage assembly 88 is located above a passenger seat (in the figure) (Not shown), the passenger seat is disposed in the interior space Y of the passenger cabin, and the passage component 88 is provided with a first passenger service component 20, a second passenger service component 21, and a partition plate 10, and one side of the partition plate and The first passenger service module is connected, and the other side is connected with the second passenger service module.
  • the partition board 10 is located between the first passenger service module 20 and the second passenger service module 21.
  • the power supply device 31 is built in the space.
  • the first passenger service component 20 is provided with a first USB interface 53, and the first USB interface 53 is connected to the power supply device 31.
  • the first passenger service component 20, the partition plate 10, and the second passenger service component 21 are arranged in a straight line in order, and further include a wire 32, and the power supply device 31 is connected to the first USB interface 53 through the wire 32 .
  • the utility model has the following beneficial effects: the installation structure in the passenger cabin of the civil aircraft of the utility model, the power supply device is built in the cavity enclosed by the partition plate, and the first passenger service component is provided with a first USB interface, so that passengers need Electronic equipment can be powered through the first USB interface on the first passenger service component, and the power supply device is built into the cavity enclosed by the partition board, and does not occupy the passenger seat space, thereby improving the utilization of the internal space of the passenger cabin. More passenger seats can be arranged.
  • the power supply unit is built in the space enclosed by the partition plate. Maintenance personnel can complete the maintenance operation by replacing the power supply unit. Compared with the traditional need to repair the power supply system on the passenger seat Easy operation and maintenance.
  • the first passenger service component 20 is provided with an air-conditioning blower structure 51 and a call button 52.
  • the call button is used to call a flight attendant after being pressed, and specifically, to make a preset decibel call sound; preferably, also It includes a storage bin 30 for storing a traveler's backpack, and the storage bin 30 is disposed on the aisle assembly 88.
  • a second USB interface is provided on the second passenger component, and the second USB interface is connected to a power supply device.
  • the cavity 100 includes a groove opened on the channel assembly 88.
  • the channel assembly 88 is further provided with a guide rail 33
  • the partition plate 10 is provided with a hook.
  • Structure 34 the partition plate is mounted on the guide rail 33 through the hook structure 34.
  • the connection relationship between the partition plate and the channel component is specifically limited, so that the partition plate can be removed through the hook structure.
  • 31 is placed on the inner surface of the partition board and installed on the guide rail, which is equivalent to placing the power supply unit 31 in the cavity 100, which improves the space utilization inside the cabin, so that the aircraft cabin can accommodate more passenger seats and improve It is economical and convenient for maintenance personnel to quickly maintain the power supply system.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

一种民用飞机客舱（99）内的安装结构，包括电源装置（31）和设置于飞机客舱（99）内的通道组件（88），所述通道组件（88）上设置有第一旅客服务组件（20）、第二旅客服务组件（21）和间隔板（10），所述间隔板（10）位于第一旅客服务组件（20）和第二旅客服务组件（21）之间，所述电源装置（31）内置于所述间隔板（10）所封存的空腔（100）内，所述第一旅客服务组件（20）上设置有第一USB接口（53），所述第一USB接口（53）与电源装置（31）连接。解决了现有技术中存在的，USB接口设置在乘客座椅两侧所导致的客舱内部空间利用率低的技术问题，以提高经济效益。

Description

民用飞机客舱内的安装结构 技术领域
本实用新型属于飞机技术领域，尤其涉及一种民用飞机客舱内的安装结构。
 背景技术
目前，现有的大多数民用飞机上，比如中国商飞ARJ21、波音B737系列等，其客舱内的对于乘客进行充电的USB接口大多数设置在乘客座椅组件上，这样提高了乘客座椅结构的复杂程度，这种充电***布置，属于后装改造（飞机主体结构拼接后，才进行供电***后装），这种后装存在较大的安装困难，成本较高，以至于一个客舱中只能布置更少的乘客座椅，同时，存在空间利用率低的问题，也影响民用飞机起飞一趟的载客数量，降低了经济效益。
因此，现有技术有待于改善。
 技术问题
在此处键入技术问题描述段落。
 技术解决方案
本实用新型的主要目的在于提出一种民用飞机客舱内的安装结构，旨在解决现有技术中存在的，USB接口设置在乘客座椅两侧所导致的客舱内部空间利用率低的技术问题，以提高经济效益。
为了解决上述技术问题，本实用新型的民用飞机客舱内的安装结构，包括电源装置和设置于飞机客舱内的通道组件，所述通道组件上设置有第一旅客服务组件、第二旅客服务组件和间隔板，所述间隔板位于第一旅客服务组件和第二旅客服务组件之间，所述电源装置内置于所述间隔板所封存的空腔内，所述第一旅客服务组件上设置有第一USB接口，所述第一USB接口与电源装置连接。
优选地，还包括导线，所述电源装置通过导线与第一USB接口连接。
优选地，所述第一旅客服务组件上设置有空调吹风结构和呼叫按钮。
优选地，还包括用于存放旅客随身背包的存储仓，所述存储仓设置在通道组件上。
优选地，所述第二旅客组件上设置有第二USB接口，所述第二USB接口与电源装置连接。
 有益效果
本实用新型具有以下有益效果：
本实用新型的民用飞机客舱内的安装结构，电源装置内置于间隔板所封存的空间内，第一旅客服务组件上设置有第一USB接口，使得乘客所需要的电子设备可以通过第一旅客服务组件上的第一USB接口进行供电，且电源装置内置于间隔板所封存的空腔内，没有占用到乘客座椅空间，因此提高了客舱内部空间利用率，能够布置更多乘客座椅，其中，电源装置内置于间隔版所封存的空腔中，维护人员通过更换电源装置，即可完成维护操作，相比传统的需要对于乘客座椅上的供电***进行维修操作，维护方便以及快捷，能产生较大经济效益。
 附图说明
图1为本实用新型民用飞机客舱内的结构示意图；
图2为图1中B区域的局部放大示意图；
图3为图2的局部放大示意图；
图4为本实用新型民用飞机客舱内的安装结构中间隔板的结构示意图。
本实用新型目的的实现、功能特点及优点将结合实施例，参照附图做进一步说明。本发明的最佳实施方式
在此处键入本发明的最佳实施方式描述段落。
 本发明的实施方式
应当理解，此处所描述的具体实施例仅仅用以解释本实用新型，并不用于限定本实用新型。
需要注意的是，相关术语如“第一”、“第二”等可以用于描述各种组件，但是这些术语并不限制该组件。这些术语仅用于区分一个组件和另一组件。例如，不脱离本发明的范围，第一组件可以被称为第二组件，并且第二组件类似地也可以被称为第一组件。术语“和/或”是指相关项和描述项的任何一个或多个的组合。
参考图1、图2和图4，图1为本实用新型民用飞机客舱内的结构示意图；图2为图1中B区域的局部放大示意图；图4为本实用新型民用飞机客舱内的安装结构中间隔板的结构示意图。
如图1和图2所示，本实用新型的民用飞机客舱内的安装结构，包括电源装置31和设置于飞机客舱99内的通道组件88，所述通道组件88位于乘客座椅上方（图中未示），所述乘客座椅设置于客舱内部空间Y内，所述通道组件88上设置有第一旅客服务组件20、第二旅客服务组件21和间隔板10，所述间隔板一侧与第一旅客服务组件连接，另一侧与第二旅客服务组件连接，所述间隔板10位于第一旅客服务组件20和第二旅客服务组件21之间，所述电源装置31内置于所述间隔板10所封存的空腔100内，所述第一旅客服务组件20上设置有第一USB接口53，所述第一USB接口53与电源装置31连接。具体地，所述第一旅客服务组件20、间隔板10和第二旅客服务组件21依先后顺序呈直线状排列，还包括导线32，所述电源装置31通过导线32与第一USB接口53连接。本实用新型具有以下有益效果：本实用新型的民用飞机客舱内的安装结构，电源装置内置于间隔板所封存的空腔内，第一旅客服务组件上设置有第一USB接口，使得乘客所需要的电子设备可以通过第一旅客服务组件上的第一USB接口进行供电，且电源装置内置于间隔板所封存的空腔内，没有占用到乘客座椅空间，因此提高了客舱内部空间利用率，能够布置更多乘客座椅，其中，电源装置内置于间隔版所封存的空间中，维护人员通过更换电源装置，即可完成维护操作，相比传统的需要对于乘客座椅上的供电***进行维修操作，维护方便以及快捷。
优选地，所述第一旅客服务组件20上设置有空调吹风结构51和呼叫按钮52，所述呼叫按钮用于按动后以呼叫乘务员，具体为发出预设分贝的呼叫声；优选地，还包括用于存放旅客随身背包的存储仓30，所述存储仓30设置在通道组件88上。所述第二旅客组件上设置有第二USB接口，所述第二USB接口与电源装置连接。
对于间隔板10所封存的空腔100；所述空腔100包括通道组件88上开设的凹槽，具体地，所述通道组件88上还设置有导轨33，所述间隔板10上设置有挂钩结构34，所述间隔板通过挂钩结构34安装在导轨33上，本优选实施例对于间隔板与通道组件的连接关系进行具体限定，以实现间隔版可通过挂钩结构卸下，此时将电源装置31置于间隔板内表面上，一同安装在导轨上，即相当于将电源装置31置于空腔100中，提高了客舱内部的空间利用率，使得飞机客舱能够容纳更多乘客座椅，提高经济效益，且也便于维护人员对于供电***进行快速维护。
以上仅为本实用新型的优选实施例，并非因此限制本实用新型的专利范围，凡是利用本实用新型说明书及附图内容所作的等效结构或等效流程变换，或直接或间接运用在其他相关的技术领域，均同理包括在本实用新型的专利保护范围内。
 工业实用性
在此处键入工业实用性描述段落。
 序列表自由内容
在此处键入序列表自由内容描述段落。

Claims (5)

  1. 一种民用飞机客舱内的安装结构，其特征在于，包括电源装置和设置于飞机客舱内的通道组件，所述通道组件上设置有第一旅客服务组件、第二旅客服务组件和间隔板，所述间隔板位于第一旅客服务组件和第二旅客服务组件之间，所述电源装置内置于所述间隔板所封存的空腔内，所述第一旅客服务组件上设置有第一USB接口，所述第一USB接口与电源装置连接。
  2. 如权利要求1所述民用飞机客舱内的安装结构，其特征在于，还包括导线，所述电源装置通过导线与第一USB接口连接。
  3. 如权利要求1所述民用飞机客舱内的安装结构，其特征在于，所述第一旅客服务组件上设置有空调吹风结构和呼叫按钮。
  4. 如权利要求1所述民用飞机客舱内的安装结构，其特征在于，还包括用于存放旅客随身背包的存储仓，所述存储仓设置在通道组件上。
  5. 如权利要求1所述民用飞机客舱内的安装结构，其特征在于，所述第二旅客组件上设置有第二USB接口，所述第二USB接口与电源装置连接。
     
PCT/CN2018/100862 2018-08-03 2018-08-16 民用飞机客舱内的安装结构 WO2020024336A1 (zh)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101687548A (zh) * 2007-06-29 2010-03-31 空中客车营运有限公司 用于飞行器客舱的模块化衣帽架
US20150097082A1 (en) * 2013-10-04 2015-04-09 Embraer S.A. Modular passenger service units and assemblies thereof
CN104648675A (zh) * 2013-11-21 2015-05-27 空中客车德国运营有限责任公司 用于灵活的乘客供给单元的空气传输***
CN105173088A (zh) * 2014-06-04 2015-12-23 波音公司 简化乘客服务单元测试器
CN206900664U (zh) * 2017-05-26 2018-01-19 中国民航大学 一种飞机行李架***
CN109319124A (zh) * 2018-08-03 2019-02-12 李宗谕 民用飞机客舱内供电方法

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101687548A (zh) * 2007-06-29 2010-03-31 空中客车营运有限公司 用于飞行器客舱的模块化衣帽架
US20150097082A1 (en) * 2013-10-04 2015-04-09 Embraer S.A. Modular passenger service units and assemblies thereof
CN104648675A (zh) * 2013-11-21 2015-05-27 空中客车德国运营有限责任公司 用于灵活的乘客供给单元的空气传输***
CN105173088A (zh) * 2014-06-04 2015-12-23 波音公司 简化乘客服务单元测试器
CN206900664U (zh) * 2017-05-26 2018-01-19 中国民航大学 一种飞机行李架***
CN109319124A (zh) * 2018-08-03 2019-02-12 李宗谕 民用飞机客舱内供电方法

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