FR3125161B1 - Display system suitable for being placed in a control station of an aircraft - Google Patents
Display system suitable for being placed in a control station of an aircraft Download PDFInfo
- Publication number
- FR3125161B1 FR3125161B1 FR2107390A FR2107390A FR3125161B1 FR 3125161 B1 FR3125161 B1 FR 3125161B1 FR 2107390 A FR2107390 A FR 2107390A FR 2107390 A FR2107390 A FR 2107390A FR 3125161 B1 FR3125161 B1 FR 3125161B1
- Authority
- FR
- France
- Prior art keywords
- display system
- control signal
- aircraft
- system suitable
- control station
- 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.)
- Active
Links
Classifications
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- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
- G06F3/14—Digital output to display device ; Cooperation and interconnection of the display device with other functional units
- G06F3/1423—Digital output to display device ; Cooperation and interconnection of the display device with other functional units controlling a plurality of local displays, e.g. CRT and flat panel display
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- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
- G06F3/14—Digital output to display device ; Cooperation and interconnection of the display device with other functional units
- G06F3/1454—Digital output to display device ; Cooperation and interconnection of the display device with other functional units involving copying of the display data of a local workstation or window to a remote workstation or window so that an actual copy of the data is displayed simultaneously on two or more displays, e.g. teledisplay
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2330/00—Aspects of power supply; Aspects of display protection and defect management
- G09G2330/02—Details of power systems and of start or stop of display operation
- G09G2330/021—Power management, e.g. power saving
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2330/00—Aspects of power supply; Aspects of display protection and defect management
- G09G2330/04—Display protection
- G09G2330/045—Protection against panel overheating
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2330/00—Aspects of power supply; Aspects of display protection and defect management
- G09G2330/08—Fault-tolerant or redundant circuits, or circuits in which repair of defects is prepared
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2330/00—Aspects of power supply; Aspects of display protection and defect management
- G09G2330/12—Test circuits or failure detection circuits included in a display system, as permanent part thereof
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2354/00—Aspects of interface with display user
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2380/00—Specific applications
- G09G2380/12—Avionics applications
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G5/00—Control arrangements or circuits for visual indicators common to cathode-ray tube indicators and other visual indicators
- G09G5/003—Details of a display terminal, the details relating to the control arrangement of the display terminal and to the interfaces thereto
- G09G5/006—Details of the interface to the display terminal
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Human Computer Interaction (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
Abstract
Système d’affichage propre à être disposé dans un poste de commande d’un aéronef L’invention concerne un système d’affichage (20) comprenant : - un écran d’affichage (22) comportant au moins deux matrices (M1, M2) ; - un calculateur graphique (24) pour générer un signal de commande local associé à chaque matrice (M1, M2) ; - un dispositif d’interface (26) configuré pour : + recevoir le signal de commande local associé à chaque matrice (M1, M2) et transmettre ledit signal de commande local à l’entrée (E1, E2) associée ; + envoyer les signaux de commandes locaux à un autre système d’affichage (20’) ; + recevoir au moins un signal de commande externe d’un autre système d’affichage (20’); et + transmettre l’au moins signal de commande externe à l’au moins une des entrées (E1, E2) de l’écran d’affichage (22) lorsque le dispositif d’interface (26) ne reçoit pas de signal de commande local. Figure pour l'abrégé : Figure 2Display system suitable for being placed in a control station of an aircraft The invention relates to a display system (20) comprising: - a display screen (22) comprising at least two matrices (M1, M2) ; - a graphics calculator (24) for generating a local control signal associated with each matrix (M1, M2); - an interface device (26) configured to: + receive the local control signal associated with each matrix (M1, M2) and transmit said local control signal to the associated input (E1, E2); + send local control signals to another display system (20’); + receive at least one external control signal from another display system (20’); and + transmit the at least external control signal to at least one of the inputs (E1, E2) of the display screen (22) when the interface device (26) does not receive a control signal local. Figure for abstract: Figure 2
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2107390A FR3125161B1 (en) | 2021-07-08 | 2021-07-08 | Display system suitable for being placed in a control station of an aircraft |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2107390A FR3125161B1 (en) | 2021-07-08 | 2021-07-08 | Display system suitable for being placed in a control station of an aircraft |
| FR2107390 | 2021-07-08 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3125161A1 FR3125161A1 (en) | 2023-01-13 |
| FR3125161B1 true FR3125161B1 (en) | 2024-04-19 |
Family
ID=77999086
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR2107390A Active FR3125161B1 (en) | 2021-07-08 | 2021-07-08 | Display system suitable for being placed in a control station of an aircraft |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR3125161B1 (en) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2843646B1 (en) | 2002-08-13 | 2004-10-29 | Thales Sa | VISUALIZATION DEVICE WITH SECURE ELECTRONIC ARCHITECTURE |
| FR2922334B1 (en) * | 2007-10-12 | 2013-02-15 | Thales Sa | DEVICE FOR VISUALIZING AN AIRCRAFT COCKPIT FOR MANAGING A VIDEO DATA NETWORK. |
| FR2974938B1 (en) * | 2011-05-05 | 2013-05-17 | Thales Sa | AVIONIC SYSTEM WITH THREE DISPLAY SCREENS FOR AN AIRCRAFT |
| KR20180055322A (en) * | 2016-11-17 | 2018-05-25 | 삼성전자주식회사 | Display device and method of controlling thereof |
| US10496351B2 (en) * | 2017-06-07 | 2019-12-03 | Ge Aviation Systems Llc | Automatic display unit backup during failures of one more display units through the utilization of graphic user interface objects defined for control transfer and reversion after resolution of the failures |
-
2021
- 2021-07-08 FR FR2107390A patent/FR3125161B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR3125161A1 (en) | 2023-01-13 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 2 |
|
| PLSC | Publication of the preliminary search report |
Effective date: 20230113 |
|
| PLFP | Fee payment |
Year of fee payment: 3 |
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| PLFP | Fee payment |
Year of fee payment: 4 |
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| PLFP | Fee payment |
Year of fee payment: 5 |