CN210895983U - Flight simulation training device - Google Patents
Flight simulation training device Download PDFInfo
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- CN210895983U CN210895983U CN201921821595.1U CN201921821595U CN210895983U CN 210895983 U CN210895983 U CN 210895983U CN 201921821595 U CN201921821595 U CN 201921821595U CN 210895983 U CN210895983 U CN 210895983U
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- screw thread
- training platform
- flight simulation
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Abstract
The utility model discloses a flight simulation trainer, the on-line screen storage device comprises a base, the last fixed surface of base installs the pneumatic cylinder, the upper end fixedly connected with lifter plate of pneumatic cylinder, two backup pads of last fixed surface of lifter plate are connected with, the last fixed surface of backup pad installs the motor, two rotate between the backup pad and be connected with the dwang, the motor passes through drive mechanism and is connected with the dwang transmission, be equipped with screw thread and threaded connection outside the dwang and have a screw thread section of thick bamboo, it is connected with the ejector pin to rotate on the lateral wall of a screw thread section of thick bamboo, the top of dwang is equipped with the training platform, the one end of training platform is articulated with a backup pad. The utility model discloses a set up the height of the adjustable training platform of pneumatic cylinder, drive the one end jack-up or fall of ejector pin with the training platform through setting up the motor, the regulation of cooperation training platform height can make the training personnel experience the flight sense of rising, decline, advancing and moving back, and the training effect is higher.
Description
Technical Field
The utility model relates to a flight training apparatus technical field especially relates to a flight simulation trainer.
Background
With the development of science and technology, the application of the aviation aircraft is more and more extensive, so that more training personnel are needed to meet the requirement of space flight. Training of training personnel is divided into theoretical education and actual operation, the theoretical education is mainly used for learning theoretical knowledge such as aerodynamics, air navigation, aerometeorology and working principle of aerotechnical equipment, and the actual operation is used for training physical quality of the training personnel to enable the training personnel to adapt to high-altitude flight environment as soon as possible.
When training personnel, if a real aircraft is adopted, the cost is high, and certain danger is caused; the existing flight experience equipment is simple in structural design and difficult to enable trainees to obtain a real experience effect, so that the problem of how to enable the trainees to obtain real flight simulation training at low cost is continuously solved.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the problem of higher and relatively poor effect of training cost among the prior art, and the lower and effectual flight simulation trainer of a cost that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a flight simulation trainer, the on-line screen storage device comprises a base, the last fixed surface of base installs the pneumatic cylinder, the upper end fixedly connected with lifter plate of pneumatic cylinder, two backup pads of last fixed surface of lifter plate are connected with the motor, two rotate between the backup pad and be connected with the dwang, the motor passes through drive mechanism and is connected with the dwang transmission, be equipped with screw thread and threaded connection outside the dwang and have a screw thread section of thick bamboo, it is connected with the ejector pin to rotate on the lateral wall of screw thread section of thick bamboo, the top of dwang is equipped with the training platform, the one end of training platform is articulated with one of them backup pad, the other end of training platform is articulated with the upper end.
Preferably, the rotating rod is rotatably connected with the supporting plate through a rotating bearing, an outer ring of the rotating bearing is fixedly connected with the supporting plate, and an inner ring of the rotating bearing is fixedly connected with the rotating rod.
Preferably, the side wall of the threaded cylinder is rotatably connected with a rotating shaft, and the rotating shaft penetrates through the ejector rod and is rotatably connected with the ejector rod.
Preferably, a training seat is fixedly mounted on the upper surface of the training table, and a safety belt is arranged on the training seat.
Preferably, the transmission mechanism comprises a driving bevel gear which is coaxially and fixedly connected with an output shaft of the motor, a driven bevel gear is coaxially and fixedly sleeved outside the rotating rod, and the driving bevel gear is meshed with the driven bevel gear.
Compared with the prior art, the utility model discloses possess following advantage:
1. the utility model discloses a flight state of simulation aircraft comes to simulate the training personnel, has reduced the training cost, the security when having promoted flight training greatly.
2. The utility model discloses a set up the pneumatic cylinder, can drive the lifter plate and go up and down, then the height of adjustable training platform can drive the dwang through setting up the motor and rotate, drives the one end jack-up or the falling of ejector pin with the training platform then, and the regulation of cooperation training platform height can make the training personnel experience the flight sense of rising, descending, advancing and moving back, and the training effect is better.
Drawings
Fig. 1 is a schematic structural view of a flight simulation training device provided by the present invention;
fig. 2 is the utility model provides a structural schematic diagram of pivot in flight simulation trainer.
In the figure: the device comprises a base 1, a hydraulic cylinder 2, a lifting plate 3, a supporting plate 4, a motor 5, a rotating rod 6, a threaded cylinder 7, an ejector rod 8, a training table 9, a rotating bearing 10, a rotating shaft 11, a training seat 12, a driving bevel gear 13 and a driven bevel gear 14.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Referring to fig. 1-2, a flight simulation training device, including base 1, the last fixed surface of base 1 installs pneumatic cylinder 2, the model of pneumatic cylinder 2 is SD250, the upper end fixedly connected with lifter plate 3 of pneumatic cylinder 2, the last fixed surface of lifter plate 3 is connected with two backup pads 4, the last fixed surface of backup pad 4 installs motor 5, the model of motor 5 is Y2-90L, it is connected with dwang 6 to rotate between two backup pads 4, it should be noted that dwang 6 rotates with backup pad 4 through rolling bearing 10 and is connected, rolling bearing 10's outer lane and backup pad 4 fixed connection, rolling bearing 10's inner circle and dwang 6 fixed connection.
The utility model discloses in, motor 5 is connected with 6 transmissions of dwang through drive mechanism, and what need explain is that drive mechanism includes the drive bevel gear 13 with 5 coaxial fixed connection of motor output shaft, and 6 outer coaxial fixed joints of dwang have driven bevel gear 14, and drive bevel gear 13 is connected with the 14 meshing of driven bevel gear.
The utility model discloses in, dwang 6 is equipped with screw thread and threaded connection outward and has a screw thread section of thick bamboo 7, the outer screw thread of dwang 6 is coarse thread, the screw thread lead angle is greater than the vice equivalent friction angle of spiral, do not have auto-lock nature, it is connected with ejector pin 8 to rotate on the lateral wall of a screw thread section of thick bamboo 7, it is connected with pivot 11 to rotate on the lateral wall of a screw thread section of thick bamboo 7, pivot 11 runs through ejector pin 8 and rotates with ejector pin 8 and be connected, the top of dwang 6 is equipped with training platform 9, it is to explain, training platform 9's last fixed surface installs training seat 12, be equipped with the safety belt on the training seat 12, training platform 9's one end is articulated with one of them backup pad 4, training.
The utility model discloses its functional principle is explained to following mode of operation of accessible: training personnel sits on training seat 12, start hydraulic cylinder 2 drives lifter plate 3 and goes up and down, then the height of adjustable training platform 9, starter motor 5 drives drive bevel gear 13 and rotates, then drive driven bevel gear 14 with it meshing and rotate, then dwang 6 rotates, because of the unable rotation of screw thread section of thick bamboo 7, then screw thread section of thick bamboo 7 slides on dwang 6, then drive the one end jack-up or the decline of ejector pin with training platform 9, the regulation of cooperation training platform 9 height, can make training personnel experience and rise, descend, the flight sense of advancing and moving back, training effect is better, and training cost has been reduced, security when flight training has been promoted greatly.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The utility model provides a flight simulation training device, includes base (1), its characterized in that, the last fixed surface of base (1) installs pneumatic cylinder (2), the upper end fixedly connected with lifter plate (3) of pneumatic cylinder (2), the last fixed surface of lifter plate (3) is connected with two backup pads (4), the last fixed surface of backup pad (4) installs motor (5), two rotate between backup pad (4) and be connected with dwang (6), motor (5) are connected with dwang (6) transmission through drive mechanism, dwang (6) are equipped with screw thread and threaded connection has a screw thread section of thick bamboo (7) outward, it is connected with ejector pin (8) to rotate on the lateral wall of a screw thread section of thick bamboo (7), the top of dwang (6) is equipped with training platform (9), the one end of training platform (9) is articulated with one of them backup pad (4), the other end of the training platform (9) is hinged with the upper end of the mandril (8).
2. A flight simulation training device according to claim 1, wherein the rotating rod (6) is rotatably connected with the support plate (4) through a rotating bearing (10), the outer ring of the rotating bearing (10) is fixedly connected with the support plate (4), and the inner ring of the rotating bearing (10) is fixedly connected with the rotating rod (6).
3. A flight simulation training device according to claim 1, wherein a rotating shaft (11) is rotatably connected to the side wall of the threaded cylinder (7), and the rotating shaft (11) penetrates through the ejector rod (8) and is rotatably connected with the ejector rod (8).
4. A flight simulation training device according to claim 1, wherein a training seat (12) is fixedly mounted on the upper surface of the training platform (9), and a safety belt is arranged on the training seat (12).
5. A flight simulation training device according to claim 1, wherein the transmission mechanism comprises a driving bevel gear (13) coaxially and fixedly connected with the output shaft of the motor (5), a driven bevel gear (14) is coaxially and fixedly sleeved outside the rotating rod (6), and the driving bevel gear (13) is in meshed connection with the driven bevel gear (14).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921821595.1U CN210895983U (en) | 2019-10-28 | 2019-10-28 | Flight simulation training device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921821595.1U CN210895983U (en) | 2019-10-28 | 2019-10-28 | Flight simulation training device |
Publications (1)
Publication Number | Publication Date |
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CN210895983U true CN210895983U (en) | 2020-06-30 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201921821595.1U Active CN210895983U (en) | 2019-10-28 | 2019-10-28 | Flight simulation training device |
Country Status (1)
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CN (1) | CN210895983U (en) |
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2019
- 2019-10-28 CN CN201921821595.1U patent/CN210895983U/en active Active
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