CN219626166U - Simulated aircraft - Google Patents
Simulated aircraft Download PDFInfo
- Publication number
- CN219626166U CN219626166U CN202321312897.2U CN202321312897U CN219626166U CN 219626166 U CN219626166 U CN 219626166U CN 202321312897 U CN202321312897 U CN 202321312897U CN 219626166 U CN219626166 U CN 219626166U
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- China
- Prior art keywords
- display
- seat
- joystick
- bedplate
- platen
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- 238000004088 simulation Methods 0.000 claims abstract description 17
- 238000004891 communication Methods 0.000 claims description 9
- 238000012549 training Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000037237 body shape Effects 0.000 description 1
- 230000001413 cellular effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
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- Devices For Indicating Variable Information By Combining Individual Elements (AREA)
Abstract
The utility model discloses a simulated aircraft, and belongs to the technical field of aircraft simulation. The seat comprises a display, a bedplate and a sliding guide rail which is arranged on the bedplate and can be used for adjusting the seat back and forth; the bottom of the seat is connected with a seat bracket which is connected with the sliding guide rail; a joystick mounted above the platen and between the display and the seat, operation of the joystick being transmitted to the flight simulation software, and operation of the joystick being reflected in the flight simulation image displayed on the display; and the trundles are arranged below the bedplate and are used for realizing the integral movement of the bedplate. According to the utility model, the display is arranged on the front side of the bedplate, the seat is arranged on the rear side of the bedplate, the operation of the operation lever is transmitted to the flight simulation software, and the operation of the operation lever is reflected in the flight simulation image displayed on the display, so that the structure is compact, the cost is low, the movement is convenient, and the flight operation can be effectively simulated.
Description
Technical Field
The utility model relates to a simulated aircraft, and belongs to the technical field of aircraft simulation.
Background
Flight simulation is a system that reproduces or simulates the flight feel of an aircraft as realistically as possible. Flight simulators range from electronic games to simulation of cabs in the same proportion driven by hydraulic or electric motors and controlled by state-of-the-art computer technology. Flight simulators have been widely used in the design and development of aircraft industry for pilot and crew training for civilian and military aircraft.
Currently, there are many mounting devices, such as computers, on the body of conventional flight simulators, but these devices are large and heavy and are not suitable for movement due to insufficient vibration resistance; on the other hand, the existing flight simulator is complicated in structure, so that the maintenance cost is high.
Thus, there is a need for a portable simulated aircraft that can be temporarily installed in a space-related school, museum, recreational facility, or the like.
Disclosure of Invention
In order to solve the above technical problems, an object of the present utility model is to provide a compact and low-cost portable analog aircraft that can be moved easily and can perform an effective analog flight operation.
The technical problems to be solved by the utility model are realized by adopting the following technical scheme:
a simulated aircraft, comprising:
the display is arranged on the front side of the bedplate through a display bracket and is used for displaying flight simulation images;
the table board is used for supporting the display and the operating lever, and a sliding guide rail capable of enabling the seat to be adjusted back and forth is arranged on the table board;
the bottom of the seat is connected with a seat bracket which is connected with the sliding guide rail;
a joystick mounted above the platen and between the display and the seat, operation of the joystick being transmitted to the flight simulation software, and operation of the joystick being reflected in the flight simulation image displayed on the display;
and the trundles are arranged below the bedplate and are used for realizing the integral movement of the bedplate.
As a preferred example, the display support is connected to the rear side of the display, the display support is fixed to the top end of the display support rod by a fixing screw, and the bottom end of the display support rod is fixed to the front side of the bedplate.
As a preferred example, the joystick includes a gimbal, a handle, a communication device support, and a connection plate, the joystick top is connected with the handle, the communication device support is provided at the side of the handle, the bottom of the joystick is connected with the gimbal, the gimbal is connected with the connection plate, the connection plate is mounted on the upper surface of the platen, and the angle and direction of the connection plate can be freely changed by the gimbal which can freely swing.
The beneficial effects of the utility model are as follows:
according to the utility model, the display is arranged on the front side of the bedplate, the seat is arranged on the rear side of the bedplate, the operation of the operation lever is transmitted to the flight simulation software, and the operation of the operation lever is reflected in the flight simulation image displayed on the display.
Drawings
FIG. 1 is a schematic overall perspective view of an embodiment of an analog aircraft;
FIG. 2 is a schematic view of a portion of a display mounted on a display stand according to an embodiment;
FIG. 3 is a schematic cross-sectional structural view of a display mounted on a display stand in an embodiment;
FIG. 4 is a schematic overall perspective view of a joystick in an embodiment;
fig. 5 is a schematic structural view of a mounting portion of the joystick in the embodiment.
In the figure:
11. a display; 12. a display stand; 13. a set screw; 14. a display support bar; 15. a platen; 151. a sliding guide rail; 16. casters; 17. a seat; 18. a seat support; 19. a joystick; 20. a universal bracket; 21. a handle; 22. a communications device cradle; 23. a foot pedal; 24. and (5) connecting a plate.
Detailed Description
Embodiments of the present utility model are described in detail below, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the drawings are exemplary only for explaining the present utility model and are not to be construed as limiting the present utility model.
In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise" indicate orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more of the described features. In the description of the present utility model, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically connected, electrically connected or can be communicated with each other; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
In the present utility model, unless expressly stated or limited otherwise, a first feature "above" or "below" a second feature may include both the first and second features being in direct contact, as well as the first and second features not being in direct contact but being in contact with each other through additional features therebetween. Moreover, a first feature being "above," "over" and "on" a second feature includes the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is higher in level than the second feature. The first feature being "under", "below" and "beneath" the second feature includes the first feature being directly under and obliquely below the second feature, or simply means that the first feature is less level than the second feature.
The following disclosure provides many different embodiments, or examples, for implementing different features of the utility model. In order to simplify the present disclosure, components and arrangements of specific examples are described below. They are, of course, merely examples and are not intended to limit the utility model. Furthermore, the present utility model may repeat reference numerals and/or letters in the various examples, which are for the purpose of brevity and clarity, and which do not themselves indicate the relationship between the various embodiments and/or arrangements discussed.
Fig. 1 shows an embodiment of a portable flight simulator of the utility model.
In this figure, a display 11 for displaying a flight simulation image is shown, and casters 16 are provided on the lower surface of the display 11, and casters 16 are provided on the front surface through a movable platen 15. A pair of monitor support bars 14 disposed at a left-right interval, the monitor support bars 14 standing on the front side of the platen 15 in a state of being inclined backward.
Further, a seat frame 18 to which the seat 17 is mounted is provided at the rear of the platen 15, and the front end of the seat frame 18 is fitted into a slide rail 151 formed on the upper surface of the platen 15. As shown in fig. 1, the seat support 18 is capable of sliding. With this slide mechanism, the seat 17 can be moved back and forth toward a lever 19 described later in accordance with the body shape of an operator or the like.
Further, reference numeral 19 denotes a lever type joystick standing on the upper surface of the pedal 15 via a gimbal 20, and a handle 21 operated by an operator is freely attached to the end portion thereof. Reference numeral 22 denotes a communication device holder, and the communication device holder 22 contains a communication device to be assembled according to the operation of the handle 21, such as a cellular phone or the like, which is mounted on the handle 21 or the joystick 19.
Accordingly, when the operator sits on the seat 17 and holds the handgrip 21 of the joystick 19 and operates according to the flight simulation image displayed on the display 11, the communication device performs flight simulation according to the operation of the handgrip 21, the manipulation motion is transmitted to the simulated flight software, and the operation state is reflected on the image of the flight simulation, and the flight simulation is performed.
Reference numeral 23 in the drawing is a pedal plate 23 for operating the pair of display support rods 14 mounted on the left and right. The foot pedal 23 controls the rudder, i.e. the heading of the aircraft, to rotate about a vertical axis when in operation in the air. And the control rod 19 is pushed forwards and pulled backwards, and is biased left and right to control pitching and rolling left and right of the simulated aircraft respectively, so that the simulated aircraft rotates around the transverse axis and the longitudinal axis respectively.
Fig. 2 and 3 show a state in which the monitor bracket 12 is fitted to the connection portion of the monitor support bar 14 and is fixed by the fixing screw 13.
By adopting the above-described structure, the display 11 can be mounted on the display stand 14 and dismounted from the display stand 14 in one-touch.
Fig. 4 and 5 show details of the lever 19.
That is, the lever 19 is mounted on the upper surface of the step 15 via the connection plate 24, and its angle and direction can be freely changed by the freely swingable gimbal 20.
In the present utility model, it is emphasized that it is used as a portable flight simulator (simple mobile ground simulation flight experience device), but various schools, work experience activities, museums, etc. unless the gist of the present utility model is changed. That is, it can be used for flight training, education, etc., in addition to simulated flight in entertainment facilities.
In the description of the present specification, reference to the terms "certain embodiments," "one embodiment," "some embodiments," "an exemplary embodiment," "an example," "a particular example," or "some examples" means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present utility model. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiments or examples. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include at least one such feature. In the description of the present utility model, the meaning of "plurality" means at least two, for example, two, three, unless specifically defined otherwise.
Although embodiments of the present utility model have been shown and described above, it will be understood that the above embodiments are illustrative and not to be construed as limiting the utility model, and that variations, modifications, alternatives and variations may be made to the above embodiments by those skilled in the art within the scope of the utility model, which is defined by the claims and their equivalents.
Claims (3)
1. A simulated aircraft, comprising:
a display (11) mounted on the front side of the platen (15) through a display bracket (12) for displaying a flight simulation image;
a platen (15) for supporting the display (11) and the joystick (19), wherein a slide rail (151) capable of adjusting the seat (17) back and forth is arranged on the platen (15);
the bottom of the seat (17) is connected with a seat bracket (18), and the seat bracket (18) is connected with a sliding guide rail (151);
a joystick (19) mounted above the platen (15) and between the display (11) and the seat (17), the operation of the joystick (19) being transmitted to the flight simulation software, and the operation of the joystick (19) being reflected in the flight simulation image displayed on the display (11);
and a caster (16) mounted below the platen (15) for effecting the overall movement of the platen (15).
2. A simulated aircraft according to claim 1, wherein a display bracket (12) is connected to the rear side of the display (11), the display bracket (12) is fixed to the top end of a display support rod (14) by a fixing screw, and the bottom end of the display support rod (14) is fixed to the front side of the bedplate (15).
3. A simulated aircraft according to claim 1, characterized in that the lever (19) comprises a gimbal (20), a handle (21), a communication device support (22) and a connection plate (24), the lever (19) top is connected with the handle (21), the communication device support (22) is provided beside the handle (21), the bottom end of the lever (19) is connected with the gimbal (20), the gimbal (20) is connected with the connection plate (24), the connection plate (24) is mounted on the upper surface of the bedplate (15), and the angle and direction of the connection plate (24) can be freely changed by the gimbal (20) capable of freely swinging.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202321312897.2U CN219626166U (en) | 2023-05-26 | 2023-05-26 | Simulated aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202321312897.2U CN219626166U (en) | 2023-05-26 | 2023-05-26 | Simulated aircraft |
Publications (1)
Publication Number | Publication Date |
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CN219626166U true CN219626166U (en) | 2023-09-01 |
Family
ID=87791406
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202321312897.2U Active CN219626166U (en) | 2023-05-26 | 2023-05-26 | Simulated aircraft |
Country Status (1)
Country | Link |
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CN (1) | CN219626166U (en) |
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2023
- 2023-05-26 CN CN202321312897.2U patent/CN219626166U/en active Active
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