CN213545617U - Liquid crystal type electronic attitude instrument for flight simulator - Google Patents
Liquid crystal type electronic attitude instrument for flight simulator Download PDFInfo
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- CN213545617U CN213545617U CN202022843181.8U CN202022843181U CN213545617U CN 213545617 U CN213545617 U CN 213545617U CN 202022843181 U CN202022843181 U CN 202022843181U CN 213545617 U CN213545617 U CN 213545617U
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Abstract
The utility model provides a liquid crystal formula electron attitude appearance that flight simulator used belongs to the aircraft instrument field. It includes the inslot of lens embedding gauge outfit, gauge outfit and gauge stand fixed connection, the casing connecting block links to each other with the connecting plate, the second copper post links to each other with the connecting plate, nuclear core plate and data mainboard pass through first copper post fastening installation, gather mainboard and first copper post fixed connection, the LCD screen sets up between gauge stand and connecting plate, the gauge stand passes through the fastener with the connecting plate and fixes linking to each other, the casing links to each other with the connecting plate is fixed. The flight simulator is mainly characterized in that the flight speed of a real airplane is simulated, the flight simulator is applied to flight experience and training of the flight simulator, the automatic calibration function is achieved, and accurate data are provided and applied to the flight simulator. The flight training simulator is mainly applied to flight training simulators to train flight learning.
Description
Technical Field
The utility model belongs to aircraft instrument field especially relates to a liquid crystal formula electron attitude appearance that flight simulator used.
Background
The market of the current simulation simulator is continuously expanding, in order to realize higher simulation degree of the simulator under the environment, the function of the real electronic product of the airplane is researched, most of the existing ground flight simulator is an instrument used on a real aircraft, and the instrument is difficult to be matched with the flight simulator and has higher cost.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve the problem among the prior art, provide a liquid crystal formula electron attitude appearance that flight simulator used.
In order to achieve the above purpose, the utility model adopts the following technical scheme: a liquid crystal electronic attitude instrument used for a flight simulator comprises a shell, a collecting main board, a first copper column, a core board, a data main board, a second copper column, a shell connecting block, a connecting board, a liquid crystal screen, a gauge stand, a lens, an adjusting knob, a gauge head, an adjusting handle, an adjusting pointer pressing sheet and an adjusting pointer; adjust the pointer preforming and use the fastener installation fixed with adjusting the pointer, adjust knob passes through the regulation handle and links to each other with the gauge outfit, the inslot of lens embedding gauge outfit, gauge outfit and gauge stand fixed connection, the casing connecting block links to each other with the connecting plate, the second copper post links to each other with the connecting plate, nuclear core plate and data mainboard are through first copper post fastening installation, gather mainboard and first copper post fixed connection, the LCD screen sets up between gauge stand and connecting plate, the gauge stand passes through the fastener with the connecting plate and fixes linking to each other, the casing links to each other with the connecting plate is fixed.
Furthermore, the first copper column and the second copper column are both knurled copper columns.
Further, the core board is an a83T core board.
Furthermore, the liquid crystal screen is of a model TL040HDS 01-T1161A.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses a key feature lies in the flying speed of the true aircraft of simulation to be applied to the flight experience and the training of flight simulator, and have the automatic calibration function, provide accurate data and be applied to the flight simulator. Accurate data of output that can be better lets flight training truer, accurate.
Drawings
Fig. 1 is a schematic structural view of a liquid crystal electronic attitude indicator used in a flight simulator.
1-shell, 3-acquisition main board, 4-first copper column, 5-core board, 6-data main board, 7-second copper column, 8-shell connecting block, 9-connecting board, 11-liquid crystal screen, 12-gauge stand, 13-lens, 14-adjusting knob, 16-gauge outfit, 18-adjusting handle, 20-adjusting pointer pressing sheet and 21-adjusting pointer.
Detailed Description
The technical solution in the embodiment of the present invention will be clearly and completely explained below with reference to the drawings in the embodiment of the present invention.
Referring to fig. 1 to explain the present embodiment, a liquid crystal electronic attitude indicator used in a flight simulator includes a housing 1, a collection main board 3, a first copper column 4, a core board 5, a data main board 6, a second copper column 7, a housing connection block 8, a connection board 9, a liquid crystal display 11, a gauge stand 12, a lens 13, an adjusting knob 14, a gauge head 16, an adjusting handle 18, an adjusting pointer pressing sheet 20, and an adjusting pointer 21; adjust pointer preforming 20 and adjust pointer 21 and use the fastener installation fixed, adjust knob 14 links to each other with gauge outfit 16 through adjusting handle 18, lens 13 embedding gauge outfit 16's inslot, gauge outfit 16 and gauge stand 12 fixed connection, casing connecting block 8 links to each other with connecting plate 9, second copper post 7 links to each other with connecting plate 9, nuclear core plate 5 and data mainboard 6 are through first copper post 4 fastening installation, gather mainboard 3 and first copper post 4 fixed connection, LCD screen 11 sets up between gauge stand 12 and connecting plate 9, gauge stand 12 and connecting plate 9 pass through the fastener and fix and link to each other, casing 1 and connecting plate 9 are fixed and link to each other.
The main operating logic of this embodiment is to control the liquid crystal display instrument contents according to flight data communication after product start-up. Preferably, the first copper column 4 and the second copper column 7 are both knurled copper columns, the core plate 5 is an A83T core plate, and the liquid crystal screen 11 is TL040HDS01-T1161A in model number. Various flight data are controlled and displayed through the graphs, and the flight data of the upper computer are used for realizing the functions of the instrument, so that the instrument is more accurate.
The liquid crystal electronic attitude indicator used by the flight simulator provided by the utility model is introduced in detail, and the principle and the implementation mode of the utility model are explained by applying specific examples, and the description of the above examples is only used for helping to understand the method and the core idea of the utility model; meanwhile, for the general technical personnel in the field, according to the idea of the present invention, there are changes in the specific implementation and application scope, to sum up, the content of the present specification should not be understood as the limitation of the present invention.
Claims (4)
1. A liquid crystal formula electron attitude appearance that flight simulator used which characterized in that: the device comprises a shell (1), a collecting main board (3), a first copper column (4), a core board (5), a data main board (6), a second copper column (7), a shell connecting block (8), a connecting plate (9), a liquid crystal screen (11), a gauge stand (12), a lens (13), an adjusting knob (14), a gauge head (16), an adjusting handle (18), an adjusting pointer pressing sheet (20) and an adjusting pointer (21); adjust pointer preforming (20) and adjust pointer (21) and use the fastener installation fixed, adjust knob (14) link to each other with gauge outfit (16) through regulation handle (18), lens (13) embedding gauge outfit (16) inslot, gauge outfit (16) and gauge stand (12) fixed connection, casing connecting block (8) link to each other with connecting plate (9), second copper post (7) link to each other with connecting plate (9), core plate (5) and data mainboard (6) are through first copper post (4) fastening installation, gather mainboard (3) and first copper post (4) fixed connection, LCD screen (11) set up between gauge stand (12) and connecting plate (9), gauge stand (12) and connecting plate (9) are through the fastener fixed linking to each other, casing (1) and connecting plate (9) fixed linking to each other.
2. A liquid crystal electronic attitude indicator for use in a flight simulator according to claim 1, wherein: and the first copper column (4) and the second copper column (7) are both knurled copper columns.
3. A liquid crystal electronic attitude indicator for use in a flight simulator according to claim 1, wherein: the core board (5) is an A83T core board.
4. A liquid crystal electronic attitude indicator for use in a flight simulator according to claim 1, wherein: the liquid crystal screen (11) is TL040HDS01-T1161A in model number.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022843181.8U CN213545617U (en) | 2020-12-01 | 2020-12-01 | Liquid crystal type electronic attitude instrument for flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022843181.8U CN213545617U (en) | 2020-12-01 | 2020-12-01 | Liquid crystal type electronic attitude instrument for flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213545617U true CN213545617U (en) | 2021-06-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022843181.8U Active CN213545617U (en) | 2020-12-01 | 2020-12-01 | Liquid crystal type electronic attitude instrument for flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213545617U (en) |
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2020
- 2020-12-01 CN CN202022843181.8U patent/CN213545617U/en active Active
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