WO2020024335A1 - 民用飞机客舱内供电方法 - Google Patents
民用飞机客舱内供电方法 Download PDFInfo
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- WO2020024335A1 WO2020024335A1 PCT/CN2018/100861 CN2018100861W WO2020024335A1 WO 2020024335 A1 WO2020024335 A1 WO 2020024335A1 CN 2018100861 W CN2018100861 W CN 2018100861W WO 2020024335 A1 WO2020024335 A1 WO 2020024335A1
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- Prior art keywords
- power supply
- passenger
- charging interface
- electronic device
- supply device
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- 238000000034 method Methods 0.000 title claims abstract description 36
- 238000005192 partition Methods 0.000 claims description 23
- 230000000630 rising effect Effects 0.000 claims description 4
- 238000012423 maintenance Methods 0.000 abstract description 7
- 125000006850 spacer group Chemical group 0.000 abstract 2
- 238000010586 diagram Methods 0.000 description 8
- 238000001514 detection method Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
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- 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
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- H02J7/0027—
Definitions
- the invention belongs to the technical field of aircraft, and in particular relates to a power supply method in a passenger cabin of a civil aircraft. Background technique
- USB ports in the cabin for charging passengers are set on the passenger seat components, that is, passenger electronic equipment can pass
- the USB interface on the passenger seat assembly can be charged, which is very convenient, but in fact, in order to achieve this convenient charging method, many cables need to be arranged inside each passenger seat, and many cables have to be eventually Converged to a power supply switchboard, this power switchboard is generally not installed in the cabin of the aircraft in order to facilitate management and maintenance, and these numerous cables obviously increase the complexity of the internal structure of the aircraft, that is, most of the existing implementations on civil aircraft
- the power supply method increases the complexity of the internal structure of the aircraft and is also not conducive to maintenance. In this way, when there is a problem with the power supply switchboard or cables, the stability of the power supply will be affected.
- the main purpose of the present invention is to propose a power supply method in the cabin of a civil aircraft, which aims to solve the existing technical problems.
- Most power supply methods improve the technical problem of reducing the stability of power supply caused by the complexity of the internal structure of the aircraft. Conducive to maintenance.
- the method for power supply in a civil aircraft cabin of the present invention includes the following steps:
- step S10 the electronic device is connected to the charging interface through a connection cable, and the voltage output by the power supply device is transmitted to the charging interface through a wire to realize power supply for the electronic device.
- the power supply device is disposed in an internal cavity sealed by the partition plate
- the charging interface is located on a first passenger service component, and the first passenger service component and the partition plate are both disposed on a passenger passage.
- the charging interface includes a USB interface and a Lightning interface.
- the method includes the steps before the step S10:
- step S1 the power supply device detects whether the charging interface generates a rising edge voltage pulse signal, and if so, executes step S10.
- the step S10 includes steps:
- Step S11 the electronic device is connected to the charging interface through a connection line;
- step S12 the power supply device obtains the first identification identification number stored on the electronic device; and determines whether the first identification identification number is the same as the stored second standard identification number, and if so, executes step S13;
- step S13 the voltage output by the power supply device is transmitted to the charging interface through a wire, so as to charge the electronic device.
- step S14 if the first identification identification number is different from the stored second standard identification number, an alarm prompt is performed.
- the voltage output by the power supply device is then transmitted to the charging interface via the wire to achieve power supply to the electronic equipment; compared with the traditional The power supply method (power supply provided by the USB interface on both sides of the passenger seat) is different.
- the key to the power supply method provided by the present invention is that the power supply device is disposed in the internal cavity sealed by the partition plate, and the charging interface is located in the first passenger.
- the first passenger service component and the partition board are both arranged on the passenger passage, that is, the source of electricity (the power supply device is located above the passenger seat) of the power supply method is very close to the passenger, and there are not many cables Structure (the power supply unit is connected to the USB interface through a wire).
- this power supply method such as power failure, maintenance personnel can directly repair or replace the power supply unit in the internal cavity, it is easy to maintain, The stability of power supply has an impact and can produce greater economic benefits.
- FIG. 1 is a schematic flowchart of a first embodiment of a power supply method in a passenger cabin of a civil aircraft according to the present invention
- FIG. 2 is a schematic flowchart of a second embodiment of a power supply method in a passenger cabin of a civil aircraft according to the present invention
- step S10 in the first embodiment of the power supply method in the cabin of a civil aircraft according to the present invention
- FIG. 4 is a schematic flowchart of a third embodiment of a power supply method in a passenger cabin of a civil aircraft according to the present invention.
- FIG. 5 is a schematic structural diagram of an aircraft cabin
- FIG. 6 is a partially enlarged schematic diagram of a region B in FIG. 1;
- FIG. 7 is a partially enlarged schematic diagram of FIG. 2;
- FIG. 8 is a schematic structural diagram of a partition plate according to the present invention.
- FIG. 9 is a schematic structural diagram of a power supply device according to 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 flowchart of a first embodiment of a power supply method in a civil aircraft cabin of the present invention
- FIG. 5 is a schematic structural diagram of a civil aircraft cabin in the present invention
- FIG. 7 is a partially enlarged schematic diagram of FIG. 2.
- the power supply method in a passenger cabin of a civil aircraft of the present invention includes the following steps:
- step S10 the electronic device is connected to the charging interface 53 through a connection cable, and the voltage output by the power supply device 31 is transmitted to the charging interface 53 through the wire 32 to implement power supply for the electronic device.
- the charging interface 53 is located on the first passenger service component 20, and the first passenger service component 20 and the partition plate 10 are both disposed on the passenger passage 88.
- the invention has the following beneficial effects: After the civil aircraft cabin power supply method of the invention, after the passenger's electronic equipment can be connected to the charging interface through a connection cable, the voltage output by the power supply device is transmitted to the charging interface via the wire to achieve The power supply of electronic equipment is different from the traditional power supply method (power supply with USB interface provided on both sides of the passenger seat).
- the key of the power supply method provided by the present invention is that the power supply device is disposed in the internal cavity sealed by the partition plate.
- the charging interface is located on the first passenger service component, and the first passenger service component and the partition plate are both arranged on the passenger channel, that is, the source of electricity of the power supply method is very close to the passenger, and there are no numerous cable structures.
- This power supply method for example, when the power supply is abnormal, the maintenance personnel can directly repair or replace the power supply device in the internal cavity, which is easy to maintain and does not affect the stability of the power supply.
- the charging interface includes a USB interface and a Lightning interface to adapt to Android phones and Apple phones.
- the power supply device includes a controller 202, a lithium battery 203, a storage module 204, and a detection module 201. The lithium battery, the storage module, and the detection module are all connected to the controller.
- the method includes the following steps:
- step S1 the power supply device detects whether the charging interface generates a rising edge voltage pulse signal, and if so, executes step S10.
- the detection module 201 of the power supply device performs signal detection on the charging interface 53 by detecting whether a rising edge voltage pulse signal is generated on the charging interface. If it is generated, it indicates that the charging interface and the passenger's electronic device have been successfully connected. Go to step S10.
- step S10 includes the following steps:
- Step S11 the electronic device is connected to the charging interface through a connection line;
- step S12 the power supply device obtains the first identification identification number stored on the electronic device; and determines whether the first identification identification number is the same as the stored second standard identification number, and if so, executes step S13;
- step S13 the voltage output by the power supply device is transmitted to the charging interface through a wire, so as to charge the electronic device.
- the storage module 204 of the power supply device stores a second standard identification number in advance, such as an E-17 seat. Then, the second standard identification number in the power supply device above the E-17 seat is E-17;
- the first identification number includes user information.
- the seat number is entered by the passenger and stored in the memory of the electronic device. For example, a passenger sitting at E-17 (seat number) wants to use the charging interface 53 on the passenger service component. , Modify the user information in the electronic device to "E-17"; that is, this user information is the same as the second standard identification number stored in the power supply unit on the E-17 seat, so that charging can be achieved and the aircraft cabin can be avoided.
- the problem that the power supply device is misused and stolen in order to improve certain security.
- the method further includes a step: Step S14, if the first identification identification number is different from the stored second standard identification number, an alarm prompt is performed. Set based on step S14 to play a prompting role.
- the power supply device 31 is disposed in the internal cavity 100 enclosed by the partition plate 10, and the charging interface 53 is located on the first passenger service component 20.
- the first passenger service component 20 and the partition board 10 are both disposed on a passenger passage 88, which is located in the internal space Y of the passenger aircraft cabin 99; specifically, the first passenger service is provided on the passenger passage 88 Module 20, second passenger service module 21, and partition board 10, one side of the partition board is connected to the first passenger service module, and the other side is connected to the second passenger service module, and the partition board 10 is located in the first passenger service module Between the second passenger service module 20 and the second passenger service module 21, the power supply device 31 is built in the internal cavity 100 sealed by the partition plate 10.
- the first passenger service module 20 is provided with a charging interface 53 for charging.
- the 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 lead 32, and the power supply device 31 is connected to the charging interface 53 through the lead 32.
- 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 passenger passage 88.
- the internal cavity 100 includes a groove opened in the passenger passage 88.
- the passenger passage 88 is further provided with a guide rail 33
- the partition plate 10 is provided with There is a hook structure 34, and 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 to realize that the partition plate can be removed through the hook structure.
- the power supply device 31 is placed on the inner surface of the partition plate and installed on the guide rail, which is equivalent to placing the power supply device 31 in the internal cavity 100, which improves the space utilization efficiency in the cabin and enables the aircraft cabin to accommodate more passenger seats. Chair, improve economic efficiency, and also facilitate maintenance personnel to quickly maintain the power supply system.
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
一种民用飞机客舱内供电方法，包括以下步骤：步骤S10，电子设备通过连接线与充电接口（53）连接，电源装置（31）所输出的电压经过导线（32）传输至充电接口（53），以实现对电子设备供电，其中，所述电源装置（31）设置于间隔板（10）所封存的内部空腔（100）中，所述充电接口（53）位于第一旅客服务组件（20）上，所述第一旅客服务组件（20）和间隔板（10）均设置在旅客通道（88）上。其解决了现有技术中存在的大多数供电方法提高了飞机内部结构复杂程度所导致的降低供电稳定性且不利于维护的技术问题。
Description
本发明属于飞机技术领域，尤其涉及一种民用飞机客舱内供电方法。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，即乘客的电子设备可以通过乘客座椅组件上的USB接口就能实现充电，非常方便，但实际上，为了实现这种使用方便的充电方法，需要在每个乘客座椅内部布置很多线缆，众多线缆还得最终都汇聚到一个供电总机，这个供电总机为了便于管理和维护，一般不会设置在飞机客舱内，且这些众多线缆显然提高了飞机内部结构复杂程度，即现有大多数在民用飞机上所实现的供电方法提高了飞机内部结构复杂程度，且也不利于维护，这样当供电总机或者电缆出现问题，会影响供电的稳定性。
因此，现有技术有待于改善。
在此处键入技术问题描述段落。
本发明的主要目的在于提出一种民用飞机客舱内供电方法，旨在解决现有技术中存在的，大多数供电方法提高了飞机内部结构复杂程度所导致的降低供电稳定性的技术问题，且不利于维护。
为了解决上述技术问题，本发明的民用飞机客舱内供电方法，包括以下步骤：
步骤S10，电子设备通过连接线与充电接口连接，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备供电，其中，所述电源装置设置于间隔板所封存的内部空腔中，所述充电接口位于第一旅客服务组件上，所述第一旅客服务组件和间隔板均设置在旅客通道上。
优选地，所述充电接口包括USB接口和Lightning接口。
优选地，在所述步骤S10之前包括步骤：
步骤S1，电源装置检测充电接口是否产生上升沿电压脉冲信号，若是，则执行步骤S10。
优选地，所述步骤S10包括步骤：
步骤S11，电子设备通过连接线与充电接口连接；
步骤S12，电源装置获取电子设备上所存储的第一识别标识编号；并判断所述第一识别标识编号与所存储的第二标准标识编号是否相同，若是，则执行步骤S13；
步骤S13，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备进行充电。
优选地，还包括步骤：
步骤S14，若所述第一识别标识编号与所存储的第二标准标识编号不同，则进行警报提示。
本发明具有以下有益效果：
本发明的民用飞机客舱内供电方法，乘客的电子设备可以通过连接线与充电接口进行连接后，然后，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备供电；与传统的供电方式（USB接口设置在乘客座椅两侧的供电）不同，本发明所提供的供电方法，关键在于，电源装置设置于间隔板所封存的内部空腔中，所述充电接口位于第一旅客服务组件上，所述第一旅客服务组件和间隔板均设置在旅客通道上，即本供电方法的电的来源（电源装置就位于乘客座椅上方）就非常接近乘客，且又没有众多线缆结构（电源装置通过导线连接至USB接口），当这种供电方法，比如供电失常时，维护人员直接对于内部空腔中的电源装置进行维修或者更换即可，是容易进行维护的，不会对于供电稳定性产生影响，能够产生较大经济效益。
图1为本发明民用飞机客舱内供电方法的第一实施例的流程示意图；
图2为本发明民用飞机客舱内供电方法的第二实施例的流程示意图；
图3为本发明民用飞机客舱内供电方法的第一实施例中步骤S10的细化流程示意图；
图4为本发明民用飞机客舱内供电方法的第三实施例的流程示意图；
图5为飞机客舱内的结构示意图；
图6为图1中B区域的局部放大示意图；
图7为图2的局部放大示意图；
图8为本发明间隔板的结构示意图；
图9为本发明电源装置的结构示意图。
本发明目的的实现、功能特点及优点将结合实施例，参照附图做进一步说明。
在此处键入本发明的最佳实施方式描述段落。
应当理解，此处所描述的具体实施例仅仅用以解释本发明，并不用于限定本发明。
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5、图6和图7，图1为本发明民用飞机客舱内供电方法的第一实施例的流程示意图，图5为本发明民用飞机客舱内的结构示意图；图6为图1中B区域的局部放大示意图；图7为图2的局部放大示意图。
本发明的民用飞机客舱内供电方法，包括以下步骤：
步骤S10，电子设备通过连接线与充电接口53连接，电源装置31所输出的电压经过导线32传输至充电接口53，以实现对于电子设备供电，其中，所述电源装置31设置于间隔板10所封存的内部空腔100中，所述充电接口53位于第一旅客服务组件20上，所述第一旅客服务组件20和间隔板10均设置在旅客通道88上。本发明具有以下有益效果：本发明的民用飞机客舱内供电方法，乘客的电子设备可以通过连接线与充电接口进行连接后，然后，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备供电；与传统的供电方式（USB接口设置在乘客座椅两侧的供电）不同，本发明所提供的供电方法，关键在于，电源装置设置于间隔板所封存的内部空腔中，所述充电接口位于第一旅客服务组件上，所述第一旅客服务组件和间隔板均设置在旅客通道上，即本供电方法的电的来源就非常接近乘客，且又没有众多线缆结构，当这种供电方法，比如供电失常时，维护人员直接对于内部空腔中的电源装置进行维修或者更换即可，是容易进行维护的，不会对于供电稳定性产生影响。所述充电接口包括USB接口和Lightning接口，以适应安卓手机和苹果手机。如图9所示，所述电源装置包括控制器202、锂电池203、存储模块204和检测模块201，所述锂电池、存储模块和检测模块均与控制器连接。
如图2所示，优选地，在所述步骤S10之前包括步骤：
步骤S1，电源装置检测充电接口是否产生上升沿电压脉冲信号，若是，则执行步骤S10。本优选实施例中，电源装置的检测模块201对于充电接口53上进行信号检测，通过检测充电接口上是否产生上升沿电压脉冲信号，若产生，表明充电接口与乘客的电子设备已成功连接，则执行步骤S10。
如图3所示，优选地，所述步骤S10包括步骤：
步骤S11，电子设备通过连接线与充电接口连接；
步骤S12，电源装置获取电子设备上所存储的第一识别标识编号；并判断所述第一识别标识编号与所存储的第二标准标识编号是否相同，若是，则执行步骤S13；
步骤S13，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备进行充电。
所述电源装置的存储模块204预先存储有第二标准标识编号，比如E-17座位，那这个E-17座位上方的电源装置中的第二标准标识编号为E-17；所述电子设备内的第一识别标识编号包括用户信息，所述座位号是通过乘客输入并存储在电子设备的内存中，比如坐在E-17（座位号）的乘客，想使用旅客服务组件上的充电接口53，将电子设备内的用户信息修改成“E-17”；即这个用户信息就与E-17座位上电源装置所存储的第二标准标识编号相同，这样就能实现充电，避免了飞机客舱内电源装置被误用、被偷用的问题，以提高一定安全性。该实施例是利用了电子设备的用户信息，是可以根据用户输入来进行更改的优势。如图4所示，优选地，还包括步骤：步骤S14，若所述第一识别标识编号与所存储的第二标准标识编号不同，则进行警报提示。基于步骤S14设置，以起到提示作用。
其中，参考图5、图6、图7、图8，所述电源装置31设置于间隔板10所封存的内部空腔100中，所述充电接口53位于第一旅客服务组件20上，所述第一旅客服务组件20和间隔板10均设置在旅客通道88上，所述旅客通道88是位于民用飞机客舱99的内部空间Y中；具体地，所述旅客通道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所封存的内部空腔100内，所述第一旅客服务组件20上设置有充电接口53，所述充电接口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与充电接口53连接。
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设置在旅客通道88上。
对于间隔板10所封存的内部空腔100；所述内部空腔100包括旅客通道88上开设的凹槽，具体地，所述旅客通道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置于内部空腔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系统进行快速维护。
以上仅为本发明的优选实施例，并非因此限制本发明的专利范围，凡是利用本发明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，均同理包括在本发明的专利保护范围内。
在此处键入工业实用性描述段落。
在此处键入序列表自由内容描述段落。
Claims (5)
- 一种民用飞机客舱内供电方法，其特征在于，包括以下步骤：步骤S10，电子设备通过连接线与充电接口连接，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备供电，其中，所述电源装置设置于间隔板所封存的内部空腔中，所述充电接口位于第一旅客服务组件上，所述第一旅客服务组件和间隔板均设置在旅客通道上。
- 如权利要求1所述民用飞机客舱内供电方法，其特征在于，所述充电接口包括USB接口和Lightning接口。
- 如权利要求1所述民用飞机客舱内供电方法，其特征在于，在所述步骤S10之前包括步骤：步骤S1，电源装置检测充电接口是否产生上升沿电压脉冲信号，若是，则执行步骤S10。
- 如权利要求1所述民用飞机客舱内供电方法，其特征在于，所述步骤S10包括步骤：步骤S11，电子设备通过连接线与充电接口连接；步骤S12，电源装置获取电子设备上所存储的第一识别标识编号；并判断所述第一识别标识编号与所存储的第二标准标识编号是否相同，若是，则执行步骤S13；步骤S13，电源装置所输出的电压经过导线传输至充电接口，以实现对于电子设备进行充电。
- 如权利要求4所述民用飞机客舱内供电方法，其特征在于，还包括步骤：步骤S14，若所述第一识别标识编号与所存储的第二标准标识编号不同，则进行警报提示。
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