CN218848926U - Annular view device of simulation aircraft - Google Patents
Annular view device of simulation aircraft Download PDFInfo
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- CN218848926U CN218848926U CN202222481385.0U CN202222481385U CN218848926U CN 218848926 U CN218848926 U CN 218848926U CN 202222481385 U CN202222481385 U CN 202222481385U CN 218848926 U CN218848926 U CN 218848926U
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- gantry
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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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Abstract
The utility model provides an annular view device of a simulated aircraft, which comprises shading cloth, a gantry component, a projection screen, a shading curtain, a frame component, an aluminum-plastic plate and a projector component, wherein the gantry component is connected with the frame component, and the gantry component and the frame component form a 180-degree arc-shaped accommodating space; the frame assembly is respectively connected with the projection screen, the shading cloth and the aluminum-plastic panel, the projection screen and the shading cloth are sequentially distributed from top to bottom; the projector assembly is connected with the gantry assembly and used for projecting on the projection screen. The utility model discloses make the user become more convenient to the use of this equipment, just the utility model discloses a light in weight, intensity is good, and supporting connecting piece is multiple types, the assembled joint of being convenient for.
Description
Technical Field
The utility model belongs to the technical field of the relevant equipment of flight training ware, especially, relate to an annular view device of simulation aircraft.
Background
In recent years, with the rapid development of simulation technology and computer technology, the development of virtual reality technology is also dramatically striking, and it has become a popular research direction. The virtual reality technology is a high and new technology, which takes a computer graphic display technology as a core, establishes a virtual environment model through three-dimensional data of a certain range of environment, and generates a visual, auditory, tactile and even olfactory virtual environment with high reality degree in a simulation system.
Users use some hardware devices to interact with objects in the virtual environment, and the interaction is realized, so that the users can experience highly vivid three-dimensional visual sensation. The flight training simulator is a ground flight simulator, which has cabin equipment and control equipment identical to those of real airplane, and the pilot receives various kinds of flight information from the flight simulating system in the cabin and operates and controls the airplane system through judgment and decision. The virtual reality technology is used for simulating a control system, a vision system and the like of the flight simulator, so that the real immersion of the trainee can be greatly improved, and the training efficiency is obviously improved.
However, the existing simulation equipment has certain technical problems, such as complex structure, high cost, inconvenient installation and disassembly, small visual picture, poor appearance and unsatisfactory visual effect.
Disclosure of Invention
The to-be-solved problem of the utility model is to provide an annular view device of simulation aircraft, especially be fit for the user and use this equipment to carry out the training of flying to reach the result of use that realizes the immersive training.
In order to solve the technical problem, the utility model discloses a technical scheme is: the annular visual device comprises shading cloth, a gantry assembly, a projection screen, a shading curtain, a frame assembly, an aluminum-plastic panel and a projector assembly, wherein the gantry assembly is connected with the frame assembly, and the gantry assembly and the frame assembly form a 180-degree arc-shaped accommodating space; the frame assembly is respectively connected with the projection screen, the shading curtain and the aluminum-plastic panel, the projection screen and the shading curtain are sequentially distributed from top to bottom; the projector assembly is connected with the gantry assembly and used for projecting on the projection screen.
The utility model discloses in the optional embodiment, the longmen subassembly includes longmen crossbeam and two portal columns, and the both ends of longmen crossbeam are connected with corresponding portal column respectively.
Furthermore, the frame assembly comprises a plurality of supporting beams, curved beams, a projection screen supporting beam and supporting legs, wherein the supporting beams and the curved beams are arranged in number, the curved beams are sequentially connected end to form two semicircular arcs, the supporting beams are supported between the two semicircular arcs at intervals to form a semicircular structure, and the semicircular structure is used for being connected with the aluminum-plastic plate; the projection screen supporting beam is connected with the bent beam and is connected with the projection screen; the one end that the camber beam was kept away from to projection screen supporting beam is connected with the landing leg, and the landing leg has a plurality ofly and interval distribution in the one end that the camber beam was kept away from to projection screen supporting beam, and the landing leg is connected with the window shade.
In an optional implementation manner of this embodiment, the annular view device for simulating an aircraft further includes an inclined strut, and two ends of the inclined strut are respectively connected to the gantry beam and the corresponding gantry column 4.
In an optional implementation manner of this embodiment, the annular view device for simulating an aircraft further includes a plurality of first ground feet, and the first ground feet are connected with the bottom of the gantry column.
In an optional implementation manner of this embodiment, the circular viewing device for simulating an aircraft further includes a second ground foot, and the second ground foot has a plurality of ground feet and is connected with the corresponding support legs.
In an optional implementation manner of this embodiment, the circular viewing device for simulating the aircraft further comprises a handle, and the handle is connected with the projection screen support beam.
In the using process, a user firstly connects the gantry beam 2 with the gantry column profile connecting pieces and the bolts on two sides, and a plurality of first ground feet arranged at the bottom of the gantry column are supported on the ground to adapt to different ground environments, so that the gantry beam can stably stand even on a not-smooth ground; and preferably, there are ten first feet 7. After six curved beams are connected with the supporting beam, the aluminum-plastic plate is arranged in an area surrounded by the curved beams and the supporting beam, so that the aluminum-plastic plate forms a semicircular annular structure, and preferably, the bending degree of the curved beams is 60 degrees; and the camber beam is connected with six projection screen supporting beams and forms connection structure with the projection screen supporting beams for installation of the projection screen, the landing leg is connected with the projection screen supporting beams, and the landing leg and the projection screen supporting beams are provided with the window shades, so that the aluminum plastic plate, the projection screen and the window shades form a 180-degree semi-surrounding annular structure, preferably, the window shades comprise shading black cloth and shading cloth shades at the bottom.
The projector assemblies are preferably three groups, each group of projector assembly comprises a projector and a hanger, and the output of signals such as videos is performed through the host computer.
The utility model has the advantages and positive effects that: by adopting the technical scheme, the use of the equipment by a user becomes more convenient, and the utility model has the advantages of light weight, good strength, complete types of matched connecting pieces and convenient assembly and connection; just the utility model discloses a structure is retrencied, and installation and debugging are convenient, and low cost provides better immersive training facility for the training personnel.
Drawings
Fig. 1 is a schematic perspective view of an annular viewing device provided by the present invention;
fig. 2 is a left side view structure diagram of the annular viewing device provided by the present invention;
fig. 3 is a schematic top view of the annular viewing device provided by the present invention;
fig. 4 is a schematic view of the annular viewing device according to the present invention.
In the figure:
1. shading cloth 2, gantry beam 3 and inclined strut
4. Gantry column 5, projection screen 6 and window shade
7. First foot margin 8, a supporting beam 9, camber beam
10. Aluminum-plastic plate 11, projection screen supporting beam 12 and handle
13. Landing leg 14, second lower foot 15 and projector assembly
Detailed Description
As shown in fig. 1-4, the utility model relates to an annular view device of a simulated aircraft, which comprises a shading cloth 1, a gantry assembly, a projection screen 5, a shading curtain 6, a frame assembly, an aluminum-plastic panel 10 and a projector assembly 15, wherein the gantry assembly is connected with the frame assembly, and the gantry assembly and the frame assembly form a 180-degree arc-shaped accommodating space; the frame assembly is respectively connected with the projection screen 5, the shading curtain 6 and the aluminum-plastic panel 10, the projection screen 5 and the shading curtain 6 are sequentially distributed from top to bottom; the projector assembly 15 is connected to the gantry assembly, and the projector assembly 15 is used for projecting on the projection screen 5.
The utility model discloses in the optional embodiment, the longmen subassembly includes longmen crossbeam 2 and two portal columns 4, and the both ends of longmen crossbeam 2 are connected with corresponding portal column 4 respectively.
Furthermore, the frame assembly comprises a plurality of supporting beams 8, a plurality of curved beams 9, a projection screen supporting beam 11 and a plurality of supporting legs 13, wherein the supporting beams 8 and the curved beams 9 are respectively connected end to form two semicircular arcs, the supporting beams 8 are supported between the two semicircular arcs at intervals to form a semicircular structure, and the semicircular structure is used for being connected with the aluminum-plastic plate 10; the projection screen supporting beam 11 is connected with the bent beam 9, and the projection screen supporting beam 11 is connected with the projection screen 5; the end of the projection screen supporting beam 11 far away from the curved beam 9 is connected with a plurality of supporting legs 13, the supporting legs 13 are distributed at intervals at the end of the projection screen supporting beam 11 far away from the curved beam 9, and the supporting legs 13 are connected with the window shade 6.
In an optional implementation manner of this embodiment, the circular viewing device for simulating an aircraft further includes an inclined strut 3, and two ends of the inclined strut 3 are respectively connected to the gantry beam 2 and the corresponding gantry column 4.
In an optional implementation manner of this embodiment, the circular viewing device for simulating an aircraft further includes a plurality of first ground pins 7, and the first ground pins 7 are connected with the bottom of the gantry column 4.
In an optional embodiment of this embodiment, the circular viewing apparatus for simulating an aircraft further includes a second ground pin 14, and the second ground pin 14 has a plurality of legs 13 connected thereto.
In an alternative embodiment of this embodiment, the circular viewing device for simulating an aircraft further comprises a handle 12, and the handle 12 is connected to the projection screen support beam 11.
In the using process, a user firstly connects the gantry beam 2 with the gantry column 4 section bar connecting pieces and the bolts on two sides, and a plurality of first ground feet 7 arranged at the bottom of the gantry column 4 are supported on the ground to adapt to different ground environments, so that the gantry beam can stably stand even on a not-flat ground; and preferably, there are ten first feet 7. After six curved beams 9 are connected with the supporting beam 8, the aluminum-plastic plate 10 is arranged in an area surrounded by the curved beams 9 and the supporting beam 8, so that the aluminum-plastic plate 10 forms a semicircular annular structure, preferably, the bending degree of the curved beams 9 is 60 degrees; and the camber beam 9 is connected with six projection screen supporting beams 11 and forms a connection structure with the projection screen supporting beams 11 for installing the projection screen 5, the supporting leg 13 is connected with the projection screen supporting beam 11, and the supporting leg 13 and the projection screen supporting beam 11 are provided with the window shade 6, so that the aluminum-plastic panel 10, the projection screen 5 and the window shade 6 all form a 180-degree semi-surrounding ring structure, preferably, the window shade 6 comprises a shading black cloth and a shading cloth curtain at the bottom.
The projector assemblies 15 are preferably three sets, and each set of projector assembly 15 includes a projector and a hanger, and outputs video signals through the host.
While one embodiment of the present invention has been described in detail, the description is only a preferred embodiment of the present invention, and should not be considered as limiting the scope of the present invention. All the equivalent changes and improvements made according to the application scope of the present invention should still fall within the patent coverage of the present invention.
Claims (7)
1. An annular view device of simulation aircraft, its characterized in that: the device comprises shading cloth (1), a gantry assembly, a projection screen (5), a shading curtain (6), a frame assembly, an aluminum-plastic plate (10) and a projector assembly (15), wherein the gantry assembly is connected with the frame assembly, and the gantry assembly and the frame assembly form a 180-degree arc-shaped accommodating space;
the frame assembly is respectively connected with the projection screen (5), the shading curtain (6) and the aluminum-plastic panel (10), the projection screen (5) and the shading curtain (6) are sequentially distributed from top to bottom;
the projector assembly (15) is connected with the gantry assembly, and the projector assembly (15) is used for projecting on the projection screen (5).
2. A landscape annular apparatus for simulating an aircraft according to claim 1, wherein: the gantry assembly comprises a gantry beam (2) and two gantry columns (4), and two ends of the gantry beam (2) are connected with the corresponding gantry columns (4) respectively.
3. A landscape annular apparatus for simulating an aircraft according to claim 2, wherein: the frame assembly comprises a plurality of supporting beams (8), curved beams (9), a projection screen supporting beam (11) and supporting legs (13), wherein the supporting beams (8) and the curved beams (9) are arranged in a plurality, the curved beams (9) are sequentially connected end to form two semicircular arcs, the supporting beams (8) are supported between the two semicircular arcs at intervals to form a semicircular structure, and the semicircular structure is used for being connected with the aluminum-plastic plate (10);
the projection screen supporting beam (11) is connected with the curved beam (9), and the projection screen supporting beam (11) is connected with the projection screen (5);
projection curtain supporting beam (11) are kept away from the one end of camber beam (9) with landing leg (13) are connected, landing leg (13) have a plurality ofly and interval distribution be in projection curtain supporting beam (11) are kept away from the one end of camber beam (9), landing leg (13) with window shade (6) are connected.
4. A landscape annular apparatus for simulating an aircraft according to claim 2, wherein: the gantry crane further comprises an inclined strut (3), and two ends of the inclined strut (3) are respectively connected with the gantry beam (2) and the corresponding gantry column (4).
5. A landscape annular apparatus for simulating an aircraft according to claim 2, wherein: the gantry column type ground anchor is characterized by further comprising a plurality of first ground anchors (7), wherein the first ground anchors (7) are connected with the bottom of the gantry column (4).
6. A landscape annular apparatus for simulating an aircraft according to claim 3, wherein: the ground foot is characterized by further comprising a second ground foot (14), wherein the second ground foot (14) is multiple and is connected with the corresponding support leg (13).
7. A landscape annular apparatus for simulating an aircraft according to claim 3, wherein: the projection screen support beam is characterized by further comprising a handle (12), wherein the handle (12) is connected with the projection screen support beam (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222481385.0U CN218848926U (en) | 2022-09-20 | 2022-09-20 | Annular view device of simulation aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222481385.0U CN218848926U (en) | 2022-09-20 | 2022-09-20 | Annular view device of simulation aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218848926U true CN218848926U (en) | 2023-04-11 |
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ID=87307251
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222481385.0U Active CN218848926U (en) | 2022-09-20 | 2022-09-20 | Annular view device of simulation aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218848926U (en) |
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2022
- 2022-09-20 CN CN202222481385.0U patent/CN218848926U/en active Active
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