CN208158217U - A kind of solar power system based on flight recorder - Google Patents
A kind of solar power system based on flight recorder Download PDFInfo
- Publication number
- CN208158217U CN208158217U CN201820741091.8U CN201820741091U CN208158217U CN 208158217 U CN208158217 U CN 208158217U CN 201820741091 U CN201820741091 U CN 201820741091U CN 208158217 U CN208158217 U CN 208158217U
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- CN
- China
- Prior art keywords
- unit
- flight
- solar
- sonar
- detection unit
- Prior art date
- 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.)
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/70—Hybrid systems, e.g. uninterruptible or back-up power supplies integrating renewable energies
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- Alarm Systems (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses a kind of flight recorder (FDR, CVR based on record aircraft flight attitude parameter and cockpit phonological working state, be commonly called as black box) solar power system, solar film battery is not under the premise of changing black box original shape, install GaAs solar energy film power generation module group additional on flight data recorder, GaAs solar energy film is insensitive to heat, still can normally work at a higher temperature will not influence its conversion ratio, high conversion efficiency, and material non-toxic is harmless does not have any influence for environment.
Description
Technical field
The utility model belongs to technical field of aerospace, based on record aircraft flight attitude parameter and drives more particularly to one kind
Sail the solar power system of the flight recorder (FDR, CVR are commonly called as black box) of cabin phonological working state.
Background technique
Record flight data and cockpit voice, energy can effectively be stored by installing black box additional in military or civil aircraft
Enough strong evidence is provided for aircraft accident analysis.However after the accident, black box is difficult to find in many cases, black
The time of the electricity that the backup power source of case the is capable of providing also only one moon.
Existing black box power source is single, and not in the ability of raw electric energy.Once designing duration black box beyond it
Son will be difficult to be found, this causes very big obstacle to crash analysis.
Utility model content
The purpose of the utility model is to provide a kind of third party's power supplys to be not easy to find to solve black box in power depletion
The problem of.
In order to achieve the above object, solar film battery provided by the utility model is not changing black box original shape
Under the premise of, install GaAs solar energy film power generation module group, GaAs solar energy film pair additional on flight data recorder
Heat is insensitive, and still can normally work will not influence its conversion ratio, high conversion efficiency, and material at a higher temperature
It is nontoxic there is no any influence for environment.
The purpose of this utility model can be achieved through the following technical solutions：
A kind of solar power system based on flight recorder installs GaAs solar energy film additional on flight recorder
Power generation module group, the GaAs solar energy film power generation module group include four blocks of GaAs solar film battery plates, integrated transformation
Device, security control unit, localpower, backup power source, detection unit, flight attitude parameters unit and cockpit voice recording list
Member, central control unit, sonar unit and ELT unit；The integrated transformer and security control unit are mounted on flight record
The inside of instrument, integrated transformer is on aircraft interface circuit board；
The input terminal of the localpower is connected with detection unit, detection unit input terminal and flight attitude parameters unit
It is connected with cockpit voice recording unit, sonar unit, the output end of detection unit is connected with central control unit, cockpit
Voice recording unit and flight attitude parameters unit are connected with detection unit；The backup power source is used for the feelings in primary source failure
Under condition, detection unit, sonar unit, the power supply of ELT unit are continued as；Central control unit is current to aircraft by detection unit
State judges, and controls sonar unit, ELT unit according to requiring to work normally；
Four pieces of solar panels are using method connection in parallel.
Integrated transformer is used to change voltage in order to charge to backup power source.
The ELT unit and sonar unit are emergency communication device for high, can voluntarily start operation when aircraft distress.
The backup power source is using the repeatable battery to charge.
Wherein GaAs solar energy film power generation module group is mounted on four outer surfaces of flight data recorder, is there is light
Solar power generation is independently carried out according under conditions of.Localpower battery and backup power source battery are mounted on flying quality note
The inside of device is recorded, is used to power to detection unit, ELT unit, sonar unit.Integrated transformer and security control unit are integrated in
On aircraft interface circuit board, integrated transformer, which is used to change voltage, charges to battery, and the effect of security control component is
It will be automatically stopped in the electricity of backup power source battery and charge to battery in a certain range, then it is directly single to detection
Member, ELT unit and the power supply of sonar unit.Detection unit, central control unit, sonar and ELT unit is also needed to match in addition
Close the work of GaAs solar film battery group.
Detection unit is aircraft detection circuit in state of flight, input terminal and flight attitude parameters unit, cockpit
Voice recording unit is connected with sonar unit, and output end is connected with central control unit, for detecting above-mentioned each unit work
State, and will test result and be transferred to central control unit；
Cockpit voice recording unit and flight attitude parameters unit are used to acquire each in the operating parameter and aircraft of aircraft
Kind of call includes the call of pilot and air traffic control person, just, dialogue of the copilot in cockpit, driver, steward
Various sound in broadcast and cockpit to passenger, the sound issued including various alarm devices simultaneously pass collected information
Pass detection unit；
Backup power source is the backup power source of battery composition, for continuing as detecting in the case where localpower failure
Unit, sonar unit, the power supply of ELT unit；
Central control unit is the core of whole device control, can be made by the detection unit state current to aircraft
Judgement, and sonar unit, ELT unit and gallium arsenide solar cell mould group are controlled according to requiring to work normally.
ELT unit and sonar unit are the emergency communication device for high taken in traditional technology, can be when aircraft distress
Voluntarily starting operation；
Integrated transformer is used to change voltage in order to charge to backup power source battery pack.
Security control unit will be automatically stopped when the electricity of backup power source battery pack reaches a certain range to battery into
Row charging, then directly power to detection unit, ELT unit and sonar unit.To protect circuit and backup power source battery
The safety of group.
GaAs solar energy film plate is the core apparatus for producing electricl energy.
The beneficial effects of the utility model：
GaAs solar film battery group provided by the utility model is the principle using solar power generation in standby electricity
More electric energy are provided other than source battery group so as to allow sonar unit and ELT cell operation more times to look for for search party
A possibility that bigger is promoted to black box.
Detailed description of the invention
In order to facilitate the understanding of those skilled in the art, the utility model will be further described below with reference to the accompanying drawings.
Fig. 1 is a kind of solar power system figure based on flight recorder provided by the utility model.
Specific embodiment
With reference to the accompanying drawing with specific implementation to provided by the utility model for charging to backup power source component
GaAs solar film battery group is further detailed.
Arsenic provided by the utility model for charging to main power source component and backup power source component as shown in Figure 1
Gallium solar film battery group includes：Four pieces of independent GaAs solar film battery plates, integrated transformers, security control list
Member, localpower and backup power source, wherein four pieces of solar panels are connected using method in parallel, when one of or more
Block solar panel can guarantee that remaining power plate works normally when impaired.Integrated transformer and security control component are mounted on flight note
The inside of instrument is recorded, for integrated transformer on aircraft interface circuit board, integrated transformer can be by GaAs solar film battery
The voltage that plate generates changes the voltage that works normally to suitable backup power source battery pack, and the electric energy of generation is stored in spare
In power-supply battery group.Security control component is to be automatically stopped to charge to it and incite somebody to action in the electricity abundance of backup power source battery pack
Electric energy is delivered directly to detection unit, ELT unit and sonar unit and is powered.Backup power source battery pack is using repeatable charging
Battery.
The GaAs solar power generation mould group includes：Four blocks of GaAs solar film battery plates they be respectively
101,102,103,104.Integrated transformer 105, security control unit 106, localpower 107, backup power source 108, detection are single
Member 109, flight attitude parameters unit and cockpit voice recording unit 110, central control unit 111,112 and of sonar unit
ELT unit 113.Main power source battery component 107 is the working power of this system under normal circumstances, and input power is by interior of aircraft
Working power provide, input terminal is connected with detection unit 109.
Detection unit 109 is aircraft detection circuit in state of flight, input terminal and flight attitude parameters unit and is driven
It sails cabin voice recording unit 110 to be connected with sonar unit 112, output end is connected with central control unit 111, on detecting
Each unit working condition is stated, and will test result and be transferred to central control unit 111；
Cockpit voice recording unit and flight attitude parameters unit 110 are used to acquire in the operating parameter and aircraft of aircraft
Various calls include the calls of pilot and air traffic control person, just, dialogue of the copilot in cockpit, driver, empty are taken
Member is to various sound in the broadcast of passenger and cockpit, the sound that issues including various alarm devices and by collected information
Pass to detection unit 109；
Backup power source 108 is the backup power source of battery composition, for continuing as in the case where main power source 107 fails
Detection unit 109, sonar unit 112, ELT unit 113 are powered；
Central control unit 111 is the core of whole device control, shape that can be current to aircraft by detection unit 109
State judges, and controls sonar unit 112, ELT unit 113 according to requiring to work normally.
ELT unit 113 and sonar unit 112 are the emergency communication device for high taken in traditional technology, can be in aircraft distress
When voluntarily start operation；
Integrated transformer 105 is used to change voltage in order to charge to backup power source battery pack 108.
Security control unit 106 will be automatically stopped when the electricity of backup power source battery pack 108 reaches a certain range to standby
It is charged with power-supply battery group 108, then directly powered to detection unit 109, ELT unit 113 and sonar unit 112.From
And the safety of circuit and backup power source battery pack is protected, therefore also extend the work of sonar unit 112 and ELT unit 113
Time can strive for more times to search and rescue team.
The preferred embodiment in the utility model disclosed above is only intended to help to illustrate the utility model.Preferred embodiment is simultaneously
There is no the details that detailed descriptionthe is all, also not limiting the utility model is only the specific embodiment.Obviously, according to this theory
The content of bright book can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably
The principles of the present invention and practical application are explained, so that skilled artisan be enable to better understand and utilize this
Utility model.The utility model is limited only by the claims and their full scope and equivalents.
Claims (5)
1. a kind of solar power system based on flight recorder, which is characterized in that install GaAs additional on flight recorder
Solar energy film power generation module group, GaAs solar energy film power generation module group are mounted on four outside tables of flight data recorder
Face；
The GaAs solar energy film power generation module group includes four pieces of GaAs solar film battery plates, integrated transformers, peace
Full control unit, localpower, backup power source, detection unit, flight attitude parameters unit and cockpit voice recording unit, in
Entreat control unit, sonar unit and ELT unit；The integrated transformer and security control unit are mounted on the interior of flight recorder
Portion, integrated transformer is on aircraft interface circuit board；Localpower battery and backup power source battery are mounted on flight number
According to the inside of logger, it is used to power to detection unit, ELT unit, sonar unit；
The input terminal of the localpower is connected with detection unit, detection unit input terminal and flight attitude parameters unit and drives
It is connected to sail cabin voice recording unit, sonar unit, the output end of detection unit is connected with central control unit, cockpit speech
Recording unit and flight attitude parameters unit are connected with detection unit；The backup power source is used for the primary source failure the case where
Under, continue as detection unit, sonar unit, the power supply of ELT unit；The central control unit shape current to aircraft by detection unit
State judges, and controls sonar unit, ELT unit according to requiring to work normally.
2. a kind of solar power system based on flight recorder according to claim 1, which is characterized in that described four
Block solar panel is using method connection in parallel.
3. a kind of solar power system based on flight recorder according to claim 1, which is characterized in that integrated to become
Depressor is used to change voltage in order to charge to backup power source.
4. a kind of solar power system based on flight recorder according to claim 1, which is characterized in that described
ELT unit and sonar unit are emergency communication device for high, can voluntarily start operation when aircraft distress.
5. a kind of solar power system based on flight recorder according to claim 1, which is characterized in that described standby
With power supply using the battery of repeatable charging.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820741091.8U CN208158217U (en) | 2018-05-18 | 2018-05-18 | A kind of solar power system based on flight recorder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820741091.8U CN208158217U (en) | 2018-05-18 | 2018-05-18 | A kind of solar power system based on flight recorder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208158217U true CN208158217U (en) | 2018-11-27 |
Family
ID=64387594
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820741091.8U Expired - Fee Related CN208158217U (en) | 2018-05-18 | 2018-05-18 | A kind of solar power system based on flight recorder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208158217U (en) |
-
2018
- 2018-05-18 CN CN201820741091.8U patent/CN208158217U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181127 |