CN106648484A - Cockpit instrument, HUD and aircraft component operating display system - Google Patents
Cockpit instrument, HUD and aircraft component operating display system Download PDFInfo
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- CN106648484A CN106648484A CN201510723719.2A CN201510723719A CN106648484A CN 106648484 A CN106648484 A CN 106648484A CN 201510723719 A CN201510723719 A CN 201510723719A CN 106648484 A CN106648484 A CN 106648484A
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- hud
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- power supply
- control panel
- computer
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Abstract
The invention discloses a cockpit instrument, HUD and aircraft component operating display system. The system comprises a flight data signal input module, an HUD and flight data processing computer, a projector, a synthesizer, a control panel, a bulletin panel and an airborne power supply, wherein the flight data signal input module is connected with the HUD computer, the HUD computer, the projector and the synthesizer are connected in sequence, the HUD computer is further connected with the control panel, the bulletin panel and the airborne power supply, and the control panel and the bulletin panel are also connected with the airborne power supply. The system can display the actual state of aircraft components such as an undercarriage, a horizontal tail, a vertical tail and a canopy in real time according to downloaded flight data, and also can display the accurate operating state of instruments and an HUD in an aircraft cockpit at that moment; compared with some two-dimensional static display systems, the system has obvious advantages.
Description
Technical field
The present invention relates to the real-time status technical field of aircraft components, and in particular to a kind of cockpit instrument, HUD and aircraft components operation display systems.
Background technology
For the real-time condition display of aircraft components, existing certain methods are by the way that the animation of aircraft components is made into dynamic model, then called and playing animation according to actual conditions when showing, but this method can only call the action for having made model, and it is not fine to play control.Running status for cockpit instrument and HUD shows that existing certain methods are, separately as a subwindow, two-dimentional drafting then to be carried out on window by it, and these schemes all be present not enough truly intuitively.
The content of the invention
For deficiency present on prior art, the present invention seeks to be that a kind of cockpit instrument, HUD and aircraft components operation display systems are provided, can be according to the flying quality for passing down, by each aircraft components（Such as undercarriage, tailplane, vertical tail, canopy）Virtual condition show in real time, and can show that the accurate running status of each instrument and HUD in aircraft cockpit at that time, there is obvious advantage than the display system of its some two-dimensional static.
To achieve these goals, the present invention is by the following technical solutions realizing：Cockpit instrument, HUD and aircraft components operation display systems, including flying quality signal input module, HUD and flight visual simulation computer, projecting apparatus, synthesizer, control panel, bulletin panel and airborne power supply, flying quality signal input module is connected with HUD computers, HUD computers, projecting apparatus, synthesizer are sequentially connected, described HUD computers are also connected with control panel, bulletin panel and airborne power supply, and described control panel, bulletin panel are also connected with airborne power supply.
Preferably, described HUD computers can be replaced cockpit instrument computer.
Beneficial effects of the present invention：Can be according to the flying quality for passing down, by each aircraft components（Such as undercarriage, tailplane, vertical tail, canopy）Virtual condition show in real time, and can show that the accurate running status of each instrument and HUD in aircraft cockpit at that time, there is obvious advantage than the display system of its some two-dimensional static.
Description of the drawings
With reference to the accompanying drawings and detailed description describing the present invention in detail；
Fig. 1 is the structural representation of the present invention.
Specific embodiment
Technological means, creation characteristic, reached purpose and effect to make present invention realization is easy to understand, and with reference to specific embodiment, the present invention is expanded on further.
With reference to Fig. 1, this specific embodiment is employed the following technical solutions：Cockpit instrument, HUD and aircraft components operation display systems, including flying quality signal input module 1, HUD and flight visual simulation computer 2, projecting apparatus 3, synthesizer 4, control panel 5, bulletin panel 6 and airborne power supply 7, flying quality signal input module 1 is connected with HUD computers 2, HUD computers 2, projecting apparatus 3, synthesizer 4 are sequentially connected, described HUD computers 2 are also connected with control panel 5, bulletin panel 6 and airborne power supply 7, and described control panel 5, bulletin panel 6 is also connected with airborne power supply 7.
It should be noted that described HUD computers 2 can be replaced cockpit instrument computer.
This specific embodiment adopts the aircraft components and cockpit instrument, the control method of HUD in simgear storehouses, the position of each frame all parts and the display state of attitude, the dispaly state of each instrument and HUD can in real time be calculated by flight parameter, animation control can be very accurate；Cockpit instrument is perfectly combined with model aircraft, and display form is very directly perceived；The operation rule of parameter and model is set up when model aircraft is loaded, the resource that animation is consumed is less.Simultaneously the control to realistic model running can be completed by xml document, extensibility and ease for use are very good.Due to the powerful hud script disposal abilities of the system, system can realize the HUD controls of complexity.Compared with other some flight softwares, the system conveniently has huge advantage in function and authenticity.
The general principle and principal character and advantages of the present invention of the present invention has been shown and described above.It should be understood by those skilled in the art that; the present invention is not restricted to the described embodiments; merely illustrating the principles of the invention described in above-described embodiment and specification; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements are both fallen within scope of the claimed invention.The claimed scope of the invention is by appending claims and its equivalent thereof
。
Claims (2)
1. cockpit instrument, HUD and aircraft components operation display systems, it is characterized in that, including flying quality signal input module (1), HUD and flight visual simulation are with computer (2), projecting apparatus (3), synthesizer (4), control panel (5), bulletin panel (6) and airborne power supply (7), flying quality signal input module (1) is connected with HUD computers (2), HUD computers (2), projecting apparatus (3), synthesizer (4) is sequentially connected, described HUD computers (2) also with control panel (5), bulletin panel (6) and airborne power supply (7) are connected, described control panel (5), bulletin panel (6) is also connected with airborne power supply (7).
2. cockpit instrument according to claim 1, HUD and aircraft components run display systems, it is characterised in that described HUD computers (2) can be replaced cockpit instrument computer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510723719.2A CN106648484A (en) | 2015-11-01 | 2015-11-01 | Cockpit instrument, HUD and aircraft component operating display system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510723719.2A CN106648484A (en) | 2015-11-01 | 2015-11-01 | Cockpit instrument, HUD and aircraft component operating display system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106648484A true CN106648484A (en) | 2017-05-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510723719.2A Pending CN106648484A (en) | 2015-11-01 | 2015-11-01 | Cockpit instrument, HUD and aircraft component operating display system |
Country Status (1)
| Country | Link |
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| CN (1) | CN106648484A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009251027A (en) * | 2008-04-01 | 2009-10-29 | Japan Aerospace Exploration Agency | Recurrence projection head-up display |
| CN103136979A (en) * | 2011-11-29 | 2013-06-05 | 中国商用飞机有限责任公司 | Airplane comprehensive procedural training device and throttle lever device |
| CN103809600A (en) * | 2014-03-04 | 2014-05-21 | 北京航空航天大学 | Human-machine interaction control system of unmanned airship |
| CN104656254A (en) * | 2013-11-22 | 2015-05-27 | 富士通天株式会社 | Head-Up Display Apparatus |
| CN205139895U (en) * | 2015-11-01 | 2016-04-06 | 北京军懋国兴科技股份有限公司 | Passenger cabin instrument, HUD and aircraft part operation display system |
-
2015
- 2015-11-01 CN CN201510723719.2A patent/CN106648484A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009251027A (en) * | 2008-04-01 | 2009-10-29 | Japan Aerospace Exploration Agency | Recurrence projection head-up display |
| CN103136979A (en) * | 2011-11-29 | 2013-06-05 | 中国商用飞机有限责任公司 | Airplane comprehensive procedural training device and throttle lever device |
| CN104656254A (en) * | 2013-11-22 | 2015-05-27 | 富士通天株式会社 | Head-Up Display Apparatus |
| CN103809600A (en) * | 2014-03-04 | 2014-05-21 | 北京航空航天大学 | Human-machine interaction control system of unmanned airship |
| CN205139895U (en) * | 2015-11-01 | 2016-04-06 | 北京军懋国兴科技股份有限公司 | Passenger cabin instrument, HUD and aircraft part operation display system |
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