CN220232593U - Flight simulation control lever of training machine - Google Patents
Flight simulation control lever of training machine Download PDFInfo
- Publication number
- CN220232593U CN220232593U CN202321674343.7U CN202321674343U CN220232593U CN 220232593 U CN220232593 U CN 220232593U CN 202321674343 U CN202321674343 U CN 202321674343U CN 220232593 U CN220232593 U CN 220232593U
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- spring
- sleeve
- pressing sleeve
- simulation control
- training machine
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- 238000004088 simulation Methods 0.000 title claims abstract description 23
- 238000003825 pressing Methods 0.000 claims abstract description 46
- 230000007246 mechanism Effects 0.000 claims description 30
- 230000000694 effects Effects 0.000 abstract description 7
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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Abstract
The utility model provides a flight simulation control rod of a training machine, which comprises the following specific steps: a fixed seat (4), a first spring (5) and a second spring (6), a top sleeve (7) and a pressing sleeve (8) are arranged in the case (1); the fixed seat (4) is fixedly arranged in the center of the bottom of the case (1); the top sleeve (7) is arranged at the top of the fixed seat (4); the first spring (5) is arranged on the top sleeve (7); the pressing sleeve (8) is pulled by the second spring (6) and is pressed on the top of the first spring (5); the number of the springs II (6) is two, one end of each spring II (6) is connected with the edge of the pressing sleeve (8), and the other end of each spring II is connected to the inner wall of the case (1) lower than the pressing sleeve (8). The utility model simulates moment by the spring and realizes resetting, has convenient use and operation, simple manufacturing process and low cost, is similar to actual combat operation in operation experience and appearance effect, and can provide good training effect.
Description
Technical Field
The utility model relates to the technical field of simulation training, in particular to a flight simulation control rod of a training machine.
Background
The helicopter is an air-heavier aircraft which takes the rotation of a rotor wing driven by an aeroengine as a lifting force and a propelling force source, can vertically rise and fall and hover in the atmosphere, and can perform controllable flying such as forward and backward flying, fixed-point rotation and the like.
In order to reduce the training cost and ensure the training safety, a helicopter is usually subjected to simulation, namely, simulation training is carried out on the training machine, so that students are familiar with the operation of each component.
Compared with other aircrafts, the control rod of the helicopter can carry out various controls such as lifting, tilting and movement on the helicopter, and is an important ring in training, so that the training effect is greatly improved if the simulation control rod is enabled to be close to actual combat in operation experience.
In patent CN202120451082.7, a helicopter simulation cycle pitch-changing rod control device is disclosed, the traditional simulation mechanism is simplified, but the structure is still more complex, and the difference between the hand feeling and the actual situation is larger, so that the training effect is poor.
Disclosure of Invention
The utility model aims to overcome the defects of the prior art, and provides a flight simulation control rod of a training machine, which is realized by the following technical scheme:
the utility model provides a flight simulation control pole of training machine, includes quick-witted case, mount pad and steering column, wherein:
the steering column is arranged at the top of the chassis through the mounting seat; the chassis is internally provided with an installation seat, a first spring, a second spring, a top sleeve and a pressing sleeve; the fixed seat is fixedly arranged in the center of the bottom of the case; the top sleeve is arranged at the top of the fixed seat; the first spring is arranged on the top sleeve; the pressing sleeve is pulled by a second spring and is pressed on the top of the first spring; the number of the second springs is two, one end of each second spring is connected with the edge of the pressing sleeve, and the other end of each second spring is connected to the inner wall of the case lower than the pressing sleeve.
Optionally or preferably, a sensor is further arranged in the case.
Optionally or preferably, a gear tooth mechanism is arranged at the bottom of the steering column; the top of the pressing sleeve is provided with a tooth-shaped structure matched with the gear tooth mechanism; when the steering column is pushed, the gear tooth mechanism drives the pressing sleeve to deflect.
Optionally or preferably, the device further comprises a limiting mechanism; the limiting mechanism is arranged above the pressing sleeve and suspended at the bottom of the mounting seat, so that the deflection angle of the pressing sleeve can be limited.
Alternatively or preferably, the number of the limiting mechanisms is two, and the limiting mechanisms are respectively arranged in the deflection directions of the steering rod and the gear tooth mechanism.
Optionally or preferably, the top sleeve and the pressing sleeve are both in a stepped round platform structure; the diameter of the upper part of the top sleeve is smaller than that of the first spring and can extend into the coil of the first spring, and the diameter of the lower part of the top sleeve is larger than that of the first spring and can support the bottom of the first spring; the diameter of the lower part of the pressing sleeve is smaller than that of the first spring and can extend into the coil of the first spring, and the diameter of the upper part of the pressing sleeve is larger than that of the first spring and can press the top of the first spring.
Based on the technical scheme, the following technical effects can be produced:
the flight simulation control rod of the training machine provided by the utility model has the advantages that the force moment is simulated by the spring, the reset is realized, the use and the operation are convenient, the manufacturing process is simple, the cost is low, the operation experience and the appearance effect are similar to actual combat operation, and the good training effect can be provided.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and other drawings may be obtained according to the structures shown in these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a top view of the present utility model;
FIG. 2 is a perspective view of the present utility model;
FIG. 3 is a left side view (interior schematic) of the present utility model;
the drawings illustrate:
the device comprises a 1-chassis, a 2-mounting seat, a 3-steering column, a 4-fixing seat, a 5-first spring, a 6-second spring, a 7-top sleeve, an 8-pressing sleeve, a 9-gear tooth mechanism and a 10-limiting mechanism.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, but not all embodiments, and the following embodiments and features of the embodiments may be combined with each other without conflict.
In a preferred embodiment:
the embodiment provides a flight simulation control rod of a training machine, as shown in fig. 1, 2 and 3, comprising a case 1, a mounting seat 2 and a driving rod 3, wherein:
the steering column 3 is arranged at the top of the chassis 1 through the mounting seat 2; a fixed seat 4, a first spring 5, a second spring 6, a top sleeve 7 and a pressing sleeve 8 are arranged in the case 1; the fixed seat 4 is fixedly arranged in the center of the bottom of the case 1; the top sleeve 7 is arranged at the top of the fixed seat 4; the first spring 5 is arranged on the top sleeve 7; the pressing sleeve 8 is pulled by the second spring 6 and is pressed on the top of the first spring 5; the number of the second springs 6 is two, one end of each second spring 6 is connected with the edge of the pressing sleeve 8, and the other end of each second spring is connected to the inner wall of the case 1 lower than the pressing sleeve 8.
Further, in this embodiment, a sensor is further disposed in the chassis 1, where the sensor is an angle sensor, and is configured to monitor angular displacement signals in a pitch direction and a roll direction, and output a position signal of the joystick through a change of an analog quantity, so as to control a posture change of the aircraft simulator.
Further, in the present embodiment, a gear tooth mechanism 9 is provided at the bottom of the steering column 3; the top of the pressing sleeve 8 is provided with a tooth-shaped structure matched with the gear tooth mechanism 9; when the steering column 3 is pushed, the pressing sleeve 8 is driven to deflect because the gear tooth mechanism 9 is kept engaged with the tooth-shaped structure;
in this embodiment, the device further comprises a limiting mechanism 10; the limiting mechanism 10 is arranged above the pressing sleeve 8 and is suspended at the bottom of the mounting seat 2, so that the deflection angle of the pressing sleeve 8 can be limited;
further, the number of the limiting mechanisms 10 is two, and the limiting mechanisms are respectively arranged in the deflection directions of the steering rod 3 and the gear tooth mechanism 9; specifically, the limiting mechanism 10 is a screw, the limiting mechanism 10 is in threaded connection with the mounting seat 2, and the deflection amplitude of the steering column 3 can be adjusted by adjusting the length extending from the mounting seat 2.
Further, in this embodiment, the top sleeve 7 and the pressing sleeve 8 are both in a stepped truncated cone structure; the diameter of the upper part of the top sleeve 7 is smaller than that of the first spring 5, the top sleeve can extend into the coil of the first spring 5, the diameter of the lower part of the top sleeve 7 is larger than that of the first spring 5, and the bottom of the first spring 5 can be supported; the diameter of the lower part of the pressing sleeve 8 is smaller than that of the first spring 5, the pressing sleeve can extend into a coil of the first spring 5, the diameter of the upper part of the pressing sleeve 8 is larger than that of the first spring 5, and the top of the first spring 5 can be pressed; the first spring 5 is pressed between the top sleeve 7 and the pressing sleeve 8, continuously supports the pressing sleeve 8, and ensures that the pressing sleeve 8 can deflect.
The working principle and flow of the flight simulation control lever of the training machine provided by the embodiment are as follows:
when a student pushes the driving rod 3 back and forth, the gear tooth mechanism 9 at the bottom of the driving rod 3 drives the pressing sleeve 8 to deflect, the first spring 5 provides support for the pressing sleeve 8, the second spring 6 provides moment simulation and enables the pressing sleeve 8 to be kept stable, the mounting seat 2 provides support for the driving rod 3, and the whole machine can be mounted on a simulation cabin.
The foregoing is merely a preferred embodiment of the utility model, and it is to be understood that the utility model is not limited to the form disclosed herein but is not to be construed as excluding other embodiments, but is capable of numerous other combinations, modifications and environments and is capable of modifications within the scope of the inventive concept, either as taught or as a matter of routine skill or knowledge in the relevant art. And that modifications and variations which do not depart from the spirit and scope of the utility model are intended to be within the scope of the appended claims.
Claims (6)
1. A flight simulation control lever of training machine, its characterized in that: including machine case (1), mount pad (2) and steering column (3), wherein:
the driving rod (3) is arranged at the top of the chassis (1) through the mounting seat (2); a fixed seat (4), a first spring (5), a second spring (6), a top sleeve (7) and a pressing sleeve (8) are arranged in the case (1); the fixed seat (4) is fixedly arranged in the center of the bottom of the case (1); the top sleeve (7) is arranged at the top of the fixed seat (4); the first spring (5) is arranged on the top sleeve (7); the pressing sleeve (8) is pulled by the second spring (6) and is pressed on the top of the first spring (5); the number of the springs II (6) is two, one end of each spring II (6) is connected with the edge of the pressing sleeve (8), and the other end of each spring II is connected to the inner wall of the chassis (1) lower than the pressing sleeve (8).
2. A flight simulation control stick of a training machine as claimed in claim 1, wherein: and a sensor is also arranged in the case (1).
3. A flight simulation control stick of a training machine as claimed in claim 1, wherein: the bottom of the driving rod (3) is provided with a gear tooth mechanism (9); the top of the pressing sleeve (8) is provided with a tooth-shaped structure matched with the gear tooth mechanism (9); when the steering column (3) is pushed, the gear tooth mechanism (9) drives the pressing sleeve (8) to deflect.
4. A flight simulation control stick of a training machine as claimed in claim 1, wherein: the device also comprises a limiting mechanism (10); the limiting mechanism (10) is arranged above the pressing sleeve (8) and is suspended at the bottom of the mounting seat (2), so that the deflection angle of the pressing sleeve (8) can be limited.
5. A flight simulation control stick for a training machine as claimed in claim 4, wherein: the number of the limiting mechanisms (10) is two, and the limiting mechanisms are respectively arranged in the deflection directions of the steering rod (3) and the gear tooth mechanism (9).
6. A flight simulation control stick of a training machine as claimed in claim 1, wherein: the top sleeve (7) and the pressing sleeve (8) are of a stepped round platform structure; the diameter of the upper part of the top sleeve (7) is smaller than that of the first spring (5), the top sleeve can extend into a coil of the first spring (5), the diameter of the lower part of the top sleeve (7) is larger than that of the first spring (5), and the bottom of the first spring (5) can be supported; the diameter of the lower part of the pressing sleeve (8) is smaller than that of the first spring (5), the pressing sleeve can extend into the coil of the first spring (5), the diameter of the upper part of the pressing sleeve (8) is larger than that of the first spring (5), and the top of the first spring (5) can be pressed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321674343.7U CN220232593U (en) | 2023-06-29 | 2023-06-29 | Flight simulation control lever of training machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321674343.7U CN220232593U (en) | 2023-06-29 | 2023-06-29 | Flight simulation control lever of training machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220232593U true CN220232593U (en) | 2023-12-22 |
Family
ID=89177735
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321674343.7U Active CN220232593U (en) | 2023-06-29 | 2023-06-29 | Flight simulation control lever of training machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220232593U (en) |
-
2023
- 2023-06-29 CN CN202321674343.7U patent/CN220232593U/en active Active
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