WO2020024336A1 - Structure de montage dans une cabine d'avion civil - Google Patents

Structure de montage dans une cabine d'avion civil Download PDF

Info

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
Authority
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)
Chinese (zh)
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/fr

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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.

Landscapes

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

Abstract

L'invention concerne une structure de montage dans une cabine d'avion civil (99), comprenant un dispositif d'alimentation électrique (31) et un ensemble de passage (88) disposé dans la cabine d'avion (99), l'ensemble de passage (88) étant pourvu d'un premier ensemble de service de passager (20), d'un second ensemble de service de passager (21) et d'un élément d'espacement (10) ; l'élément d'espacement (10) est situé entre le premier ensemble de service de passagers (20) et le second ensemble de service de passager (21) ; le dispositif d'alimentation électrique (31) est intégré dans une cavité (100) scellée par l'élément d'espacement (10) ; le premier ensemble de services de passagers (20) est pourvu sur celui-ci d'une première interface USB (53) ; et la première interface USB (53) est connectée au dispositif d'alimentation électrique (31). Le problème technique existant dans la technologie existante selon lequel l'utilisation d'un espace d'un intérieur de cabine est faible en raison des interfaces USB disposées sur deux côtés d'un siège de passager est résolu de façon à améliorer les avantages économiques.
PCT/CN2018/100862 2018-08-03 2018-08-16 Structure de montage dans une cabine d'avion civil WO2020024336A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201821247018.1 2018-08-03
CN201821247018 2018-08-03

Publications (1)

Publication Number Publication Date
WO2020024336A1 true WO2020024336A1 (fr) 2020-02-06

Family

ID=69231405

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2018/100862 WO2020024336A1 (fr) 2018-08-03 2018-08-16 Structure de montage dans une cabine d'avion civil

Country Status (1)

Country Link
WO (1) WO2020024336A1 (fr)

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系统
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 一种飞机行李架系统
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系统
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 一种飞机行李架系统
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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