CN209859358U - Simulation steering column device used in airplane simulator - Google Patents
Simulation steering column device used in airplane simulator Download PDFInfo
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- CN209859358U CN209859358U CN201920171267.5U CN201920171267U CN209859358U CN 209859358 U CN209859358 U CN 209859358U CN 201920171267 U CN201920171267 U CN 201920171267U CN 209859358 U CN209859358 U CN 209859358U
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- base
- connecting rod
- control
- concave part
- protection strip
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Abstract
The utility model relates to a simulation steering column device used in an aircraft simulator, which comprises a base, a connecting rod and a control rod, wherein the base is provided with a control mainboard, a switch button, a display lamp, a protective strip, a fixed hole and a USB interface, the control mainboard is positioned inside the base, the switch button and the display lamp are in adhesive connection, the switch button and the display lamp are positioned on one side of the base, the USB interface is positioned on the base and positioned on one side far away from the display lamp, the protective strip and the fixed hole are positioned on the upper surface of the base, the fixed hole is provided with a raised column, one end of the raised column is connected with the control mainboard through an electrical lead, the lower part of the connecting rod is provided with an inner concave part, the surface is provided with a spring, the inner concave part is connected with the raised column, the control rod is provided with a lower concave part and a control button, one end of, compared with the prior art, the device reasonable in design, stable in structure improves user experience.
Description
Technical Field
The utility model relates to a machinery, in particular to emulation steering column device that uses in aircraft simulator.
Background
Along with the development of science and technology, the aviation industry has been developed fast, and especially aircraft is because its is fast, saves time, receives passenger's favor, in order to guarantee flight safety, the pilot need do a large amount of training, and wherein simulation flight is one of them topic, often can use emulation steering column when the simulation, and present emulation steering column is because the design is unreasonable, uses for a long time, causes the structure unstable, causes emulation steering column to damage, influences user experience.
Therefore, how to provide a simulation steering column device, the device reasonable in design, stable in structure improves user experience.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an emulation steering column device that uses in aircraft simulator, the device reasonable in design, stable in structure improves user experience.
In order to solve the above technical problem, an embodiment of the present invention provides an emulation joystick device for use in an aircraft simulator, comprising a base, a connecting rod located on an upper portion of the base, and a control rod located on an upper portion of the connecting rod, wherein the base is provided with a control motherboard, a switch button, a display lamp, a protection strip, a fixing hole, and a USB interface, the control motherboard is located inside the base, the switch button and the display lamp are located on one side of the base, the USB interface is located on the base and located on a side away from the display lamp, the protection strip and the fixing hole are located on an upper surface of the base, the fixing hole is provided with a protruding column, one end of the protruding column is connected with the control motherboard through an electrical wire, the protection strip is located around the fixing hole, the base has a rectangular parallelepiped structure, the appearance of protection strip is circular structure, and both ends communicate with each other, protruding post is the cylinder structure, the connecting rod lower part is equipped with interior concave part, and the surface is equipped with the spring, interior concave part with protruding column connection, the control lever is equipped with concave part and control button down, connecting rod one end is located in the concave part down, the connecting rod with the appearance of control lever is the cylinder structure.
Compared with the prior art, the embodiment of the utility model, because the simulation steering column device used in the aircraft simulator comprises a base, a connecting rod and a control rod, a user drives the connecting rod to move through the control rod, the connecting rod contacts with a control mainboard on the base and is connected with a computer through a USB interface, the simulation control of the aircraft running direction is completed through a computer display, the protective strip and the fixed hole are positioned on the upper surface of the base, the fixed hole is provided with a convex column, the protective strip is positioned around the fixed hole, so that impurities can be prevented from entering the fixed hole, the cleanness of the fixed hole is ensured, the lower part of the connecting rod is provided with an inner concave part, the surface is provided with a spring, the inner concave part is connected with the convex column, so that the inner concave part and the convex column are connected tightly, meanwhile, the control rod is provided with a lower concave part, make things convenient for both to connect, convenient to detach simultaneously, the device reasonable in design, stable in structure because the appearance of control lever is the cylinder structure, and convenience of customers controls, improves user experience.
Further, the protection strip and the base are integrally formed or are mutually independent parts.
Further, the protection strip with when the base is the mutual independence part, both adhesive connections, because the protection strip with when the base is the mutual independence part, both adhesive connections for both connect inseparabler, and firm, avoid appearing the displacement each other.
Further, the base lower surface is equipped with the colloid gasket, just the colloid gasket with base adhesive connection, the appearance of colloid gasket is circular structure, because the colloid gasket plays the cushioning effect on the one hand, on the other hand because the appearance of colloid gasket is circular structure, can increase area of contact, avoids appearing the turn-up phenomenon.
Furthermore, the surface of the control rod is provided with a corrugated structure, so that friction can be increased due to the corrugated structure arranged on the surface of the control rod, and a user can operate the control rod conveniently.
Further, the internal diameter of the lower concave part is the same as the appearance of the connecting rod, and the internal diameter of the lower concave part is the same as the appearance of the connecting rod, so that the internal diameter of the lower concave part and the appearance of the connecting rod are in concave-convex fit, the connection between the internal diameter of the lower concave part and the appearance of the connecting rod is tight, impurities are prevented from entering the lower concave part, and the cleanness.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of the specification of the invention, illustrate exemplary embodiments of the invention and together with the description, serve to explain the principles of the invention.
Fig. 1 is a schematic structural diagram of an emulation joystick device used in an aircraft simulator according to the present invention;
FIG. 2 is a schematic cross-sectional view of a control rod of the present invention;
fig. 3 is a top view of the base of the present invention.
Description of the reference numerals
1 base 11 control mainboard
12 switch button 13 display lamp
14 fixing hole for protective strip 15
151 protruding column 16 USB interface
2 connecting rod 21 inner recess
22 spring 3 control lever
31 lower recess 32 control button
33 corrugated structure.
Detailed Description
To make the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the spirit of the present invention will be described in detail with reference to the accompanying drawings, and any person skilled in the art can change or modify the techniques taught by the present invention without departing from the spirit and scope of the present invention after understanding the embodiments of the present invention.
The exemplary embodiments and descriptions of the present invention are provided to explain the present invention, but not to limit the present invention. Additionally, the same or similar numbered elements/components used in the drawings and the embodiments are used to represent the same or similar parts.
As used herein, the terms "first," "second," …, etc. do not denote any order or sequential importance, nor are they used to limit the invention, but rather are used to distinguish one element from another or from another element or operation described in the same technical language.
With respect to directional terminology used herein, for example: up, down, left, right, front or rear, etc., are simply directions with reference to the drawings. Accordingly, the directional terminology used is intended to be illustrative and is not intended to be limiting of the present teachings.
As used herein, the terms "comprising," "including," "having," "containing," and the like are open-ended terms that mean including, but not limited to.
As used herein, "and/or" includes any and all combinations of the described items.
As used herein, the terms "substantially", "about" and the like are used to modify any slight variation in quantity or error that does not alter the nature of the variation. Generally, the range of slight variations or errors modified by such terms may be 20% in some embodiments, 10% in some embodiments, 5% in some embodiments, or other values. It should be understood by those skilled in the art that the aforementioned values can be adjusted according to actual needs, and are not limited thereto.
Certain words used to describe the present application are discussed below or elsewhere in this specification to provide additional guidance to those skilled in the art in describing the present application.
In the utility model, as shown in fig. 1, fig. 2 and fig. 3, the simulated steering column device used in the aircraft simulator comprises a base 1, a connecting rod 2 positioned on the upper part of the base 1, a control rod 3 positioned on the upper part of the connecting rod 2, wherein the base 1 is provided with a control mainboard 11, a switch button 12, a display lamp 13, a protective strip 14, a fixed hole 15 and a USB interface 16, the control mainboard 11 is positioned inside the base 1, the two are connected by viscosity, the switch button 12 and the display lamp 13 are positioned on one side of the base 1, the USB interface 16 is positioned on the base 1 and on one side far away from the display lamp 13, the protective strip 14 and the fixed hole 15 are positioned on the upper surface of the base 1, the fixed hole 15 is provided with a convex column 151, one end of the convex column 151 is connected with the control mainboard 11 by an electric lead, the protective strip 14 is positioned around the fixed hole 15, base 1 appearance is the cuboid structure, and the appearance of protection strip 14 is circular structure, and both ends communicate with each other, and protruding post 151 is the cylinder structure, and 2 lower parts of connecting rod are equipped with interior concave part 21, and the surface is equipped with spring 22, and interior concave part 21 is connected with protruding post 151, and control lever 3 is equipped with concave part 31 and control button 32 down, and 2 one end of connecting rod are located concave part 31 down, and the appearance of connecting rod 2 and control lever 3 is the cylinder structure.
Through the discovery, because the simulation steering column device used in the aircraft simulator comprises a base 1, a connecting rod 2 and a control rod 3, a user drives the connecting rod 2 to move through the control rod 3, the connecting rod 2 is contacted with a control mainboard 11 on the base 1 and is connected with a computer through a USB interface 16, the simulation control of the aircraft running direction is completed through a computer display, a protective strip 14 and a fixed hole 15 are positioned on the upper surface of the base 1, the fixed hole 15 is provided with a convex column 151, the protective strip 14 is positioned around the fixed hole 15, impurities can be prevented from entering the fixed hole 15, the cleanness of the fixed hole 15 is ensured, the lower part of the connecting rod 2 is provided with an inner concave part 21, the surface is provided with a spring 22, the inner concave part 21 is connected with the convex column 151, so that the inner concave part and the convex column are tightly connected, meanwhile, the control rod 3 is provided with a lower concave part 31, simultaneously convenient to detach, the device reasonable in design, stable in structure because the appearance of control lever 3 is the cylinder structure, convenience of customers controls, improves user experience.
In the present embodiment, when the protection strip 14 and the base 1 are mutually independent components, they are adhesively connected to each other, so that they are connected more tightly and firmly, and displacement between them is avoided, and in the practical application process, in order to make the protection strip 14 and the base 1 connected more tightly, they are designed to be integrally formed.
It should be noted that the lower surface of the base 1 is provided with a colloid gasket, the colloid gasket is in adhesive connection with the base, the colloid gasket is in a circular structure, the colloid gasket plays a role in shock absorption on the one hand, and on the other hand, because the colloid gasket is in a circular structure, the contact area can be increased, and the phenomenon of edge curling is avoided.
In addition, the surface of the control rod 3 is provided with a corrugated structure, and friction can be increased due to the corrugated structure arranged on the surface of the control rod 3, so that a user can operate the control rod conveniently.
It is worth mentioning that the inner diameter of the lower concave part 31 is the same as the appearance of the connecting rod 2, and the inner diameter of the lower concave part and the appearance of the connecting rod are in concave-convex fit, so that the lower concave part 31 is tightly connected, impurities are prevented from entering the lower concave part 31, and the lower concave part 31 is ensured to be tidy.
It will be understood by those skilled in the art that the foregoing embodiments are specific examples of the invention, and that various changes in form and details may be made therein without departing from the spirit and scope of the invention in its practical application.
Claims (6)
1. A simulated flight bar apparatus for use in an aircraft simulator, the apparatus comprising: comprises a base, a connecting rod arranged on the upper part of the base, and a control rod arranged on the upper part of the connecting rod, wherein the base is provided with a control mainboard, a switch button, a display lamp, a protection strip, a fixed hole and a USB interface, the control mainboard is arranged in the base, the switch button and the display lamp are in adhesive connection, the switch button and the display lamp are arranged on one side of the base, the USB interface is arranged on the base and is arranged on one side far away from the display lamp, the protection strip and the fixed hole are arranged on the upper surface of the base, the fixed hole is provided with a raised column, one end of the raised column is connected with the control mainboard through an electric lead, the protection strip is arranged around the fixed hole, the base is of a cuboid structure, the protection strip is of a circular structure, the two ends of the protection strip are communicated, the raised column is of a cylinder structure, and the, the surface is equipped with the spring, interior recess with protruding post connection, the control lever is equipped with concave part and control button down, connecting rod one end is located in the concave part down, the connecting rod with the appearance of control lever is the cylinder structure.
2. The simulated steering column apparatus for use in an aircraft simulator of claim 1, wherein: the protection strip and the base are integrally formed or are mutually independent parts.
3. The simulated steering column apparatus for use in an aircraft simulator of claim 2, wherein: when the protection strip and the base are mutually independent parts, the protection strip and the base are in adhesive connection.
4. The simulated steering column apparatus for use in an aircraft simulator of claim 1, wherein: the base lower surface is equipped with the colloid gasket, just the colloid gasket with base adhesive linkage, the appearance of colloid gasket is circular structure.
5. The simulated steering column apparatus for use in an aircraft simulator of claim 1, wherein: the surface of the control rod is provided with a corrugated structure.
6. The simulated steering column apparatus for use in an aircraft simulator of claim 1, wherein: the inner diameter of the lower concave part is the same as the appearance of the connecting rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920171267.5U CN209859358U (en) | 2019-01-31 | 2019-01-31 | Simulation steering column device used in airplane simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920171267.5U CN209859358U (en) | 2019-01-31 | 2019-01-31 | Simulation steering column device used in airplane simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209859358U true CN209859358U (en) | 2019-12-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920171267.5U Active CN209859358U (en) | 2019-01-31 | 2019-01-31 | Simulation steering column device used in airplane simulator |
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| CN (1) | CN209859358U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111210694A (en) * | 2020-03-03 | 2020-05-29 | 孙涛 | Aircraft simulator |
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2019
- 2019-01-31 CN CN201920171267.5U patent/CN209859358U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111210694A (en) * | 2020-03-03 | 2020-05-29 | 孙涛 | Aircraft simulator |
| CN111210694B (en) * | 2020-03-03 | 2023-01-06 | 吉林省视米科技有限公司 | Airplane simulation method |
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