CN220064992U - Flight simulator - Google Patents
Flight simulator Download PDFInfo
- Publication number
- CN220064992U CN220064992U CN202320224451.8U CN202320224451U CN220064992U CN 220064992 U CN220064992 U CN 220064992U CN 202320224451 U CN202320224451 U CN 202320224451U CN 220064992 U CN220064992 U CN 220064992U
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- China
- Prior art keywords
- tray
- bracket
- hydraulic cylinder
- driving gear
- flight simulator
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000003014 reinforcing effect Effects 0.000 claims abstract description 24
- 230000000694 effects Effects 0.000 claims description 7
- 238000003466 welding Methods 0.000 claims description 7
- 238000005096 rolling process Methods 0.000 claims description 6
- 238000004088 simulation Methods 0.000 abstract description 10
- 239000011435 rock Substances 0.000 abstract description 3
- 230000002787 reinforcement Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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- Body Structure For Vehicles (AREA)
Abstract
The utility model discloses a flight simulator, which relates to the technical field of flight simulators and comprises the following components: the hydraulic cylinder I is connected between the tray and the reinforcing base, the connecting column is connected in the middle of the upper surface of the reinforcing base, and the connecting column is movably connected with the tray; this flight simulator through installing hydraulic cylinder one between tray and reinforcement base, goes up and down the tray through hydraulic cylinder one to the slope is connected with hydraulic cylinder two between tray and the bracket, utilizes hydraulic cylinder two to realize the oscilaltion of bracket like this, and because hydraulic cylinder two adopts the setting of slope, can effectively drive the bracket and rock, increases the range of rocking of cabin, lets the cabin be close the state of simulation more.
Description
Technical Field
The utility model relates to the technical field of flight simulators, in particular to a flight simulator.
Background
The flight simulator is dead to be used for simulating an airplane used for pilot training and is used for simulating actual conditions encountered in the flight process, so that the purpose of training is achieved, along with continuous improvement of the prior art, the flight simulator also starts to market, the flight condition is simulated through the flight simulator, the flight requirement is met, and the flight simulator is very common training equipment in the pilot training process.
The prior art can refer to the publication number: the utility model patent of CN213844443U discloses a flight simulator, which adopts a flexible cable parallel robot structure to realize large swing in the simulation flight process, namely, flexible cables replace rigid rods, so that the length constraint of the rigid rods is reduced; the lifting and rotating mechanism is added, so that the rotation and climbing in the simulated flight can be realized; on the basis of increasing functions and performances, the structure is simplified, the occupied space is reduced, and the cost is reduced. The simulation flight simulation method has the advantages that various actions and flight difficulty of the simulation flight are increased, the fidelity of the simulation flight is improved, and the sense of reality of the simulation flight is improved. And on the level of the realization of the same function, the cost is greatly reduced.
Although the flight simulator solves the problems that the prior simulation experience is limited in amplitude and cannot give the experienter an all-round better visual impact effect, the prior flight simulator has smaller overall amplitude in simulation flight training, is unfavorable for training, reduces the overall amplitude, also weakens the training effect, reduces the overall safety of the flight simulator, and is easy to cause safety accidents.
Disclosure of Invention
The utility model aims to solve the technical problems that in the prior art, the whole amplitude is smaller, the training is unfavorable, the whole amplitude is reduced, the training effect is weakened, the whole safety of the flight simulator is reduced, and safety accidents are easy to occur.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
a flight simulator, comprising:
the hydraulic cylinder I is connected between the tray and the reinforcing base, the connecting column is connected in the middle of the upper surface of the reinforcing base, and the connecting column is movably connected with the tray;
the bracket is arranged above the tray, and a second hydraulic cylinder is obliquely connected between the bracket and the tray;
the cabin body, the cabin body is installed in the top of bracket, and the lower fixed surface of cabin body has the mount pad, and the activity is provided with the roating seat between mount pad and the bracket, be fixed connection between roating seat and the bracket, and the hollow cavity is connected to the upper surface of roating seat, the internally mounted of cavity has drive gear, drive gear's one side is installed and is driven the gear, and drive gear's internal connection has the erection column.
Preferably, the bracket forms a lifting structure with the tray through a second hydraulic cylinder, and the second hydraulic cylinder is distributed in a triangular shape about the symmetrical center line of the bracket.
Preferably, the upper surface of the mounting seat is fixedly connected with the bottom of the cabin body, and the mounting seat is movably connected with the rotating seat.
Preferably, the cabin, the bracket, the tray and the reinforcing base are all positioned on the same straight line, and the surface area of the reinforcing base is larger than that of the bracket and the tray.
Preferably, the driving gear includes:
the spherical groove is fixedly formed on the surface of the driving gear;
the rolling ball is fixedly arranged at the lower end of the mounting column;
the connecting welding rod is fixedly connected to the upper end of the mounting column.
Preferably, the driving gear is in meshed connection with the driving gear, and the driving gear is connected with the lower surface of the mounting seat through a connecting welding rod connected with the upper end of the mounting column.
Preferably, the internal structure size of the spherical groove is matched with the external structure size of the rolling ball, and the spherical groove is movably connected with the lower end of the mounting column through the rolling ball.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the flight simulator, the first hydraulic cylinder is arranged between the tray and the reinforcing base, the tray is lifted through the first hydraulic cylinder, the second hydraulic cylinder is obliquely connected between the tray and the bracket, the bracket is lifted up and down by the second hydraulic cylinder, and the bracket can be effectively driven to shake due to the fact that the second hydraulic cylinder is obliquely arranged, the shaking amplitude of the cabin is increased, and the cabin is more similar to a simulated state;
2. this flight simulator, through the setting of roating seat, utilize the inside drive gear of roating seat and drive the gear and can drive the mount pad and rock, and the mount pad is connected with the bottom of the cabin body, and drive the gear and be connected with the mount pad through the erection column, be swing joint between erection column and the drive gear, utilize the rocking of spin in spherical groove, let mount pad and cabin body rock, further increase the range of rocking of cabin body.
Drawings
FIG. 1 is a schematic view of the overall structure of a flight simulator in one embodiment of the utility model;
FIG. 2 is a schematic view of a nacelle and swivel mount installation structure of a flight simulator according to one embodiment of the utility model;
FIG. 3 is a schematic view showing a split structure of a mounting base and a swivel base of a flight simulator according to an embodiment of the utility model;
fig. 4 is a schematic diagram of an exploded structure of a driving gear and a mounting post of a flight simulator according to an embodiment of the utility model.
1. Reinforcing a base; 2. a tray; 3. a connecting column; 4. a first hydraulic cylinder; 5. a bracket; 6. a second hydraulic cylinder; 7. a cabin body; 8. a mounting base; 9. a rotating seat; 901. a cavity; 902. a drive gear; 903. driving a gear; 904. a mounting column; 905. a spherical groove; 906. a rolling ball; 907. and connecting the welding rods.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, in this embodiment, a flight simulator includes: the device comprises a reinforcing base 1, wherein a tray 2 is arranged above the reinforcing base 1, a first hydraulic cylinder 4 is connected between the tray 2 and the reinforcing base 1, a connecting column 3 is connected in the middle of the upper surface of the reinforcing base 1, and the connecting column 3 is movably connected with the tray 2;
specifically, through the arrangement of the reinforcing base 1, the reinforcing base 1 is connected with the first hydraulic cylinder 4 and the tray 2, and the first hydraulic cylinder 4 is utilized to lift and adjust the tray 2, so that the vertical amplitude can be increased, the connecting column 3 is positioned in the middle of the tray 2, penetrates through the tray 2 and the tray 2, but is not fixedly connected, a gap exists between the tray 2 and the connecting column 3, and the guiding effect is mainly achieved, so that the lifting movement of the tray 2 is not influenced;
the bracket 5 is arranged above the tray 2, a second hydraulic cylinder 6 is obliquely connected between the bracket 5 and the tray 2, the bracket 5 forms a lifting structure with the tray 2 through the second hydraulic cylinder 6, and the second hydraulic cylinder 6 is distributed in a triangular shape about the symmetrical center line of the bracket 5;
specifically, through the arrangement of the second hydraulic cylinder 6, the second hydraulic cylinder 6 is connected to the edges of the bracket 5 and the tray 2, and the second hydraulic cylinder 6 adopts an inclined connection mode, so that the shaking range and amplitude of the bracket 5 can be increased, the inclined connection mode is adopted, the second hydraulic cylinder 3 is started asynchronously, shaking and swinging of the bracket 5 can be realized, the joint point between the lower end of the second hydraulic cylinder 6 and the tray 2 is a movable link, the upper end output end of the second hydraulic cylinder 6 and the bracket 5 are both in movable links, two rotation points are respectively arranged on the upper part and the lower part of each group of cylinders, the activity cannot be influenced during asynchronous starting, each two of the second hydraulic cylinders 6 is in one group, three groups of the two cylinders in each group are started synchronously, and the three groups of the two cylinders are started asynchronously, so that the lifting points are three;
the cabin body 7 is arranged above the bracket 5, the installation seat 8 is fixed on the lower surface of the cabin body 7, the rotating seat 9 is movably arranged between the installation seat 8 and the bracket 5, the upper surface of the installation seat 8 is fixedly connected with the bottom of the cabin body 7, the installation seat 8 is movably connected with the rotating seat 9, the cabin body 7, the bracket 5, the tray 2 and the reinforcing base 1 are all positioned on the same straight line, and the surface area of the reinforcing base 1 is larger than that of the bracket 5 and the tray 2;
specifically, the area of the reinforcing base 2 is enlarged, so that the area of the reinforcing base 1 is larger than the area of any structure arranged above, the stability of the bottom is improved, and the safety in the simulation training process is ensured;
the rotating seat 9 is fixedly connected with the bracket 5, the upper surface of the rotating seat 9 is connected with a hollow cavity 901, a driving gear 902 is arranged in the cavity 901, a driving gear 903 is arranged on one side of the driving gear 902, and a mounting column 904 is connected with the driving gear 903.
The driving gear 903 includes: a spherical groove 905, wherein the spherical groove 905 is fixedly arranged on the surface of the driving gear 903; a ball 906, the ball 906 being fixedly mounted at the lower end of the mounting post 904; a connection rod 907, the connection rod 907 being fixedly connected to the upper end of the mounting post 904. The driving gear 903 is engaged with the driving gear 902, and the driving gear 903 is connected with the lower surface of the mounting seat 8 through a connecting welding rod 907 connected with the upper end of the mounting column 904. The internal structure size of the ball groove 905 is matched with the external structure size of the ball 906, and the ball groove 905 is movably connected with the lower end of the mounting column 904 through the ball 906.
Specifically, through the setting of roating seat 9, utilize the setting of roating seat 9 and mount pad 8, can carry out the erection joint with cabin 7 and bracket 5, and then let cabin 7 receive bracket 5's influence to accomplish rocking to cabin 7, drive gear 903 can be driven the rotation by drive gear 902, is connected with driving motor equipment on the drive gear 902, can be used for driving drive gear 902 and rotate, increases the flexibility that drives gear 903.
Working principle: firstly, the pilot enters the cabin 7 through the ladder stand, the height of the tray 2 can be adjusted in an up-down lifting manner by utilizing the first hydraulic cylinder 4, the cabin 7 can be increased and adjusted in the up-down lifting manner, secondly, the second hydraulic cylinder 6 between the bracket 5 and the tray 2 is utilized, the second hydraulic cylinder 6 is provided with a plurality of groups and is connected in an inclined manner, so that when the bracket 5 is adjusted in the up-down manner, the bracket 5 can shake and lift in an amplitude manner, the flexibility of the cabin 7 is increased, secondly, the driving gear 902 is utilized to drive the driving gear 903 to rotate, the driving gear 902 is connected with the driving device, and then the driving gear 903 can be driven to rotate, the driving gear 903 is connected with the mounting seat 8 through the mounting column 904, the bottom of the mounting seat 8 is connected with the bottom of the cabin 7, the mounting column 904 is in movable connection with the driving gear 903, and the driving gear 903 rotates in the driving gear 903, so that the mounting column 904 is triggered to shake, the cabin 7 is caused to shake, and the cabin 7 is once swayed, so that the cabin 7 can simulate a flight state better.
Claims (7)
1. A flight simulator, comprising:
the hydraulic pressure base comprises a reinforcing base (1), wherein a tray (2) is arranged above the reinforcing base (1), a first hydraulic cylinder (4) is connected between the tray (2) and the reinforcing base (1), a connecting column (3) is connected in the middle of the upper surface of the reinforcing base (1), and the connecting column (3) is movably connected with the tray (2);
the bracket (5) is arranged above the tray (2), and a second hydraulic cylinder (6) is obliquely connected between the bracket (5) and the tray (2);
cabin body (7), the top at bracket (5) is installed in cabin body (7), and the lower fixed surface of cabin body (7) has mount pad (8), and the activity is provided with roating seat (9) between mount pad (8) and bracket (5), be fixed connection between roating seat (9) and bracket (5), and hollow cavity (901) is connected to the upper surface of roating seat (9), internally mounted of cavity (901) has driving gear (902), one side of driving gear (902) is installed and is driven gear (903), and the internal connection who drives gear (903) has erection column (904).
2. The flight simulator of claim 1, wherein: the bracket (5) forms a lifting structure between the second hydraulic cylinder (6) and the tray (2), and the second hydraulic cylinder (6) is distributed in a triangular shape relative to the symmetrical center line of the bracket (5).
3. The flight simulator of claim 1, wherein: the upper surface of the mounting seat (8) is fixedly connected with the bottom of the cabin body (7), and the mounting seat (8) is movably connected with the rotating seat (9).
4. The flight simulator of claim 1, wherein: the cabin body (7), the bracket (5), the tray (2) and the reinforcing base (1) are all positioned on the same straight line, and the surface area of the reinforcing base (1) is larger than that of the bracket (5) and the tray (2).
5. The flight simulator of claim 1, wherein:
the driving gear (903) includes:
the spherical groove (905) is fixedly formed on the surface of the driving gear (903);
a ball (906), the ball (906) being fixedly mounted at the lower end of the mounting post (904);
and a connection welding rod (907), wherein the connection welding rod (907) is fixedly connected to the upper end of the mounting column (904).
6. The flight simulator of claim 5, wherein: the driving gear (903) is in meshed connection with the driving gear (902), and the driving gear (903) is connected with the lower surface of the mounting seat (8) through a connecting welding rod (907) connected with the upper end of the mounting column (904).
7. The flight simulator of claim 5, wherein: the internal structure size of the spherical groove (905) is matched with the external structure size of the rolling ball (906), and the spherical groove (905) is movably connected with the lower end of the mounting column (904) through the rolling ball (906).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320224451.8U CN220064992U (en) | 2023-02-15 | 2023-02-15 | Flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320224451.8U CN220064992U (en) | 2023-02-15 | 2023-02-15 | Flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220064992U true CN220064992U (en) | 2023-11-21 |
Family
ID=88767379
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320224451.8U Active CN220064992U (en) | 2023-02-15 | 2023-02-15 | Flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220064992U (en) |
-
2023
- 2023-02-15 CN CN202320224451.8U patent/CN220064992U/en active Active
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