CN109229406A - Aircraft high-frequency communication warning system - Google Patents
Aircraft high-frequency communication warning system Download PDFInfo
- Publication number
- CN109229406A CN109229406A CN201811211023.1A CN201811211023A CN109229406A CN 109229406 A CN109229406 A CN 109229406A CN 201811211023 A CN201811211023 A CN 201811211023A CN 109229406 A CN109229406 A CN 109229406A
- Authority
- CN
- China
- Prior art keywords
- ground
- antenna
- frequency communication
- warning system
- controlled component
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B3/00—Audible signalling systems; Audible personal calling systems
- G08B3/10—Audible signalling systems; Audible personal calling systems using electric transmission; using electromagnetic transmission
- G08B3/1008—Personal calling arrangements or devices, i.e. paging systems
- G08B3/1016—Personal calling arrangements or devices, i.e. paging systems using wireless transmission
- G08B3/1025—Paging receivers with audible signalling details
- G08B3/1033—Paging receivers with audible signalling details with voice message alert
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/18502—Airborne stations
- H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18517—Transmission equipment in earth stations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D2231/00—Emergency oxygen systems
- B64D2231/02—Supply or distribution systems
- B64D2231/025—Oxygen masks; Mask storages; Features related to mask deployment
Abstract
The present invention relates to a kind of radio technologies, and in particular to aircraft high-frequency communication warning system.Aircraft high-frequency communication warning system, including radio communication panel, HF antenna coupler, Remote Electronic Unit, flying quality acquisition component, the selection calling decoder being connect respectively with HF transceiver signal；The HF antenna coupler is connected with HF antenna, and the Remote Electronic Unit is connected with controlled component, and the controlled component includes alarm, ground signal receiver, surface warning device, and the ground signal receiver, surface warning device are set to ground.The present invention, in case of flight failure, can notify unit and ground in aircraft flight in time.
Description
Technical field
The present invention relates to a kind of radio technologies, and in particular to aircraft high-frequency communication warning system.
Background technique
High frequency communication system (HFCOM) is for report words communicate it at a distance between aircraft and ground or aircraft and other aircrafts
With.Traditional high frequency communication system is made of transmitting-receiving unit, antenna coupler, control box and antenna, if hair in flight course
Raw flight failure, cannot notify unit and ground in time.
Summary of the invention
The purpose of the present invention is to provide aircraft high-frequency communication warning systems, solve existing high frequency communication system and fly
In case of flight failure in journey, the problem of cannot notifying unit and ground in time.
In order to solve the above technical problems, the invention adopts the following technical scheme:
Aircraft high-frequency communication warning system, including radio communication panel, the HF antenna coupling being connect respectively with HF transceiver signal
Clutch, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupler is connected with HF
Antenna, the Remote Electronic Unit are connected with controlled component, the controlled component include alarm, ground signal receiver,
Face alarm device, the ground signal receiver, surface warning device are set to ground.
During flight, when flying quality acquisition component flying quality collected has deviation, flying quality acquisition component will
Signal is transmitted Remote Electronic Unit by HF antenna coupler, HF antenna by data information transfer to HF transceiver, HF transceiver,
Remote Electronic Unit is set to work, the alarm equipment alarm of controlled component, to play the role of instant automatic alarm.Positioned at ground
Ground signal receiver receives signal, and control surface warning device alarm is timely automated to notify ground.
Preferably, the controlled component further includes microphone, headset earpiece, crew can be by microphone to the ear of passenger
Machine earpiece carries out audio alert.
Preferably, the controlled component further includes oxygen mask, the enabling of oxygen mask can be automatically controled, improve and fly
Row safety.
Preferably, the controlled component further includes barn door, the opening and closing of barn door can be automatically controled, in emergency circumstances
Barn door is automatically controlled, flight safety is improved.
Preferably, the Remote Electronic Unit is also connected with audio frequency control plate, the controlled component further includes loudspeaker,
Loudspeaker in cabin can be controlled by audio frequency control plate.
Preferably, the HF antenna is installed on the vertical tail of aircraft, 2 meters of personnel's seat or more in cabin of disembarking.HF
There is radiation injury to human body when antenna emits, 2 meters of distance or more can control in safe range, prevent from being harmful to human body.
Compared with prior art, the beneficial effects of the present invention are: if it happens the present invention flies in aircraft flight
Failure can notify unit and ground in time；Crew of the present invention can carry out audio alert to the headset earpiece of passenger by microphone；
The present invention can be automatically controled the enabling of oxygen mask, improve flight safety；The present invention can be automatically controled the opening and closing of barn door, tightly
Barn door is automatically controlled in anxious situation, improves flight safety；HF antenna setting of the present invention position prevents from being harmful to human body.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to embodiments, to the present invention
It is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not used to
Limit the present invention.
Embodiment 1:
Aircraft high-frequency communication warning system, including radio communication panel, the HF antenna coupling being connect respectively with HF transceiver signal
Clutch, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupler is connected with HF
Antenna, the Remote Electronic Unit are connected with controlled component, the controlled component include alarm, ground signal receiver,
Face alarm device, the ground signal receiver, surface warning device are set to ground.
During flight, when flying quality acquisition component flying quality collected has deviation, flying quality acquisition component will
Signal is transmitted Remote Electronic Unit by HF antenna coupler, HF antenna by data information transfer to HF transceiver, HF transceiver,
Remote Electronic Unit is set to work, the alarm equipment alarm of controlled component, to play the role of instant automatic alarm.Positioned at ground
Ground signal receiver receives signal, and control surface warning device alarm is timely automated to notify ground.
Embodiment 2:
Aircraft high-frequency communication warning system, including radio communication panel, the HF antenna coupling being connect respectively with HF transceiver signal
Clutch, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupler is connected with HF
Antenna, the Remote Electronic Unit are connected with controlled component, and the controlled component includes alarm, microphone, headset earpiece, ground
Signal receiver, surface warning device, the ground signal receiver, surface warning device are set to ground.
During flight, when flying quality acquisition component flying quality collected has deviation, flying quality acquisition component will
Signal is transmitted Remote Electronic Unit by HF antenna coupler, HF antenna by data information transfer to HF transceiver, HF transceiver,
Remote Electronic Unit is set to work, the alarm equipment alarm of controlled component, to play the role of instant automatic alarm.Crew may be used also
Audio alert is carried out to the headset earpiece of passenger by microphone.Ground signal receiver positioned at ground receives signal, control ground
The alarm of face alarm device, it is timely automated to notify ground.
Embodiment 3:
Aircraft high-frequency communication warning system, including radio communication panel, the HF antenna coupling being connect respectively with HF transceiver signal
Clutch, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupler is connected with HF
Antenna, the Remote Electronic Unit are connected with controlled component, and the controlled component includes alarm, microphone, headset earpiece, oxygen
Mask, ground signal receiver, surface warning device, the ground signal receiver, surface warning device are set to ground.
During flight, when flying quality acquisition component flying quality collected has deviation, flying quality acquisition component will
Signal is transmitted Remote Electronic Unit by HF antenna coupler, HF antenna by data information transfer to HF transceiver, HF transceiver,
Remote Electronic Unit is set to work, the alarm equipment alarm of controlled component, to play the role of instant automatic alarm.Crew may be used also
Audio alert is carried out to the headset earpiece of passenger by microphone, the enabling of oxygen mask is also can be automatically controled, improves flight safety
Property.Ground signal receiver positioned at ground receives signal, and control surface warning device alarm is timely automated to notify ground.
Embodiment 4:
Aircraft high-frequency communication warning system, including radio communication panel, the HF antenna coupling being connect respectively with HF transceiver signal
Clutch, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupler is connected with HF
Antenna, the Remote Electronic Unit are connected with controlled component, and the controlled component includes alarm, microphone, headset earpiece, oxygen
Mask, barn door, ground signal receiver, surface warning device, the ground signal receiver, surface warning device are set to ground
Face.
During flight, when flying quality acquisition component flying quality collected has deviation, flying quality acquisition component will
Signal is transmitted Remote Electronic Unit by HF antenna coupler, HF antenna by data information transfer to HF transceiver, HF transceiver,
Remote Electronic Unit is set to work, the alarm equipment alarm of controlled component can also be controlled automatically to play the role of instant automatic alarm
The opening and closing of barn door processed in emergency circumstances automatically controls barn door, improves flight safety.Crew can also be by microphone to multiplying
The headset earpiece of visitor carries out audio alert, also can be automatically controled the enabling of oxygen mask, improves flight safety.Positioned at ground
Ground signal receiver receives signal, and control surface warning device alarm is timely automated to notify ground.
Optimum embodiment:
Aircraft high-frequency communication warning system, including radio communication panel, the HF antenna coupling being connect respectively with HF transceiver signal
Clutch, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupler is connected with HF
Antenna, HF antenna are installed on the vertical tail of aircraft, 2 meters of personnel's seat or more in cabin of disembarking.HF antenna has human body when emitting
Radiation injury, 2 meters of distance or more can control in safe range, prevent from being harmful to human body.Remote Electronic Unit is also connected with sound
Frequency control panel, the Remote Electronic Unit are connected with controlled component, the controlled component include alarm, microphone, headset earpiece,
Oxygen mask, barn door, loudspeaker, ground signal receiver, surface warning device, the ground signal receiver, ground are alert
Report device is set to ground.
During flight, when flying quality acquisition component flying quality collected has deviation, flying quality acquisition component will
Signal is transmitted Remote Electronic Unit by HF antenna coupler, HF antenna by data information transfer to HF transceiver, HF transceiver,
Remote Electronic Unit is set to work, the alarm equipment alarm of controlled component can also be controlled automatically to play the role of instant automatic alarm
The opening and closing of barn door processed in emergency circumstances automatically controls barn door, improves flight safety.Crew can also be by microphone to multiplying
The headset earpiece of visitor carries out audio alert, can control loudspeaker in cabin by audio frequency control plate.It also can be automatically controled oxygen face
The enabling of cover improves flight safety.Ground signal receiver positioned at ground receives signal, and control surface warning device is alarmed,
It is timely automated to notify ground.
Multiple explanatory embodiments spoken of in the present specification refer to the specific method packet for combining embodiment description
It includes at least one embodiment of the application generality description.It is not certain that statement of the same race, which occur, in multiple places in the description
Refer to the same embodiment.Furthermore, it is understood that is advocated is to combine when describing a method in conjunction with any one embodiment
Other embodiments realize that this method is fallen within the scope of the present invention.
Claims (6)
1. aircraft high-frequency communication warning system, it is characterised in that: including the radio communication being connect respectively with HF transceiver signal
Panel, HF antenna coupler, Remote Electronic Unit, flying quality acquisition component, selection calling decoder；The HF antenna coupling
Clutch is connected with HF antenna, and the Remote Electronic Unit is connected with controlled component, and the controlled component includes alarm, ground letter
Number receiver, surface warning device, the ground signal receiver, surface warning device are set to ground.
2. aircraft high-frequency communication warning system according to claim 1, it is characterised in that: the controlled component further includes
Microphone, headset earpiece.
3. aircraft high-frequency communication warning system according to claim 2, it is characterised in that: the controlled component further includes
Oxygen mask.
4. aircraft high-frequency communication warning system according to claim 2, it is characterised in that: the controlled component further includes
Barn door.
5. aircraft high-frequency communication warning system according to claim 2, it is characterised in that: the Remote Electronic Unit also connects
It is connected to audio frequency control plate, the controlled component further includes loudspeaker.
6. aircraft high-frequency communication warning system according to claim 1, it is characterised in that: the HF antenna is installed on winged
The vertical tail of machine, 2 meters of personnel's seat or more in cabin of disembarking.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811211023.1A CN109229406A (en) | 2018-10-17 | 2018-10-17 | Aircraft high-frequency communication warning system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811211023.1A CN109229406A (en) | 2018-10-17 | 2018-10-17 | Aircraft high-frequency communication warning system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109229406A true CN109229406A (en) | 2019-01-18 |
Family
ID=65053101
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811211023.1A Pending CN109229406A (en) | 2018-10-17 | 2018-10-17 | Aircraft high-frequency communication warning system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109229406A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1266404A (en) * | 1997-07-30 | 2000-09-13 | 维达电子设备股份公司 | Surveillance device for use in aircraft interiors, especially in passenger aeroplanes |
| US20030098773A1 (en) * | 2001-11-26 | 2003-05-29 | The Boeing Company | Methods and systems for air vehicle telemetry |
| US20030135311A1 (en) * | 2002-01-17 | 2003-07-17 | Levine Howard B. | Aircraft flight and voice data recorder system and method |
| US20030225492A1 (en) * | 2002-05-29 | 2003-12-04 | Cope Gary G. | Flight data transmission via satellite link and ground storage of data |
| CN104512552A (en) * | 2013-10-04 | 2015-04-15 | 埃姆普里萨有限公司 | Modular passenger service units and assemblies thereof |
| US20150151838A1 (en) * | 2013-12-03 | 2015-06-04 | Federal Express Corporation | System and method for enhancing vision inside an aircraft cockpit |
-
2018
- 2018-10-17 CN CN201811211023.1A patent/CN109229406A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1266404A (en) * | 1997-07-30 | 2000-09-13 | 维达电子设备股份公司 | Surveillance device for use in aircraft interiors, especially in passenger aeroplanes |
| US20030098773A1 (en) * | 2001-11-26 | 2003-05-29 | The Boeing Company | Methods and systems for air vehicle telemetry |
| US20030135311A1 (en) * | 2002-01-17 | 2003-07-17 | Levine Howard B. | Aircraft flight and voice data recorder system and method |
| US20030225492A1 (en) * | 2002-05-29 | 2003-12-04 | Cope Gary G. | Flight data transmission via satellite link and ground storage of data |
| CN104512552A (en) * | 2013-10-04 | 2015-04-15 | 埃姆普里萨有限公司 | Modular passenger service units and assemblies thereof |
| US20150151838A1 (en) * | 2013-12-03 | 2015-06-04 | Federal Express Corporation | System and method for enhancing vision inside an aircraft cockpit |
Non-Patent Citations (1)
| Title |
|---|
| 杨江等: "机载音频选择板和内话系统修理研究", 《电子技术与软件工程》 * |
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Legal Events
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190118 |
|
| RJ01 | Rejection of invention patent application after publication |