CN212112837U - Dedicated flight simulator structure - Google Patents
Dedicated flight simulator structure Download PDFInfo
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- CN212112837U CN212112837U CN202021145611.2U CN202021145611U CN212112837U CN 212112837 U CN212112837 U CN 212112837U CN 202021145611 U CN202021145611 U CN 202021145611U CN 212112837 U CN212112837 U CN 212112837U
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- 238000004088 simulation Methods 0.000 claims abstract description 13
- 239000004973 liquid crystal related substance Substances 0.000 claims abstract description 6
- 230000000694 effects Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract 1
- 238000009434 installation Methods 0.000 description 5
- 230000000007 visual effect Effects 0.000 description 3
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
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Abstract
The utility model discloses a dedicated flight simulator structure is exclusively used in the simulation flight of seiner 172 aircraft and similar model to obtain more real experience effect and the sense of immersing in flight. The flight simulator structure comprises a supporting underframe, a pedal platform arranged below the supporting underframe, a bottom plate arranged above the supporting underframe, a flight display control device arranged on the bottom plate, a view device support arranged behind the supporting underframe and a liquid crystal display screen arranged on the view device support through a screen support. Through the design, the utility model discloses flight simulator structure to the design of the 172 models of the sisner can let the user of service carry out flight simulation experience, flight science popularization, aircraft instrument operation training, trouble and special condition and deal with rehearsal etc. can show reduction training cost and furthest control training risk. Therefore, the method is suitable for popularization and application.
Description
Technical Field
The utility model relates to a flight simulator structure, specifically speaking relates to a dedicated flight simulator structure.
Background
With the rapid development of civil aviation industry in China, the opening of airspace in China and the relaxation of personal flight driving licenses, various flight experience devices and flight simulators become more concerned.
The Seiner 172 is a single engine, four-seat, small airplane, and is the most popular trainer in the world. The production of 1956 is over 42500 shelves. The sesna 172 was the small aircraft that historically produced the most successful production volumes. The airplane is firm and durable, has excellent performance, meets the requirements of civil aviation instrument flight regulations, is easy to drive and maintain, has low requirements on take-off and landing sites, and can take off and land on any slightly flat ground with the altitude of less than 3000 meters. Many flight enthusiasts use the sessile 172 as their own portal model for flight learning.
When a flight enthusiast utilizes an airplane to carry out flight training, a flight simulator is generally required to be used for simulating, and although some simulator structures are already generated at present, the problems that the experience effect is poor and the difference with the real flight experience is large exist for a special-purpose Sissner 172 airplane.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a dedicated flight simulator structure is exclusively used in the simulation flight of the seiner 172 aircraft and similar model to obtain more real experience effect and the sense of immersing in flight.
In order to achieve the above object, the utility model adopts the following technical scheme:
a special flight simulator structure comprises a supporting underframe, a pedal platform arranged below the supporting underframe, a bottom plate arranged above the supporting underframe, a flight display control device arranged on the bottom plate, a view device support arranged behind the supporting underframe, and a liquid crystal display screen arranged on the view device support through a screen support.
Further, flight display control device sets up the flight analog control system in the electric storehouse including installing the electric storehouse on the bottom plate, welds the front shroud of terminal surface before the electric storehouse to and set up rocker and on-off controller mounting hole, two multi-functional radio station panel mounting holes, autopilot panel mounting hole, throttle mounting hole and a plurality of panel board mounting hole on the front shroud.
Furthermore, the view device support comprises a vertical support fixedly connected with the supporting underframe, a cross beam support arranged on the vertical support, and expansion supports fixedly connected with the two ends of the cross beam support through connecting pieces by using cross-recessed pan head screws; and the expansion support and the beam support are both provided with screen supports.
Further, the bottom of the supporting underframe is also provided with a movable roller.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model discloses flight simulator structure to the design of the 172 models of the sisner can let the user of service carry out flight simulation experience, flight science popularization, aircraft instrument operation training, trouble and special condition and deal with rehearsal etc. can show and reduce training cost and furthest control training risk. And, the utility model discloses a simulator possesses the higher flight of immersing sense and fidelity, combines professional aviation training knowledge and flight data simultaneously, realizes the high accuracy flight simulation to the serna 172 aircraft.
Drawings
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 is a schematic top view of the present invention.
Fig. 3 is an enlarged schematic view of a portion a in fig. 2.
Wherein, the names corresponding to the reference numbers are:
1-supporting chassis, 2-pedal platform, 3-bottom plate, 4-flight display control device, 5-view bracket, 6-screen bracket, 7-liquid crystal display screen, 8-electric cabin, 9-front cover plate, 10-rocker and switch controller mounting hole, 11-multifunctional radio panel mounting hole, 12-autopilot panel mounting hole, 13-accelerator mounting hole, 14-instrument panel mounting hole, 15-vertical bracket, 16-beam bracket, 17-connecting piece, 18-expansion bracket and 19-moving roller.
Detailed Description
The present invention will be further described with reference to the following description and examples, which include but are not limited to the following examples.
Examples
As shown in fig. 1-3, the utility model discloses a dedicated flight simulator structure, including supporting chassis 1, install in the pedal platform 2 that supports chassis 1 below, set up in the bottom plate 3 that supports chassis 1 top, install flight display controlling means 4 on bottom plate 3, install in the view ware support 5 that supports chassis 1 rear to and install the liquid crystal display 7 on view ware support 5 through screen support 6. Wherein the foot platform 2 is used for mounting a flight foot rudder.
The flight display control device 4 comprises an electrical bin 8 installed on the bottom plate 3, a flight analog control system arranged in the electrical bin 8, a front cover plate 9 welded to the front end face of the electrical bin 8, and a rocker and switch controller installation hole 10, two multifunctional radio station panel installation holes 11, an autopilot panel installation hole 12, an accelerator installation hole 13 and a plurality of instrument panel installation holes 14 arranged on the front cover plate 9. The rocker and switch controller mounting hole 10 is used for mounting a flight simulation rocker and switch controller, and the accelerator mounting hole 13 is used for mounting a flight simulation accelerator. The instrument panel mounting hole mainly comprises 6 main flight instruments (height/airspeed/attitude/heading/sideslip/lifting rate), 1 tachometer, 3 navigation instruments, 4 engine/generator state instruments, 1 flight clock, 1 flap indicator and 1 trim indicator; each instrument receives instrument information from flight analog control system respectively and with information visual reality, greatly promoted flight simulator's experience effect. The multifunctional radio panel transmits data to the flight simulation control system through receiving operation.
In this embodiment, the flight simulation control system: the hardware comprises a CPU Intel I59400F, an independent display card GTX 10806G, a memory 16G, a 500G high-speed SSD solid state disk, a high-performance mainboard, a 500W power supply, a wireless 2.4G keyboard mouse and a headset. The system generates viewpoint, position, attitude, speed, acceleration, height, lifting speed, attack angle, sideslip angle data and the like of the flight simulator according to the output control instruction, and then makes corresponding display response through the display screen and the instrument.
In this embodiment, the view finder support 5 includes a vertical support 15 fixedly connected to the support chassis 1, a beam support 16 mounted on the vertical support, and an extension support 18 fixedly connected to both ends of the beam support 16 by a cross-head screw through a connection piece 17; the screen support 6 is mounted on each of the expansion support 18 and the beam support 16 and used for mounting three 24-inch LED ultra-narrow-side liquid crystal display screens, the total resolution is 5760 multiplied by 1080dpi, and the visual angle is larger than 120 degrees. And acquiring an operation instruction through the flight simulation control system, calling a corresponding imaging model in a visual database in the system, generating a corresponding real-time image, and displaying the real-time image through a display screen.
In this embodiment, the bottom of the supporting chassis 1 is further provided with a moving roller 19, which facilitates the movement of the whole device.
Through the design, the utility model discloses flight simulator structure to the design of the 172 models of the sisner can let the user of service carry out flight simulation experience, flight science popularization, aircraft instrument operation training, trouble and special condition and deal with rehearsal etc. can show reduction training cost and furthest control training risk. And, the utility model discloses a simulator possesses the higher flight of immersing sense and fidelity, combines professional aviation training knowledge and flight data simultaneously, realizes the high accuracy flight simulation to the serna 172 aircraft. Therefore, compared with the prior art, the utility model has the substantive characteristics and progress.
The above embodiment is only one of the preferred embodiments of the present invention, and should not be used to limit the protection scope of the present invention, but all the insubstantial changes or modifications made in the spirit and the idea of the main design of the present invention, the technical problems solved by the embodiment are still consistent with the present invention, and all should be included in the protection scope of the present invention.
Claims (4)
1. The utility model provides a dedicated flight simulator structure, its characterized in that, including supporting chassis (1), install in pedal platform (2) of supporting chassis (1) below, set up in bottom plate (3) of supporting chassis (1) top, install flight display controlling means (4) on bottom plate (3), install in the view ware support (5) of supporting chassis (1) rear to and install in liquid crystal display (7) on view ware support (5) through screen support (6).
2. A dedicated flight simulator structure as claimed in claim 1, characterized in that said flight display control device (4) comprises an electrical cabin (8) mounted on the bottom plate (3), a flight simulation control system disposed in the electrical cabin (8), a front cover plate (9) welded to the front end face of the electrical cabin (8), and a rocker and switch controller mounting hole (10), two multifunctional radio station panel mounting holes (11), an autopilot panel mounting hole (12), a throttle mounting hole (13) and a plurality of instrument panel mounting holes (14) disposed on the front cover plate (9).
3. A dedicated flight simulator structure according to claim 2, characterized in that the view finder support (5) comprises a vertical support (15) fixedly connected to the support chassis (1), a cross beam support (16) mounted on the vertical support, an extension support (18) fixedly connected to both ends of the cross beam support (16) by means of a cross recessed pan head screw through a connection piece (17); wherein, the screen bracket (6) is arranged on the expansion bracket (18) and the beam bracket (16).
4. A dedicated flight simulator configuration according to claim 3, characterized in that the bottom of the support chassis (1) is also provided with moving rollers (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021145611.2U CN212112837U (en) | 2020-06-19 | 2020-06-19 | Dedicated flight simulator structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021145611.2U CN212112837U (en) | 2020-06-19 | 2020-06-19 | Dedicated flight simulator structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212112837U true CN212112837U (en) | 2020-12-08 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021145611.2U Active CN212112837U (en) | 2020-06-19 | 2020-06-19 | Dedicated flight simulator structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212112837U (en) |
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2020
- 2020-06-19 CN CN202021145611.2U patent/CN212112837U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240602 Address after: Room 608, block B, 35 Changjiang South Road, Xinwu District, Wuxi City, Jiangsu Province Patentee after: Weifei Technology Co.,Ltd. Country or region after: China Address before: G41, 7th floor, angel building, 9 Gaoxin 2nd Road, Zhangba Street office, high tech Zone, Xi'an City, Shaanxi Province, 710000 Patentee before: Xi'an Weifei Simulation Technology Co.,Ltd. Country or region before: China |