CN109319124A - Method of supplying power in civil aircraft main cabin - Google Patents
Method of supplying power in civil aircraft main cabin Download PDFInfo
- Publication number
- CN109319124A CN109319124A CN201810935899.4A CN201810935899A CN109319124A CN 109319124 A CN109319124 A CN 109319124A CN 201810935899 A CN201810935899 A CN 201810935899A CN 109319124 A CN109319124 A CN 109319124A
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- China
- Prior art keywords
- charging interface
- power supply
- supply device
- electronic equipment
- supplying power
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- Legal status (The legal status 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 status listed.)
- Pending
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- 238000000034 method Methods 0.000 title claims abstract description 30
- 230000005540 biological transmission Effects 0.000 claims abstract description 8
- 238000001514 detection method Methods 0.000 claims description 7
- 230000000630 rising effect Effects 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 12
- 230000008901 benefit Effects 0.000 description 5
- 230000005611 electricity Effects 0.000 description 5
- 238000012423 maintenance Methods 0.000 description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 238000004378 air conditioning Methods 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
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
-
- H02J7/0027—
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses method of supplying power in a kind of civil aircraft main cabin, the following steps are included: step S10, electronic equipment is connect by connecting line with charging interface, the voltage that power supply device is exported is by wire transmission to charging interface, to realize for power electronic equipment, wherein the power supply device is set in the internal cavities that spacing board is sealed up for safekeeping, the charging interface is located on the first Passenger Service Unit, and first Passenger Service Unit and spacing board are arranged on passenger route.It solves the technical issues of existing in the prior art, most of method of supplying power to improve reduction electrical stability caused by interior of aircraft complex degree of structure, and is unfavorable for safeguarding.
Description
Technical field
The invention belongs to method of supplying power in aircraft technology field more particularly to a kind of civil aircraft main cabin.
Background technique
Currently, on existing most of civil aircrafts, for example Chinese quotient flies ARJ21, Boeing B737 series etc., in main cabin
Most of the USB interface to charge for passenger be arranged on passenger seat component, i.e., the electronic equipment of passenger can lead to
The USB interface crossed on passenger seat component can be achieved with charging, very convenient, but in fact, this easy to use in order to realize
Charging method, need to arrange that many cables, numerous cables finally must all converge to a confession inside each passenger seat
Electric exchange, this power supply exchange will not be generally arranged in aircraft passenger compartment for the ease of managing and maintaining, and these numerous cables
Obviously interior of aircraft complex degree of structure is improved, i.e., existing most of method of supplying power to realized on civil aircraft improve
Interior of aircraft complex degree of structure, and be also unfavorable for safeguarding will affect power supply in this way when power supply exchange or cable go wrong
Stability.
Therefore, the prior art is to be improved.
Summary of the invention
It is a primary object of the present invention to propose method of supplying power in a kind of civil aircraft main cabin, it is intended to solve in the prior art
Existing, the technology that most of method of supplying power to improve reduction electrical stability caused by interior of aircraft complex degree of structure is asked
Topic, and be unfavorable for safeguarding.
In order to solve the above-mentioned technical problem, method of supplying power in civil aircraft main cabin of the invention, comprising the following steps:
Step S10, electronic equipment are connect by connecting line with charging interface, and the voltage that power supply device is exported passes through wire transmission
To charging interface, to realize for power electronic equipment, wherein it is empty that the power supply device is set to the inside that spacing board is sealed up for safekeeping
In chamber, the charging interface is located on the first Passenger Service Unit, and first Passenger Service Unit and spacing board are arranged at
On passenger route.
Preferably, the charging interface includes USB interface and Lightning interface.
Preferably, before the step S10 comprising steps of
Step S1, whether power supply device detection charging interface generates rising edge voltage pulse signal, if so, thening follow the steps S10.
Preferably, the step S10 comprising steps of
Step S11, electronic equipment are connect by connecting line with charging interface；
Step S12, power supply device obtain the first identification marking number stored on electronic equipment；And judge first identification
Whether identifier number and the second standard logo number stored are identical, if so, thening follow the steps S13；
Step S13, the voltage that power supply device is exported carry out electronic equipment with realizing by wire transmission to charging interface
Charging.
Preferably, it further comprises the steps of:
Step S14 carries out alarm and mentions if first identification marking number is different from the second standard logo number stored
Show.
The invention has the following advantages:
The electronic equipment of method of supplying power in civil aircraft main cabin of the invention, passenger can be carried out by connecting line and charging interface
After connection, then, the voltage that power supply device is exported supplies electronic equipment with realizing by wire transmission to charging interface
Electricity；It is different from traditional power supply mode (power supply that passenger seat two sides are arranged in USB interface), supplier of electricity provided by the present invention
Method, it is critical that power supply device is set in the internal cavities that spacing board is sealed up for safekeeping, the charging interface is located at the first passenger clothes
It is engaged on component, first Passenger Service Unit and spacing board are arranged on passenger route, i.e., the electricity of this method of supplying power to is next
With regard to very close passenger, and again, without numerous cable structures, (power supply device is logical in source (power supply device is located in above passenger seat)
Cross conducting wire and be connected to USB interface), when this method of supplying power to, such as when powering not normal, maintenance personnel is directly in internal cavities
Power supply device repair or replace, be easy to be safeguarded, electrical stability will not be had an impact, energy
Enough generate larger economic benefit.
Detailed description of the invention
Fig. 1 is the flow diagram of the first embodiment of method of supplying power in civil aircraft main cabin of the present invention；
Fig. 2 is the flow diagram of the second embodiment of method of supplying power in civil aircraft main cabin of the present invention；
The refinement flow diagram that Fig. 3 is step S10 in the first embodiment of method of supplying power in civil aircraft main cabin of the present invention；
Fig. 4 is the flow diagram of the 3rd embodiment of method of supplying power in civil aircraft main cabin of the present invention；
Fig. 5 is the structural schematic diagram in aircraft passenger compartment；
Fig. 6 is the partial enlargement diagram of B area in Fig. 1；
Fig. 7 is the partial enlargement diagram of Fig. 2；
Fig. 8 is the structural schematic diagram of spacing board of the present invention；
Fig. 9 is the structural schematic diagram of power supply device of the present invention.
The embodiments will be further described with reference to the accompanying drawings for the realization, the function and the advantages of the object of the present invention.
Specific embodiment
It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not intended to limit the present invention.
It should be noted that relational language such as " first ", " second " can be used for describing various assemblies, but these arts
Language is not intended to limit the component.These terms are only used to distinguish a component and another component.For example, not departing from model of the invention
It encloses, first assembly can be referred to as the second component, and the second component can also similarly be referred to as first assembly.Term " and/
Or " refer to continuous item and describe the combination of any one or more of item.
With reference to Fig. 1, Fig. 5, Fig. 6 and Fig. 7, Fig. 1 is the first embodiment of method of supplying power in civil aircraft main cabin of the present invention
Flow diagram, Fig. 5 are the structural schematic diagram in civil aircraft main cabin of the present invention；Fig. 6 is that the partial enlargement of B area in Fig. 1 shows
It is intended to；Fig. 7 is the partial enlargement diagram of Fig. 2.
Method of supplying power in civil aircraft main cabin of the invention, comprising the following steps:
Step S10, electronic equipment are connect by connecting line with charging interface 53, and the voltage that power supply device 31 is exported passes through conducting wire
32 are transmitted to charging interface 53, to realize for power electronic equipment, wherein the power supply device 31 is set to 10 institute of spacing board
In the internal cavities 100 sealed up for safekeeping, the charging interface 53 is located on the first Passenger Service Unit 20, the first passenger facilities group
Part 20 and spacing board 10 are arranged on passenger route 88.The invention has the following advantages: civil aircraft visitor of the invention
Method of supplying power in cabin, after the electronic equipment of passenger can be attached by connecting line and charging interface, then, power supply device institute
The voltage of output is by wire transmission to charging interface, to realize for power electronic equipment；With traditional power supply mode (USB
The power supply of passenger seat two sides is arranged in interface) different, method of supplying power to provided by the present invention, it is critical that power supply device is set
It is placed in the internal cavities that spacing board is sealed up for safekeeping, the charging interface is located on the first Passenger Service Unit, first passenger
Serviced component and spacing board are arranged on passenger route, i.e. the source of the electricity of this method of supplying power to just very close passenger, and again
There is no numerous cable structures, when this method of supplying power to, such as when powering not normal, maintenance personnel is directly for the electricity in internal cavities
Source device is repaired or is replaced, and is easy to be safeguarded, electrical stability will not be had an impact.It is described to fill
Electrical interface includes USB interface and Lightning interface, to adapt to Android mobile phone and iPhone.As shown in figure 9, the power supply
Device includes controller 202, lithium battery 203, memory module 204 and detection module 201, the lithium battery, memory module and inspection
Module is surveyed to connect with controller.
As shown in Figure 2, it is preferable that before the step S10 comprising steps of
Step S1, whether power supply device detection charging interface generates rising edge voltage pulse signal, if so, thening follow the steps S10.
In this preferred embodiment, the detection module 201 of power supply device is charged for carrying out signal detection on charging interface 53 by detection
Rising edge voltage pulse signal whether is generated on interface, if generating, shows that the electronic equipment of charging interface and passenger successfully connect
It connects, thens follow the steps S10.
As shown in Figure 3, it is preferable that the step S10 comprising steps of
Step S11, electronic equipment are connect by connecting line with charging interface；
Step S12, power supply device obtain the first identification marking number stored on electronic equipment；And judge first identification
Whether identifier number and the second standard logo number stored are identical, if so, thening follow the steps S13；
Step S13, the voltage that power supply device is exported carry out electronic equipment with realizing by wire transmission to charging interface
Charging.
The memory module 204 of the power supply device is previously stored with the second standard logo number, such as the seat E-17, this
The second standard logo number in power supply device above a seat E-17 is E-17；The first identification mark in the electronic equipment
Knowing number includes user information, and the seat number is to be input and stored in the memory of electronic equipment by passenger, for example be sitting in
E-17(seat number) passenger, want to repair the user information in electronic equipment using the charging interface 53 on Passenger Service Unit
It is changed to " E-17 "；I.e. this user information is just identical as the second standard logo number that power supply device on the seat E-17 is stored,
It can be achieved with charging in this way, avoid aircraft passenger compartment interior power device and misapplied, be stolen the problem of using, to improve certain safety
Property.The embodiment is that the user information of electronic equipment is utilized, and is the advantage that can be modified according to user's input.Such as figure
Shown in 4, it is preferable that step S14 is further comprised the steps of:, if the second standard logo that first identification marking is numbered and stored
Number is different, then carries out alarm sounds.It is arranged based on step S14, to play suggesting effect.
Wherein, with reference to Fig. 5, Fig. 6, Fig. 7, Fig. 8, the power supply device 31 is set to the internal cavities that spacing board 10 is sealed up for safekeeping
In 100, the charging interface 53 is located on the first Passenger Service Unit 20, first Passenger Service Unit 20 and spacing board 10
It is arranged on passenger route 88, the passenger route 88 is in the inner space Y in civil aircraft main cabin 99；Specifically,
The first Passenger Service Unit 20, the second Passenger Service Unit 21 and spacing board 10 are provided on the passenger route 88, between described
Partition side is connect with the first Passenger Service Unit, and the other side is connect with the second Passenger Service Unit, and the spacing board 10 is located at
Between first Passenger Service Unit 20 and the second Passenger Service Unit 21, the power supply device 31 is built in 10 institute of spacing board
In the internal cavities 100 sealed up for safekeeping, be provided with charging interface 53 on first Passenger Service Unit 20, the charging interface 53 with
Power supply device 31 connects.Specifically, first Passenger Service Unit 20, spacing board 10 and the second Passenger Service Unit 21 are according to elder generation
The linearly arrangement of sequence afterwards, further includes conducting wire 32, and the power supply device 31 is connect by conducting wire 32 with charging interface 53.
Preferably, it is provided with air-conditioning blow structure 51 and call button 52 on first Passenger Service Unit 20, it is described
Call button specially issues the ring tone of default decibel for calling crew after pressing；It preferably, further include for depositing
The storage silo 30 of the carry-on knapsack of passenger is put, the storage silo 30 is arranged on passenger route 88.
The internal cavities 100 sealed up for safekeeping for spacing board 10；The internal cavities 100 include opening up on passenger route 88
Groove is specifically additionally provided with guide rail 33, hook structure 34, institute is provided on the spacing board 10 on the passenger route 88
It states spacing board to be mounted on guide rail 33 by hook structure 34, this preferred embodiment closes the connection of spacing board and channel components
System is specifically limited, and to realize that interval version can be unloaded by hook structure, power supply device 31 is placed in table in spacing board at this time
It on face, is mounted on guide rail together, that is, power supply device 31 is placed in internal cavities 100, improves cabin interior
Space utilization rate enables aircraft passenger compartment to accommodate more passenger seats, increases economic efficiency, and be also convenient for maintenance personnel for
Power supply system carries out Fast-Maintenance.
The above is only a preferred embodiment of the present invention, is not intended to limit the scope of the invention, all to utilize this hair
Equivalent structure or equivalent flow shift made by bright specification and accompanying drawing content is applied directly or indirectly in other relevant skills
Art field, is included within the scope of the present invention.
Claims (5)
1. method of supplying power in a kind of civil aircraft main cabin, which comprises the following steps:
Step S10, electronic equipment are connect by connecting line with charging interface, and the voltage that power supply device is exported passes through wire transmission
To charging interface, to realize for power electronic equipment, wherein it is empty that the power supply device is set to the inside that spacing board is sealed up for safekeeping
In chamber, the charging interface is located on the first Passenger Service Unit, and first Passenger Service Unit and spacing board are arranged at
On passenger route.
2. method of supplying power in civil aircraft main cabin as described in claim 1, which is characterized in that the charging interface includes that USB connects
Mouth and Lightning interface.
3. method of supplying power in civil aircraft main cabin as described in claim 1, which is characterized in that include before the step S10
Step:
Step S1, whether power supply device detection charging interface generates rising edge voltage pulse signal, if so, thening follow the steps S10.
4. method of supplying power in civil aircraft main cabin as described in claim 1, which is characterized in that the step S10 comprising steps of
Step S11, electronic equipment are connect by connecting line with charging interface；
Step S12, power supply device obtain the first identification marking number stored on electronic equipment；And judge first identification
Whether identifier number and the second standard logo number stored are identical, if so, thening follow the steps S13；
Step S13, the voltage that power supply device is exported carry out electronic equipment with realizing by wire transmission to charging interface
Charging.
5. method of supplying power in civil aircraft main cabin as claimed in claim 4, which is characterized in that further comprise the steps of:
Step S14 carries out alarm and mentions if first identification marking number is different from the second standard logo number stored
Show.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810877596 | 2018-08-03 | ||
| CN2018108775961 | 2018-08-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109319124A true CN109319124A (en) | 2019-02-12 |
Family
ID=65263519
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810935899.4A Pending CN109319124A (en) | 2018-08-03 | 2018-08-16 | Method of supplying power in civil aircraft main cabin |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN109319124A (en) |
| WO (1) | WO2020024335A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020024335A1 (en) * | 2018-08-03 | 2020-02-06 | 李宗谕 | Power supply method for airliner cabin |
| WO2020024336A1 (en) * | 2018-08-03 | 2020-02-06 | 李宗谕 | Mounting structure in civil aircraft cabin |
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|---|---|---|---|---|
| DE102010034410A1 (en) * | 2010-08-14 | 2012-02-16 | Diehl Aerospace Gmbh | Supply device for passenger cabin, particularly for aircraft passenger cabin, comprises hood body, functional unit and supply duct which is attached on passenger facing side, where hood body comprises operating section |
| CN102439816A (en) * | 2011-08-22 | 2012-05-02 | 华为终端有限公司 | Hand held device, usb charger, and method for hand held device to identify usb charger |
| CN103580085A (en) * | 2012-08-09 | 2014-02-12 | 惠州市尚联达电子有限公司 | Mobile power supply with output currents capable of being automatically adjusted and charging method for loads |
| CN107108034A (en) * | 2014-09-29 | 2017-08-29 | Be航天公司 | Intelligent passenger service units |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN104085527A (en) * | 2014-07-09 | 2014-10-08 | 李庆宏 | Cuboid-shaped aircraft with upper support large flat plate |
| CN104973259B (en) * | 2015-07-09 | 2017-03-08 | 山东太古飞机工程有限公司 | Aircraft seat Power Transfer Unit installing rack |
| CN206590130U (en) * | 2016-11-09 | 2017-10-27 | 中国航空工业集团公司上海航空测控技术研究所 | A kind of power-supply management system for airborne entertainment system |
| US9914548B1 (en) * | 2017-02-22 | 2018-03-13 | Imagik International Corporation | USB power management and load distribution system |
| CN207089661U (en) * | 2017-04-19 | 2018-03-13 | 深圳喜乐航科技有限公司 | A kind of contactor control device based on airplane passenger cabin seat |
| CN109319124A (en) * | 2018-08-03 | 2019-02-12 | 李宗谕 | Method of supplying power in civil aircraft main cabin |
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2018
- 2018-08-16 CN CN201810935899.4A patent/CN109319124A/en active Pending
- 2018-08-16 WO PCT/CN2018/100861 patent/WO2020024335A1/en active Application Filing
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102010034410A1 (en) * | 2010-08-14 | 2012-02-16 | Diehl Aerospace Gmbh | Supply device for passenger cabin, particularly for aircraft passenger cabin, comprises hood body, functional unit and supply duct which is attached on passenger facing side, where hood body comprises operating section |
| CN102439816A (en) * | 2011-08-22 | 2012-05-02 | 华为终端有限公司 | Hand held device, usb charger, and method for hand held device to identify usb charger |
| CN103580085A (en) * | 2012-08-09 | 2014-02-12 | 惠州市尚联达电子有限公司 | Mobile power supply with output currents capable of being automatically adjusted and charging method for loads |
| CN107108034A (en) * | 2014-09-29 | 2017-08-29 | Be航天公司 | Intelligent passenger service units |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020024335A1 (en) * | 2018-08-03 | 2020-02-06 | 李宗谕 | Power supply method for airliner cabin |
| WO2020024336A1 (en) * | 2018-08-03 | 2020-02-06 | 李宗谕 | Mounting structure in civil aircraft cabin |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2020024335A1 (en) | 2020-02-06 |
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Application publication date: 20190212 |