CN101290687B - Method for rapidly obtaining cockpit voice recording - Google Patents

Method for rapidly obtaining cockpit voice recording Download PDF

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Publication number
CN101290687B
CN101290687B CN2008100664613A CN200810066461A CN101290687B CN 101290687 B CN101290687 B CN 101290687B CN 2008100664613 A CN2008100664613 A CN 2008100664613A CN 200810066461 A CN200810066461 A CN 200810066461A CN 101290687 B CN101290687 B CN 101290687B
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CN
China
Prior art keywords
sound signal
voice
aircraft
voice recording
playback
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Expired - Fee Related
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CN2008100664613A
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Chinese (zh)
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CN101290687A (en
Inventor
林帆
喻建黎
冯文强
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Shenzhen Donika Avionics Co ltd
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SHENZHEN AVIATION ENGINEERING Co Ltd
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Priority to CN2008100664613A priority Critical patent/CN101290687B/en
Publication of CN101290687A publication Critical patent/CN101290687A/en
Application granted granted Critical
Publication of CN101290687B publication Critical patent/CN101290687B/en
Expired - Fee Related legal-status Critical Current
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Abstract

The invention aims to solve technical problems of complicated operation, short recording period and so on for an airborne CVR recorder during application, and provides a method for acquiring cockpit voice record quickly. The method has the advantages of simple operation and long recording. The technical proposal adopted by the method comprises the following steps of: acquiring a voice source in a cockpit through a service platform and a remote electronic component and converting the voice source into an audio signal; then, accessing the acquired audio signal to a quick acquisition device in parallel through a transfer cable; performing audio conversion, analog-to-digital conversion and processing and coding encryption to the audio signal with the quick acquisition device; storing data into a memory card; taking out the memory card from the quick acquisition device, and inserting the memory card into a player for voice playback. The method has the advantages that longer voice period can be recorded; voice data with larger volume can be stored; the operation is simple, and the playback processing is convenient; meanwhile, the voice data can be encrypted to prevent voice information from leaking.

Description

A kind of method of obtaining cockpit voice recording fast
Technical field
The present invention relates to the speech recording apparatus in a kind of aircraft, relate to a kind of method of obtaining cockpit voice recording fast particularly.
Background technology
At present, some airline is in order to improve service quality, tighten security flight consciousness, need examine the in-flight crew term of conversing, with standard crew's conversation term.The way that can only take at present be by flight finish the airborne CVR register of back dismounting (in modern times on the commercial aircraft like Boeing, Air Passenger aircraft etc.; Cockpit voice recording device (Cockpit Voice Recorder; Be called for short airborne CVR registering instrument) airborne equipment that is absolutely necessary, its significant feature is to be used for the aircraft accident analysis of causes is used.Cockpit voice recording device cycle index aircraft various sound of nearest 2 hours or 30 minutes in the driving cabin in flight course; Comprise words in the unit, the empty conversation in land, audible warning sound etc.), handle playback apparatus through dedicated ground again the content of airborne CVR recorder trace is carried out playback.But because the time of CVR recorder trace short (the longest 2 hours) does not reach the purpose that the crew is examined far away; Itself costs an arm and a leg, and often dismantles its easy damage and causes serious economy loss; Need to bring inconvenience to work through dedicated ground playback process very complicacy.These all are the difficult problems of puzzlement airline.
Summary of the invention
Technical matterss such as the present invention bothers for solving above-mentioned airborne CVR registering instrument complicated operation in application process, and writing time is short provide a kind of simple to operate, the method for obtaining cockpit voice recording fast that writing time is long.
The present invention realizes goal of the invention through following technical scheme; A kind of method of obtaining cockpit voice recording fast; The steps include: sound signal is collected and changed into to the speech source in the aircraft cockpit through operating platform and electronic remote parts, then the sound signal of collecting is inserted quick deriving means through the transit cable parallel connection; Fast deriving means to sound signal carry out audio conversion, analog to digital conversion and processing, encoding compression is encrypted, and data storing to storing in the card, take out the storage card in the quick deriving means, the insertion playback equipment directly carries out audio playback.
Described quick deriving means carries out audio conversion, analog to digital conversion and processing, encoding compression to sound signal to be encrypted, and data storing to storing in the card, its concrete grammar is:
A is with the power supply connecting system power module on the aircraft;
The b voicefrequency circuit becomes non-equilibrium sound signal with the Balanced Audio signal transition of aircraft, and the sound signal that the recording module input requires is satisfied in output;
C clock Acquisition Circuit is carried out conversion processing to the clock signal in the aircraft, makes it to close main control module and receives and gather;
After the clock signal that d main control module collects, control each road recording module and record;
The e recording module carries out each road sound signal after the analog to digital conversion by certain sampling rate image data, and data are carried out compress-encrypt and in storing card, are that filename store with the temporal information with data storage.
The f auxiliary functional circuit to each recording channel, road monitor, the indication of System self-test, state.
The invention has the beneficial effects as follows that deriving means can use with airborne cockpit voice recording device is parallel fast, can write down the longer voice time on the basis that does not change original airborne cockpit voice recording device device structure; Store more jumbo speech data, and simple to operate, and playback process is convenient; Need not dismantle equipment; Directly choose to store to block and just can carry out playback to voice recording, can encrypt speech data simultaneously, prevent that the voice messaging data from leaking through playback equipment.
Embodiment
A kind of method of obtaining cockpit voice recording fast; The steps include: sound signal is collected and changed into to the speech source in the aircraft cockpit through operating platform and electronic remote parts, then the sound signal of collecting is inserted quick deriving means through the transit cable parallel connection; Fast deriving means to sound signal carry out audio conversion, analog to digital conversion and processing, encoding compression is encrypted, and data storing to storing in the card, take out the storage card in the quick deriving means, the insertion playback equipment directly carries out audio playback.
Described quick deriving means carries out audio conversion, analog to digital conversion and processing, encoding compression to sound signal to be encrypted, and data storing to storing in the card, its concrete grammar is:
A is the AC115V power supply connecting system power module on the aircraft, after the input protection circuit of power module, AC/DC, DC/DC conversion output+28V ,+5V ,+12V ,-the 12V WV;
The b voicefrequency circuit becomes non-equilibrium sound signal with the Balanced Audio signal transition of aircraft, satisfies the sound signal that the recording module input requires through attenuation network, LPF, amplitude adjustment back output again;
C clock Acquisition Circuit is carried out level conversion to 429 data buss in the machine, converts to be fit to the Transistor-Transistor Logic level that master controller receives and handles;
The d recording module carries out each road sound signal after the analog to digital conversion by certain sampling rate image data, and data are carried out compress-encrypt and in storing card, are that filename store with the temporal information with data storage.
E main control module receives and handles 429 clocks, indicates the control and the recording state of each passage recording module;
The f auxiliary functional circuit is mainly accomplished passage monitoring, System self-test, state indication.When pushing the button of a certain passage, monitoring signal will switch to this passage.When pinning certain passage button and unclamp again more than 2 seconds,, show that this passage recording is normal if from monitoring headpone, hear tone signal 3.In addition when each passage is in proper working order, the regular flicker of respective channel duty lantern festival.

Claims (2)

1. method of obtaining cockpit voice recording fast; The steps include: sound signal is collected and changed into to the speech source in the aircraft cockpit through operating platform and electronic remote parts; Then the audio signal transmission of collecting is carried out record to airborne cockpit voice recording device; Airborne cockpit voice recording device under the dismounting carries out audio playback through handling playback apparatus again;
It is characterized in that: carry out following steps again in operating platform and the collection of electronic remote parts and after changing into sound signal:
(1) through transit cable the sound signal parallel connection of collecting is inserted quick deriving means;
(2) fast deriving means to sound signal carry out audio conversion, analog to digital conversion and processing, encoding compression is encrypted, and blocks data storing to storing, and comprises step by step following:
A is with the power supply connecting system power module on the aircraft;
The b voicefrequency circuit becomes non-equilibrium sound signal with the Balanced Audio signal transition of aircraft, and the sound signal that the recording module input requires is satisfied in output;
C clock Acquisition Circuit is carried out conversion processing to the clock signal in the aircraft, makes it to be fit to main control module and receives and gather;
After the clock signal that d main control module collects, control each road recording module and record;
The e recording module carries out each road sound signal after the analog to digital conversion by certain sampling rate image data, and data are carried out compress-encrypt and in storing card, are that filename store with the temporal information with data storage;
(3) the storage card in the quick deriving means of taking-up inserts playback equipment and directly carries out audio playback.
2. a kind of method of obtaining cockpit voice recording fast according to claim 1 is characterized in that: said (2) step is further comprising the steps of:
The f auxiliary functional circuit to each recording channel, road monitor, the indication of System self-test, state.
CN2008100664613A 2008-04-07 2008-04-07 Method for rapidly obtaining cockpit voice recording Expired - Fee Related CN101290687B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2008100664613A CN101290687B (en) 2008-04-07 2008-04-07 Method for rapidly obtaining cockpit voice recording

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2008100664613A CN101290687B (en) 2008-04-07 2008-04-07 Method for rapidly obtaining cockpit voice recording

Publications (2)

Publication Number Publication Date
CN101290687A CN101290687A (en) 2008-10-22
CN101290687B true CN101290687B (en) 2012-06-27

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Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102867345B (en) * 2012-09-13 2014-12-24 深圳市多尼卡电子技术有限公司 Aviation onboard voice recording device
FR3001075B1 (en) * 2013-01-15 2016-07-01 Airbus Operations Sas FLIGHT RECORDING SYSTEM IN AN AIRCRAFT INCORPORATING THE AUDIO MANAGEMENT FUNCTION
CN103679847B (en) * 2013-12-05 2016-09-14 成都民航空管科技发展有限公司 Voice collecting storage system and method
CN107103925B (en) * 2016-02-22 2020-11-10 深圳市多尼卡电子技术有限公司 Access passenger cabin voice recorder equipment
CN115022776B (en) * 2022-08-09 2022-11-22 中国电子科技集团公司第十研究所 Airborne comprehensive audio processing unit
CN115620721A (en) * 2022-12-05 2023-01-17 山东盖特航空科技有限公司 System and method for acquiring audio record

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2240742Y (en) * 1995-08-31 1996-11-20 合肥迪宏电子技术发展有限公司 IC disc recording instrument for data of motive vehicle running state
CN2436385Y (en) * 2000-08-08 2001-06-27 张成虎 Black box for passenger coach
CN2886950Y (en) * 2006-05-18 2007-04-04 西安交通大学 Video automobile black box
CN200983252Y (en) * 2006-09-12 2007-11-28 深圳市多尼卡电子技术有限公司 Aviation carried digital recordable video player

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2240742Y (en) * 1995-08-31 1996-11-20 合肥迪宏电子技术发展有限公司 IC disc recording instrument for data of motive vehicle running state
CN2436385Y (en) * 2000-08-08 2001-06-27 张成虎 Black box for passenger coach
CN2886950Y (en) * 2006-05-18 2007-04-04 西安交通大学 Video automobile black box
CN200983252Y (en) * 2006-09-12 2007-11-28 深圳市多尼卡电子技术有限公司 Aviation carried digital recordable video player

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
JP特开2001-184089A 2001.07.06

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EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20081022

Assignee: SHENZHEN INSTITUTE OF AVIONICS TECHNOLOGY

Assignor: DONICA AVIATION ENGINEERING Co.,Ltd.

Contract record no.: 2014440020280

Denomination of invention: Method for rapidly obtaining cockpit voice recording

Granted publication date: 20120627

License type: Common License

Record date: 20140721

LICC Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model
TR01 Transfer of patent right

Effective date of registration: 20190306

Address after: 518000 Guangzhou Nanshan Nantou Street Pass No. 2 Zhiheng Strategic Emerging Industrial Park, 1 Building and 1 Floor

Patentee after: Shenzhen Donika Avionics Co.,Ltd.

Address before: 518000 South Building, 29 South Science and Technology 6 Road, Nanshan High-tech Zone, Shenzhen City, Guangdong Province, 3rd Floor

Patentee before: DONICA AVIATION ENGINEERING Co.,Ltd.

TR01 Transfer of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20120627

CF01 Termination of patent right due to non-payment of annual fee