CN213211400U - Airplane GPS system teaching simulator - Google Patents
Airplane GPS system teaching simulator Download PDFInfo
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- CN213211400U CN213211400U CN202022364862.6U CN202022364862U CN213211400U CN 213211400 U CN213211400 U CN 213211400U CN 202022364862 U CN202022364862 U CN 202022364862U CN 213211400 U CN213211400 U CN 213211400U
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- gps system
- gps
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Abstract
The utility model discloses an aircraft GPS system teaching simulator, including support and GPS system, wherein GPS system fixed connection is on the support, and the GPS system includes GPS computer, display, antenna, control box, the input of GPS computer links to each other with the antenna, the output of GPS computer links to each other with the display, the display still links to each other with the control box, the utility model discloses the part that will disperse each position of aircraft originally is integrated to the minizone in, and is more directly perceived simple, makes the principle that the student can better understand and the learning system.
Description
Technical Field
The utility model relates to aircraft system teaching field, especially aircraft GPS system teaching simulator.
Background
The aircraft GPS system is a technology for automatically performing integral operation to obtain instantaneous speed and instantaneous position data of an aircraft by measuring the acceleration of the aircraft, equipment is installed in the aircraft, does not depend on external information during working, does not radiate energy to the outside, is not easy to be interfered, and consists of a GPS computer, an antenna, a display and the like.
Therefore, the aircraft GPS teaching simulator is urgently needed, components originally scattered to all parts of the aircraft are integrated in a small range, the system is more visual and simple, and students can better understand and learn the principle of the system.
SUMMERY OF THE UTILITY MODEL
For overcoming the not enough of above-mentioned prior art, the utility model provides an aircraft GPS system teaching simulator teaches through using aircraft GPS system simulator, makes students know aircraft GPS system's structural component and principle more, surveyability, popular understandable.
In order to realize the purpose, the utility model discloses a technical scheme is:
aircraft GPS system teaching simulator, including support and GPS system, GPS system fixed connection is on the support, the support includes base, riser, support frame, universal wheelset, the vertical fixed connection in one side of base in bottom of support frame, the one side fixed connection of riser is in the upper portion of support frame, universal wheelset includes four universal wheels, four universal wheels are fixed connection respectively in the bottom four corners of base, GPS system fixed connection is on the riser and realizes the fixed connection of GPS system and support, GPS system includes GPS computer, display, antenna, control box, GPS computer's input links to each other with the antenna, GPS computer's output links to each other with the display, the display still links to each other with the control box.
Preferably, be equipped with power, circuit breaker one, circuit breaker two, switch, lamp, working switch, working lamp, self-checking switch in the control box, the power, circuit breaker one, circuit breaker two, switch link to each other in proper order, switch falls into three branch road, is branch road one, branch road two, branch road three respectively, be connected with the lamp on the branch road one, working switch, working lamp, display have connected gradually on the branch road two, self-checking switch has connected gradually on the branch road three, has examined the lamp.
Preferably, the display is provided with a ground terminal, and is connected to a ground terminal using a ground dedicated line lead-out.
The utility model has the advantages that:
1. the aircraft GPS system teaching simulator shows GPS relevant parts in a small range, the parts which are originally scattered to all parts of the aircraft are integrated in the small range, the system is more visual and simple, students can better understand the composition and the principle of a learning system, typical faults in actual work can be simulated, the students can carry out fault processing learning, and the better teaching purpose is achieved.
2. The aircraft GPS system teaching simulator integrates the repairing of aircraft wires, the manufacturing of the aircraft wires, the bundling of the aircraft wires, the installation of aircraft parts, the electrifying technology of an aircraft system and the like in the installation process, can restore the installation process of the system to a greater extent, and provides good display for students.
Drawings
FIG. 1 is a schematic view of the structure of the present invention;
FIG. 2 is a connection diagram of the inner parts of the control box of the present invention;
the reference symbols shown in the figures are: the device comprises a base 1, a vertical plate 2, a support frame 3, universal wheels 4, a GPS computer 5, a display 6, an antenna 7, a control box 8, a power source 801, a breaker I802, a breaker II 803, a breaker switch 804, a power switch 805, a power lamp 806, a working switch 807, a working lamp 808, a self-checking switch 809 and a checking lamp 809.
Detailed Description
The following describes the present design in detail with reference to the accompanying drawings.
As shown in fig. 1-2, aircraft GPS system teaching simulator, including support and GPS system, wherein GPS system fixed connection is on the support, and the support includes base 1, riser 2, support frame 3, universal wheelset, and the vertical fixed connection in one side of base 1 in bottom of support frame 3, and one side fixed connection in the upper portion of support frame 3 of riser 2, universal wheelset include four universal wheels 4, four universal wheels 4 are fixed connection in the bottom four corners of base 1 respectively, and wherein GPS system fixed connection is on riser 2 and realizes the fixed connection of GPS system and support, and GPS system includes GPS computer 5, display 6, antenna 7, control box 8, and the input of GPS computer 5 links to each other with antenna 7, and the output of GPS computer 5 links to each other with display 6, and display 6 still links to each other with control box 8.
The power source 801, the first circuit breaker 802, the second circuit breaker 803, the power switch 804, the power lamp 805, the working switch 806, the working lamp 807, the self-checking switch 808 and the checking lamp 809 are arranged in the control box 8, wherein the power source 801, the first circuit breaker 802, the second circuit breaker 803 and the power switch 804 are sequentially connected, the power switch 804 is divided into three branches, namely a branch I, a branch II and a branch III, the power lamp 805 is connected to the branch I, the working switch 806, the working lamp 807 and the display 6 are sequentially connected to the branch II, and the self-checking switch 808 and the checking lamp 809 are sequentially connected to the branch III.
The display 6 is provided with a ground terminal, and is connected to a ground terminal by using a ground dedicated line.
The first circuit breaker 802 and the second circuit breaker 803 can ensure that when a system fails, the fault current is cut off rapidly, so that the accident is prevented from being enlarged, and the safe operation of the system is ensured.
Examples
The teaching simulator of the airplane GPS system mainly comprises two parts of signal processing and display. The signal processing is transmitted to the GPS computer 5 through the antenna 7, and the calculation result is displayed through the display 6. The display section is composed of a display 6 and a control box 8. The power source 801 is switched on to turn on the power switch 804 and the self-checking switch 808 on the control box 8, so that the system performs self-checking, the related indicator light is lighted, the self-checking switch 808 is turned off, the working switch 806 is turned on, the display 6 displays the system interface, and the result transmitted by the GPS computer 5, namely the current longitude and latitude and the time, can be displayed.
The aircraft GPS simulator displays GPS related components in a small range, the components originally scattered to all parts of the aircraft are integrated in the small range, the simulation method is more visual and simple, working conditions and operation steps in the actual working process can be simulated, and a better teaching purpose can be achieved.
Claims (3)
1. Aircraft GPS system teaching simulator, its characterized in that, including support and GPS system, GPS system fixed connection is on the support, the support includes base, riser, support frame, universal wheelset, the vertical fixed connection in one side of base in bottom of support frame, the one side fixed connection in the upper portion of support frame of riser, universal wheelset includes four universal wheels, four universal wheels are fixed connection in the bottom four corners of base respectively, GPS system fixed connection is on the riser and realizes the fixed connection of GPS system and support, GPS system includes GPS computer, display, antenna, control box, GPS computer's input links to each other with the antenna, GPS computer's output links to each other with the display, the display still links to each other with the control box.
2. The aircraft GPS system teaching simulator according to claim 1, wherein a power supply, a first breaker, a second breaker, a power switch, a power lamp, a working switch, a working lamp, a self-checking switch and a checking lamp are arranged in the control box, the power supply, the first breaker, the second breaker and the power switch are sequentially connected, the power switch is divided into three branches, namely a first branch, a second branch and a third branch, the first branch is connected with the power lamp, the second branch is sequentially connected with the working switch, the working lamp and the display, and the third branch is sequentially connected with the self-checking switch and the checking lamp.
3. An aircraft GPS system teaching simulator according to claim 1 wherein the display is provided with a ground terminal, connected to ground using a ground dedicated line lead-out.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022364862.6U CN213211400U (en) | 2020-10-22 | 2020-10-22 | Airplane GPS system teaching simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022364862.6U CN213211400U (en) | 2020-10-22 | 2020-10-22 | Airplane GPS system teaching simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213211400U true CN213211400U (en) | 2021-05-14 |
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ID=75826488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022364862.6U Active CN213211400U (en) | 2020-10-22 | 2020-10-22 | Airplane GPS system teaching simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213211400U (en) |
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2020
- 2020-10-22 CN CN202022364862.6U patent/CN213211400U/en active Active
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