CN202373152U - System for graphical display of radio range station and aircraft identification instructions - Google Patents
System for graphical display of radio range station and aircraft identification instructions Download PDFInfo
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- CN202373152U CN202373152U CN2011205096888U CN201120509688U CN202373152U CN 202373152 U CN202373152 U CN 202373152U CN 2011205096888 U CN2011205096888 U CN 2011205096888U CN 201120509688 U CN201120509688 U CN 201120509688U CN 202373152 U CN202373152 U CN 202373152U
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Abstract
The utility model discloses a system for the graphical display of radio range station and aircraft identification instructions. The system comprises a calling identification circuit, a radio station transmitter and audio output equipment, wherein the radio station transmitter and the audio output equipment are connected with the calling identification circuit through a radio audio wire, and the calling identification circuit is respectively connected with mode conversion equipment, audio input equipment and visual output equipment for graphical display. The system has the advantages that pilots can be reminded to watch instructions sent by air management workers, meanwhile, a calling activation system with selectable configuration is provided, and the setting or the calling identification replacement can be carried out according to the requirements of the pilots.
Description
Technical field
The utility model relates to a kind of radio navigation station and aircraft sign and order set, the system of particularly a kind of patterned radio navigation station indication and aircraft sign and instruction.
Technical background
As far as pilot and air traffic management personnel, near the airport or the spatial domain in landing area is very busy.Along with the increase of air traffic, the blank pipe staff must accurate and effective and the radio navigation station that passes through of system instruction is sent to the pilot, meanwhile, as the means that increase security, the pilot need reply the blank pipe staff.There is o lot of reasons can influence the instruction that the clear reception of pilot blank pipe personnel provide; The for example noise in the weather, pilothouse, near aircraft or the like; If owing to pilot's reason is missed radio command, make that the communication loop between pilot and the blank pipe staff interrupts.As in too busy, the driving cabin of work between noise, weather, aircraft apart from many reasons such as tensions, all can cause the pilot can not clearly receive the radio command of sending from the blank pipe staff.If in pilot and this communication loop of blank pipe staff, lose owing to the reason that is the pilot has caused radio command, a series of chain problem will take place in this.This is not only the repetition that needs the work of blank pipe staff repetitive instruction, accepts the instruction promptness but also can influence other aircraft.Existing audio-signal-driven application apparatus has the figure deixis, but the overall problem that exists is that system can not be programmed and concrete adjustment receiving circuit can not be changed.To the problems referred to above, a kind of scheme efficiently of ten minutes needs solves the pilot and loses the radio command from the blank pipe staff.
The utility model content
The purpose of the utility model is to existing technical deficiency; Call identification to radio navigation station sends is indicated in order to the image that activates on the multifunction display; The system and the method thereof of a kind of graphical display radio guidance station and aircraft sign and instruction are provided; This method can provide redundant and ensure, can remind the pilot to see the instruction of sending from the blank pipe staff.Provide simultaneously and can select the calling activation system that disposes, so just can be provided with or change call identification according to pilot's needs or custom.In addition, the ground monitoring system equally can be as the calling active mode of the same identical working method of use of aircraft.
The purpose of the utility model realizes through following technical proposals.
The system of a kind of graphical display radio guidance station and aircraft sign and instruction is characterized in that: comprise the calling identification circuit, and pass through the radio station tone frequency channel wire and call out radio station transmitter and the audio output apparatus that identification circuit links to each other; Said calling identification circuit is connected with mode switch, audio input device respectively and is used for the visual output device of display graphics.
Said calling identification circuit comprises the speech recognition integrated circuit, and the audio frequency impecance tansformer and the control transformation circuit that link to each other with the speech recognition integrated circuit respectively, and the control transformation circuit is connected with power supply; Said speech recognition integrated circuit links to each other with the visualization display driving circuit.
Said radio station transmitter has amplifier, and the radio station transmitter links to each other with the control panel of audio output apparatus.
Said audio output apparatus is loudspeaker or headset earpiece.
Said visual output device is LED lamp or Multi-Function Display curtain.
The beneficial effect of the utility model is:
Owing to taked technique scheme, make communicate by letter between blank pipe staff and the pilot become more effective, the pilot can receive the instruction of sending from the blank pipe personnel more efficiently.The blank pipe staff need not repetitive instruction work, and can not influence other aircraft acceptance instruction promptnesses.
Description of drawings
Fig. 1 is the graphical indication mechanism structured flowchart of the utility model aircraft;
Fig. 2 is that the utility model is called out the identification circuit structured flowchart.
Embodiment
Below in conjunction with specific embodiment the utility model is further specified.
As shown in Figure 1; The system of a kind of graphical display radio guidance station and aircraft sign and instruction; Comprise and call out identification circuit 104, and pass through radio station tone frequency channel wire 102 and call out the radio station transmitter 101 and audio output apparatus 103 that identification circuit 104 links to each other; Call out the visual output device 106 that identification circuit 104 is connected with mode switch 108, audio input device 107 respectively and is used for display graphics.
And then in this system, radio station transmitter 101 has amplifier, can accept the sound input from the pilot, and radio station transmitter 101 links to each other with the control panel of audio output apparatus 103.These radio stations can be connected on the audio frequency control panel, and Audio Controller for example can have one or two audio output apparatus 103: loudspeaker or headset earpiece.This audio frequency control panel can be the audio frequency control panel on the commercial aircraft that is applied to of arbitrary money.Audio output apparatus can be a loudspeaker, but generally all is that the pilot is with overhead headset earpiece.
System also comprise ground test or monitoring equipment for example the same meeting of portable wireless radio transceiver equipment or aviation monitoring equipment (occurring among the figure) to comprise radio station, radio station tone frequency channel wire and audio frequency apparatus as shown in Figure 1.
Can see that from Fig. 1 the input of the calling identification circuit 104 that comes from broadcasting station transmitter is to be connected on the broadcasting station transmitter output audio line 102.Audio output apparatus 103 is in fact mostly to be that loudspeaker is used as call circuit second input and connects.In other words, the wireless station's transmitter 101 in the integral body is connected in the audio input device 107, and input equipment just can be by the substituted audio input equipment like this.
The graphical visual output device 106 that shows is connected in the output of calling out identification circuit 104, and visual output device 106 can be one or two by LED, lamp or the Multi-Function Display curtain that the pilot was familiar with.Graphical display screen can be placed on a plurality of places, and for example in the application of aircraft, graphical display screen can be placed in the pilothouse.
Mode switch is connected to the calling identification circuit, is used for switching pattern or operator scheme are set.Mode switch can be mechanical type, touch, computer control state or the mode that can between two kinds of patterns, select arbitrarily.
The initialization of system starts from being provided with pattern.With operator scheme comparatively speaking, the calling identification circuit is keyed in and be stored in to the call identification that it is unique that " pattern is set " makes aircraft.In this scheme, pilot's role is that this call identification is input in the audio input device.Call identification can be selected by " keyboard input " or through using mouse or similar devices to press Menu key in software icon simultaneously.In tone frequency channel wire, arrive correct call identification when calling out the identification circuit monitoring, the select operating mode system gets into operating environment.
The details of calling out identification circuit is as shown in Figure 2.Speech recognition integrated circuit 205, this circuit can carry out self-adaptation according to the information of application type and read machine to be regulated.Power supply control transformation 207 is used to the power supply 209 that speech recognition circuit 205 provides, and audio frequency impecance tansformer 203 drives 211 with graphic presentation.Sound from radio station or loudspeaker is connected to audio frequency impecance tansformer 203, and the effect of sound resistance convertor is the pre-service that voice signal is provided for speech recognition circuit 205.When being activated, speech recognition circuit 205 output signals drive 211 to graphic presentation, and Signal Regulation can be provided.Special feature, if the blank pipe staff sends instruction, aircraft call identification able to programme, patterned indication can be called out identification circuit and activated.After the pilot receives the instruction of blank pipe staff transmission, access arrangement behind just corresponding aircraft self distinctive instruction the becoming sound, the call identification that comes from local audio source subsequently repeats, and closes the figure indication successively.Equally can through manual operation for example knob-operated can be used to close graphic presentation.
Claims (5)
1. the system of graphical display radio guidance station and the instruction of aircraft sign; It is characterized in that: comprise and call out identification circuit (104), and pass through radio station tone frequency channel wire (102) and call out radio station transmitter (101) and the audio output apparatus (103) that identification circuit (104) links to each other; Said calling identification circuit (104) is connected with mode switch (108), audio input device (107) respectively and is used for the visual output device (106) of display graphics.
2. the system of graphical display radio guidance station according to claim 1 and the instruction of aircraft sign; It is characterized in that: said calling identification circuit (104) comprises the speech recognition integrated circuit; And the audio frequency impecance tansformer and the control transformation circuit that link to each other with the speech recognition integrated circuit respectively, the control transformation circuit is connected with power supply; Said speech recognition integrated circuit links to each other with the visualization display driving circuit.
3. the system of graphical display radio guidance station according to claim 1 and the instruction of aircraft sign; It is characterized in that: said radio station transmitter (101) has amplifier, and radio station transmitter (101) links to each other with the control panel of audio output apparatus (103).
4. the system of graphical display radio guidance station according to claim 1 and the instruction of aircraft sign is characterized in that: said audio output apparatus (103) is loudspeaker or headset earpiece.
5. the system of graphical display radio guidance station according to claim 1 and the instruction of aircraft sign, it is characterized in that: said visual output device (106) is LED lamp or Multi-Function Display curtain.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205096888U CN202373152U (en) | 2011-12-08 | 2011-12-08 | System for graphical display of radio range station and aircraft identification instructions |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205096888U CN202373152U (en) | 2011-12-08 | 2011-12-08 | System for graphical display of radio range station and aircraft identification instructions |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202373152U true CN202373152U (en) | 2012-08-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205096888U Expired - Fee Related CN202373152U (en) | 2011-12-08 | 2011-12-08 | System for graphical display of radio range station and aircraft identification instructions |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202373152U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102855835A (en) * | 2012-10-13 | 2013-01-02 | 管存忠 | Single-board integrated voice identification light emitting diode (LED) dot matrix module |
| CN110444047A (en) * | 2018-05-04 | 2019-11-12 | 泰雷兹公司 | Method and system for assisting in flying device |
| CN111247576A (en) * | 2017-08-11 | 2020-06-05 | 联想(北京)有限公司 | Subscription information configuration |
-
2011
- 2011-12-08 CN CN2011205096888U patent/CN202373152U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102855835A (en) * | 2012-10-13 | 2013-01-02 | 管存忠 | Single-board integrated voice identification light emitting diode (LED) dot matrix module |
| CN111247576A (en) * | 2017-08-11 | 2020-06-05 | 联想(北京)有限公司 | Subscription information configuration |
| CN110444047A (en) * | 2018-05-04 | 2019-11-12 | 泰雷兹公司 | Method and system for assisting in flying device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120808 Termination date: 20141208 |
|
| EXPY | Termination of patent right or utility model |