CN210804848U - Aircraft teaching model passenger cabin - Google Patents
Aircraft teaching model passenger cabin Download PDFInfo
- Publication number
- CN210804848U CN210804848U CN201922142643.0U CN201922142643U CN210804848U CN 210804848 U CN210804848 U CN 210804848U CN 201922142643 U CN201922142643 U CN 201922142643U CN 210804848 U CN210804848 U CN 210804848U
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- CN
- China
- Prior art keywords
- adjusting frame
- teaching model
- cabin
- rotating shaft
- driving experience
- Prior art date
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- Expired - Fee Related
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Abstract
The utility model discloses an aircraft teaching model cabin, which comprises an adjusting frame with a rectangular structure, a supporting base movably connected with one end side of the adjusting frame, a servo telescopic cylinder movably connected with the other end side of the adjusting frame and a driving experience cabin rotatably arranged on the adjusting frame; the support base is provided with a hinged seat, and the side wall of the adjusting frame close to the support base is provided with a hinged piece. In the application, the servo telescopic cylinder is regulated to lift through the control system at the other end side of the regulating frame, so that the regulating frame is driven to incline, and a driving experience cabin on the regulating frame is driven to incline up and down; on the other hand, the servo motor is adjusted by the control system at the other end side of the adjusting frame to drive the rotating shaft, so that the driving experience cabin on the rotating shaft is driven to rotate; therefore, the lifting driving mode of the cabin for driving experience is simulated.
Description
Technical Field
The utility model relates to a simulation model technical field especially relates to an aircraft teaching model passenger cabin.
Background
Conventional flight model can be used for visiting the structure of understanding the aircraft, but the model of conventional aircraft only has apparent result, and visitor can't experience the driving experience that the aircraft reverses, turns to, also can't know to some extent the mode of driving of aircraft model simultaneously, and its mode of driving is not clear enough to the flight teaching model is only to the show of outward appearance, does not compromise to its inside and mode of operation.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an aircraft teaching model passenger cabin for student or visitor carry out the experience that reverses or turn to aircraft teaching model.
In order to solve the technical problem, the utility model adopts the following technical scheme:
the utility model provides an aircraft teaching model cabin, which comprises an adjusting bracket with a rectangular structure, a supporting base movably connected with one end side of the adjusting bracket, a servo telescopic cylinder movably connected with the other end side of the adjusting bracket and a driving experience cabin rotatably arranged on the adjusting bracket; the servo telescopic cylinder is arranged on the support base, a hinge seat is arranged on the side wall, close to the support base, of the adjusting frame, a hinge piece is arranged on the hinge seat through a hinge shaft, a second hinge piece is arranged on the end side, close to the servo telescopic cylinder, of the support base, and the servo telescopic cylinder adjusts the other end side of the adjusting frame through the second hinge piece to perform lifting operation; two preformed holes are formed in the side wall of the adjusting frame along the central shaft of the adjusting frame, two ends of the rotating shaft are rotatably installed in the two preformed holes, the end portion of the rotating shaft is driven to rotate through a servo motor installed on the adjusting frame, and a driving experience cabin is fixedly installed on the rotating shaft.
Further, the hinge seat is a double-lug hinge seat.
Still further, the rotating shaft is installed in the preformed hole of the adjusting bracket through a bearing seat.
Still further, the adjusting bracket is adjusted in a lifting manner through two servo telescopic cylinders.
Still further, the servo motor drives the rotating shaft through a speed reducer.
Still further, the servo motor is fixedly arranged on the adjusting frame.
Still further, the driving experience cabin is fixed on the rotating shaft through a cabin base.
Still further, the servo motor and the servo telescopic cylinder are controlled by a control system located in the cabin.
Still further, a flying simulation seat, a control rod and a simulation picture display screen are installed in the driving experience cabin.
Still further, the adjusting bracket is of a square supporting steel frame structure, wherein the width of the adjusting bracket is larger than the rotation diameter of the driving experience cabin.
Compared with the prior art, the utility model discloses a beneficial technological effect: in the application, the servo telescopic cylinder is regulated to lift through the control system at the other end side of the regulating frame, so that the regulating frame is driven to incline, and a driving experience cabin on the regulating frame is driven to incline up and down; on the other hand, the servo motor is adjusted by the control system at the other end side of the adjusting frame to drive the rotating shaft, so that the driving experience cabin on the rotating shaft is driven to rotate; therefore, the lifting driving mode of the cockpit experiencing the driving is simulated, and the experience of reversal or steering of the aircraft teaching model by a student or a visitor is provided, so that the aircraft teaching model is applicable.
Drawings
The present invention will be further explained with reference to the following description of the drawings.
FIG. 1 is a schematic view of the main body of the aircraft teaching model cabin of the present invention;
FIG. 2 is a schematic structural diagram of the aircraft teaching model cabin of the present invention;
FIG. 3 is a schematic view of the cockpit of the aircraft teaching model cockpit of the present invention;
FIG. 4 is a schematic view of the lifting of the cockpit of the aircraft teaching model of the present invention;
figure 5 is the utility model discloses the lift schematic diagram of aircraft teaching model passenger cabin.
Description of reference numerals: 1. a support base; 101. a hinged seat; 2. an adjusting bracket; 201. an articulation member; 202. hinging a shaft; 203. reserving a hole; 3. a servo telescopic cylinder; 301. a second hinge member; 4. a driving experience cabin; 401. a cabin base; 402. a rotating shaft; 5. a servo motor.
Detailed Description
As shown in fig. 1-5, the present embodiment discloses an aircraft teaching model cockpit, which includes an adjusting frame 2 with a rectangular structure, a supporting base 1 movably connected with one end side of the adjusting frame 2, a servo telescopic cylinder 3 movably connected with the other end side of the adjusting frame 2, and a driving experience cockpit 4 rotatably disposed on the adjusting frame 2; the two sides of the support base 1 are provided with the stable ribbed plates, so that the support base 1 is supported and fixed, and the side turning and the inclination along with the support base 1 are avoided; the adjusting frame 2 is of a square supporting steel frame structure, wherein the width of the adjusting frame is larger than the rotation diameter of the driving experience cabin 4, so that the cabin can be conveniently rotated; the rotating shaft 402 is installed in a prepared hole 203 of the adjusting bracket 2 through a bearing seat; the supporting base 1 is provided with a hinge seat 101, the side wall of the adjusting bracket 2 close to the supporting base 1 is provided with a hinge 201, the hinge 201 is arranged on the hinge seat 101 through a hinge shaft 202, the end side of the supporting base 1 close to the servo telescopic cylinder 3 is provided with a second hinge 301, and the servo telescopic cylinder 3 adjusts the other end side of the adjusting bracket 2 through the second hinge 301 to perform lifting operation; two prepared holes 203 are formed in the side wall of the adjusting frame 2 along the central axis of the adjusting frame, two ends of a rotating shaft 402 are rotatably installed in the two prepared holes 203, the end of the rotating shaft 402 is driven to rotate by a servo motor 5 installed on the adjusting frame 2, and a driving experience cabin 4 is fixedly installed on the rotating shaft 402.
In this embodiment, the hinge base 101 is a double-lug hinge base, wherein a hinge hole is installed on the hinge base 101, the adjusting frame 2 is installed on the hinge base 101 through a hinge shaft 202, and the other end side of the adjusting frame 2 is adjusted in a lifting manner through two servo telescopic cylinders 3, so that the adjusting frame 2 is lifted by taking the hinge base 101 as a fulcrum, and further the action state of the aircraft operation is simulated. The servo motor 5 is fixedly installed on the adjusting frame 2, the servo motor 5 drives the rotating shaft 402 through a speed reducer, and therefore the servo motor 5 drives the driving experience cabin 4 on the rotating shaft 402 to perform lateral reversal. The driving experience cabin 4 is fixed on the rotating shaft 402 through a cabin base 401, wherein a balancing weight for balancing the driving experience cabin 4 is arranged on the lower portion of the cabin base 401 in a balancing mode, and the gravity center of the cabin base 401 is located on the rotating shaft 402. The servo motor 5 with servo telescoping cylinder 3 all controls through the control system who is located the cockpit, and wherein servo telescoping cylinder 3 is hydraulic telescoping cylinder, and wherein hydraulic telescoping cylinder's lower extreme articulates and installs the subaerial fixing base, and wherein hydraulic telescoping cylinder passes through the telescopic link and carries out when adjusting the alignment jig 2, and hydraulic telescoping cylinder also can slope thereupon, consequently utilizes the articulated fixing base of installing subaerial of hydraulic telescoping cylinder's lower extreme to play stabilizing effect. The driving experience cabin 4 is internally provided with a flying simulation seat, a control rod and a simulation picture display screen, so that the real experience feeling of an experiencer is improved conveniently.
The utility model discloses an action process:
in the application, the servo telescopic cylinder 3 is adjusted to ascend and descend through the control system at the other end side of the adjusting frame 2, so that the adjusting frame 2 is driven to incline, and the driving experience cabin 4 on the adjusting frame 2 is driven to incline up and down; on the other hand, the other end side of the adjusting frame 2 is adjusted by the control system to adjust the servo motor 5 to drive the rotating shaft, so as to drive the driving experience cabin 4 on the rotating shaft 402 to rotate; therefore, the lifting driving mode of the cabin for driving experience is simulated.
In the description of the present invention, it is to be understood that the terms "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used for convenience of description only, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention.
The above embodiments are only for describing the preferred mode of the invention, and are not intended to limit the scope of the invention, and various modifications and improvements made to the technical solution of the invention by those skilled in the art without departing from the spirit of the invention should fall within the protection scope defined by the claims of the invention.
Claims (10)
1. An aircraft teaching model cockpit, its characterized in that: the device comprises an adjusting frame (2) with a rectangular structure, a supporting base (1) movably connected with one end side of the adjusting frame (2), a servo telescopic cylinder (3) movably connected with the other end side of the adjusting frame (2) and a driving experience cabin (4) rotatably arranged on the adjusting frame (2); the supporting base (1) is provided with a hinge seat (101), the side wall of the adjusting frame (2) close to the supporting base (1) is provided with a hinge piece (201), the hinge piece (201) is installed on the hinge seat (101) through a hinge shaft (202), the end side of the supporting base (1) close to the servo telescopic cylinder (3) is provided with a second hinge piece (301), the lower end of the servo telescopic cylinder (3) is hinged and installed on a fixed seat on the bottom surface, and the servo telescopic cylinder (3) adjusts the other end side of the adjusting frame (2) through the second hinge piece (301) to perform lifting operation; two preformed holes (203) are formed in the side wall of the adjusting frame (2) along the central axis of the adjusting frame, two ends of a rotating shaft (402) are rotatably installed in the two preformed holes (203), the end of the rotating shaft (402) is driven to rotate through a servo motor (5) installed on the adjusting frame (2), and a driving experience cabin (4) is fixedly installed on the rotating shaft (402).
2. The aircraft teaching model cockpit of claim 1 wherein: the hinge seat (101) is a double-lug hinge seat.
3. The aircraft teaching model cockpit of claim 1 wherein: the rotating shaft (402) is installed in a preformed hole (203) of the adjusting frame (2) through a bearing seat.
4. The aircraft teaching model cockpit of claim 1 wherein: the adjusting frame (2) is adjusted in a lifting way through the two servo telescopic cylinders (3).
5. The aircraft teaching model cockpit of claim 1 wherein: the servo motor (5) drives the rotating shaft (402) through a speed reducer.
6. The aircraft teaching model cockpit of claim 5 wherein: the servo motor (5) is fixedly arranged on the adjusting frame (2).
7. The aircraft teaching model cockpit of claim 1 wherein: the driving experience cabin (4) is fixed on the rotating shaft (402) through a cabin base (401).
8. The aircraft teaching model cockpit of claim 1 wherein: the servo motor (5) and the servo telescopic cylinder (3) are controlled by a control system positioned in the cockpit.
9. The aircraft teaching model cockpit of claim 1 wherein: and a flying simulation seat, a control rod and a simulation picture display screen are arranged in the driving experience cabin (4).
10. The aircraft teaching model cockpit of claim 1 wherein: the adjusting frame (2) is of a square supporting steel frame structure, wherein the width of the adjusting frame is larger than the rotating diameter of the driving experience cabin (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922142643.0U CN210804848U (en) | 2019-12-04 | 2019-12-04 | Aircraft teaching model passenger cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922142643.0U CN210804848U (en) | 2019-12-04 | 2019-12-04 | Aircraft teaching model passenger cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210804848U true CN210804848U (en) | 2020-06-19 |
Family
ID=71232657
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922142643.0U Expired - Fee Related CN210804848U (en) | 2019-12-04 | 2019-12-04 | Aircraft teaching model passenger cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210804848U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114898630A (en) * | 2022-05-05 | 2022-08-12 | 信阳泰蓝仿真科技有限公司 | Situation experience type airplane test run simulator |
-
2019
- 2019-12-04 CN CN201922142643.0U patent/CN210804848U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114898630A (en) * | 2022-05-05 | 2022-08-12 | 信阳泰蓝仿真科技有限公司 | Situation experience type airplane test run simulator |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200619 Termination date: 20201204 |