CN220164187U - Portable aircraft simulation test stand - Google Patents
Portable aircraft simulation test stand Download PDFInfo
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- CN220164187U CN220164187U CN202321958916.9U CN202321958916U CN220164187U CN 220164187 U CN220164187 U CN 220164187U CN 202321958916 U CN202321958916 U CN 202321958916U CN 220164187 U CN220164187 U CN 220164187U
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- simulation test
- aircraft simulation
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- 238000012360 testing method Methods 0.000 title claims abstract description 42
- 238000004088 simulation Methods 0.000 title claims abstract description 30
- 230000000694 effects Effects 0.000 abstract description 20
- 230000003028 elevating effect Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012549 training Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
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Abstract
The utility model discloses a convenient airplane simulation test bed, which relates to the technical field of airplane simulation test beds, and comprises a base, wherein the top end of the base is fixedly connected with a lifting device, one end of the lifting device is fixedly connected with a rotating device, the rotating device comprises a first motor and a vertical plate, the output end of the first motor penetrates through one end of the vertical plate to be fixedly connected with a first gear, one end of the first gear, which is opposite to the first motor, is fixedly connected with a connecting rod, one end of the connecting rod, which is opposite to the first gear, is fixedly connected with a support, one side inner wall of the support is rotationally connected with a first rotating rod, one end of the support is penetrated with a second rotating rod, one end of the second rotating rod is fixedly connected with a belt pulley, one end of the first gear is meshed with the second gear, the effect that the airplane simulation test bed has an omnibearing rotating function is achieved through the rotating device, and the lifting capability of the airplane can be tested through the lifting device.
Description
Technical Field
The utility model relates to the technical field of aircraft simulation test tables, in particular to a convenient aircraft simulation test table.
Background
Before the aircraft is put into operation, in order to ensure the safety of the aircraft, a simulation experiment is required to be carried out on the structural strength of the aircraft, and whether the bearing capacity of the aircraft meets the requirements is obtained through the simulation experiment, so that the aircraft is required to be controlled in five degrees of freedom (yaw, pitch, roll, lift and translation) in hanging and posture, and a test bed is required to test the aircraft.
The prior art also has the following problems:
firstly, the existing aircraft simulation training platform does not have the function of omnibearing rotation, and cannot rotate in omnibearing in the simulation experiment process of an aircraft using test platform, so that the aircraft testing performance is incomplete, and the service efficiency of the aircraft simulation test platform is reduced.
Secondly, the existing aircraft simulation training platform does not have a lifting function, and because the aircraft has a lifting process in the flight process, the test platform does not have a lifting device, so that the lifting resistance of the aircraft cannot be tested when the aircraft is tested, and the idealization of the aircraft test platform cannot be achieved.
In view of the above problems, the inventors propose a portable aircraft simulation test stand for solving the above problems.
Disclosure of Invention
In order to solve the problems of the omnibearing rotation function and the lifting function of the aircraft test bed; the utility model aims to provide a convenient airplane simulation test bed.
In order to solve the technical problems, the utility model adopts the following technical scheme: the utility model provides a convenient type aircraft simulation test platform, includes the base, the bottom fixedly connected with four support columns of base, the support column plays the effect of supporting the base, and the equal fixedly connected with in bottom of four support columns stops the wheel of stopping, stops the wheel of stopping and plays the effect of conveniently removing aircraft simulation test platform, four it is rectangular array to stop the wheel of stopping and distributes, the top fixedly connected with elevating gear of base, elevating gear plays the effect of elevating gear's cabin body, elevating gear's one end fixedly connected with rotary device, rotary device plays the effect that makes the cabin body realize all-round rotation, rotary device includes first motor and riser, and first motor plays the effect of drive rotary device, the bottom fixedly connected with first motor seat of first motor, and the one end fixed connection of riser of first motor seat, the output end of first motor runs through the one end fixedly connected with first gear of riser, makes things convenient for the output end of first motor to drive first gear rotation, the one end fixedly connected with rotary rod of first gear back to the first motor, the gear back to the rack is equipped with the connecting rod, the gear is equipped with the gear rack is connected with the first end, the rack is equipped with the first rotary connection, the first rack is equipped with the first rack is connected with the first rack, the first rack is equipped with the first rack, and the first rack is equipped with the rack, one end fixedly connected with round bar of second gear, the one end fixedly connected with belt pulley of round bar dorsad second gear makes things convenient for the first gear to drive the belt pulley rotation, two the belt has been cup jointed jointly to the surface of belt pulley, makes one of them belt pulley drive another belt pulley rotation through the belt pulley to play the rotatory effect of drive cabin body.
Preferably, elevating gear includes the second motor, and the second motor plays drive elevating gear's effect, top one side fixedly connected with backup pad of base, backup pad start-up support's effect, the backup pad is "L" type, the output of second motor runs through the first bevel gear of one end lower part fixedly connected with of backup pad, makes things convenient for the output of second motor to drive the rotatory effect of first bevel gear, the top meshing of first bevel gear is connected with the second bevel gear, plays first bevel gear rotatory effect of driving the second bevel gear, the top fixedly connected with threaded rod of second bevel gear, makes things convenient for the second bevel gear rotatory to drive the threaded rod rotatory, and the one end of threaded rod dorsad second bevel gear rotates with the top internal surface of backup pad to be connected, the surface of threaded rod has cup jointed the slider, and the one end of slider and the one end lower part fixedly connected with of riser play the slider and remove the effect that the riser, the spout that the cooperation slider used has been seted up to the one end of backup pad, the bottom fixedly connected with second motor base of second motor, the bottom fixedly connected with second motor base of second motor base and the bottom fixedly connected with bottom of second motor base.
Compared with the prior art, the utility model has the beneficial effects that:
the utility model starts the first motor by arranging the rotating device, the output end of the first motor drives the first gear to rotate, the first gear drives the bracket to rotate, meanwhile, the first gear is matched with the second gear to be used, the belt pulley is driven to rotate, and the belt pulley drives the second rotating rod to rotate, so that the effect that the aircraft simulation test bed has an omnibearing rotating function is achieved, and the use efficiency of the aircraft simulation test bed is improved;
2, the lifting device is arranged, the second motor is started, the output end of the second motor drives the first bevel gear to rotate, the second bevel gear is matched with the first bevel gear to drive the threaded rod to rotate, and the threaded rod is matched with the sliding block to use, so that the function of the test bed in testing the lifting resistance of the aircraft is achieved, and the idealization of the use of the aircraft test bed is achieved.
Drawings
In order to more clearly illustrate the embodiments of the 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, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic diagram of the structure of the present utility model.
Fig. 2 is a schematic structural view of a rotating device according to the present utility model.
FIG. 3 is a schematic view of another view of the internal structure of the present utility model.
Fig. 4 is a schematic structural view of the lifting device of the present utility model.
In the figure: 1. a base; 2. a rotating device; 21. a first motor; 22. a first motor base; 23. a riser; 24. a second gear; 25. a round bar; 26. a belt; 27. a belt pulley; 28. a bracket; 29. a connecting rod; 201. a first gear; 202. a second rotating rod; 204. a first rotating lever; 3. a lifting device; 31. a support plate; 32. a slide block; 33. a threaded rod; 34. a second bevel gear; 35. a first bevel gear; 36. the second motor base; 37. a second motor; 38. a chute; 4. a support column; 5. and stopping the brake wheel.
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.
Embodiment one: as shown in fig. 1-3, the utility model provides a portable aircraft simulation test stand, which comprises a base 1, wherein the top end of the base 1 is fixedly connected with a lifting device 3, the lifting device 3 plays a role in lifting, one end of the lifting device 3 is fixedly connected with a rotating device 2, the rotating device 2 plays a role in omnidirectionally rotating a cabin body, the rotating device 2 comprises a first motor 21 and a vertical plate 23, the first motor 21 plays a role in driving the rotating device 2, the output end of the first motor 21 penetrates through one end of the vertical plate 23 and is fixedly connected with a first gear 201, the output end of the first motor 21 is convenient to drive the first gear 201 to rotate, one end of the first gear 201, which is opposite to the first motor 21, is fixedly connected with a connecting rod 29, the connecting rod 29 plays a role in connection, one end of the connecting rod 29 opposite to the first gear 201 is fixedly connected with a bracket 28, the connecting rod 29 is convenient to rotate to drive the bracket 28 to rotate, one side inner wall of the bracket 28 is rotationally connected with the first rotating rod 204, one end of the bracket 28 is penetrated and provided with the second rotating rod 202, the first rotating rod 204 is matched with the second rotating rod 202 to be used to drive the cabin body to rotate, one end of the second rotating rod 202 is fixedly connected with the belt pulley 27, the belt pulley 27 is convenient to rotate to drive the second rotating rod 202 to rotate, one end of the first gear 201 is meshed and connected with the second gear 24, the first gear 201 is convenient to rotate to drive the second gear 24, one end of the second gear 24 is fixedly connected with the round rod 25, the round rod 25 plays a role in connection, one end of the round rod 25 back to the second gear 24 is fixedly connected with the belt pulley 27, the belt pulley 27 is convenient to rotate to be driven by the second gear 24, the outer surfaces of the two belt pulleys 27 are sleeved with the belt 26 together, one of the pulleys 27 is rotated by the other pulley 27 via a belt 26.
The bottom fixedly connected with four support columns 4 of base 1, support column 4 play the effect of supporting base 1, and the equal fixedly connected with of bottom of four support columns 4 stops wheel 5.
By adopting the technical scheme, the brake stopping wheel 5 plays a role in conveniently moving the test bed.
The bottom fixedly connected with first motor cabinet 22 of first motor 21, and the one end of first motor cabinet 22 and the one end fixed connection of riser 23.
By adopting the above technical scheme, the first motor seat 22 plays a role in supporting and fixing the first motor 21.
The teeth of the first gear 201 are the same shape as the teeth of the second gear 24.
By adopting the above technical scheme, the function of facilitating the engagement of the first gear 201 and the second gear 24 is achieved.
The four brake wheels 5 are distributed in rectangular arrays.
By adopting the technical scheme, the movable test bed has a more convenient effect.
Embodiment two: as shown in fig. 4, the lifting device 3 includes a second motor 37, the second motor 37 plays the effect of driving the lifting device 3, top one side fixedly connected with backup pad 31 of base 1, the output of second motor 37 runs through the first bevel gear 35 of one end lower part fixedly connected with of backup pad 31, make things convenient for the rotatory effect of first bevel gear 35 of output drive of second motor 37, the top meshing of first bevel gear 35 is connected with second bevel gear 34, play the rotatory effect of first bevel gear 35 drive second bevel gear 34, the top fixedly connected with threaded rod 33 of second bevel gear 34, make things convenient for the second bevel gear 34 rotatory drive threaded rod 33 rotatory, and the one end of threaded rod 33 dorsad second bevel gear 34 is connected with the top internal surface rotation of backup pad 31, the surface of threaded rod 33 has cup jointed slider 32, threaded rod 33 cooperation slider 32 uses, make slider 32 reciprocate, and the one end of slider 32 and the one end lower part fixedly connected with of riser 23 make things convenient for slider 32 to remove and drive riser 23, the bottom fixedly connected with second motor seat 36 of second motor seat 37, the bottom fixedly connected with second motor seat 36 plays the effect of supporting fixed bottom of second motor seat 37 and the bottom fixedly connected with the bottom of second motor seat 1 of 36.
Through adopting above-mentioned technical scheme, play the effect that the cabin body realized going up and down.
The support plate 31 has an inverted "L" shape.
By adopting the technical scheme, the support is more stable.
One end of the supporting plate 31 is provided with a chute 38 which is matched with the sliding block 32.
By adopting the above technical solution, the chute 38 plays a role in limiting the slide 32.
Working principle: firstly, an aircraft simulation test bed is moved to a test site through a brake stopping wheel 5, a cabin body is fixed at one end of the opposite faces of a first rotating rod 204 and a second rotating rod 202, then a first motor 21 is started, the output end of the first motor 21 drives a first gear 201 to rotate, the first gear 201 rotates to drive a bracket 28 to rotate, meanwhile, the first gear 201 rotates to drive a second gear 24 to rotate, the second gear 24 rotates to drive a first belt pulley 27 to rotate, the belt pulley 27 drives another belt pulley 27 to rotate through a belt 26, the other belt pulley 27 rotates to drive a second rotating rod 202 to rotate, the first rotating rod 204 is matched with the second rotating rod 202 to play a role of fixing and driving the cabin body to rotate, so that the test bed can test the aircraft in all directions, the service efficiency of the aircraft simulation test bed is improved, then a second motor 37 is started, the output end of the second motor 37 drives the first bevel gear 35 to rotate, the first bevel gear 35 rotates to drive a second bevel gear 34 to rotate, the first bevel gear 35 is matched with the second bevel gear 34 to use, the threaded rod 33 rotates, the threaded rod 33 is matched with a sliding block 32 to use, the sliding block 32 to move upwards, the sliding block 32 moves upwards, the bracket 28 is driven to move, and the test bed can move downwards, and the test bed can be tested.
It will be apparent to those skilled in the art that various modifications and variations can be made to the present utility model without departing from the spirit or scope of the utility model. Thus, it is intended that the present utility model also include such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.
Claims (8)
1. The utility model provides a portable aircraft simulation test platform, includes base (1), its characterized in that: the top end of the base (1) is fixedly connected with a lifting device (3), and one end of the lifting device (3) is fixedly connected with a rotating device (2);
the rotating device (2) comprises a first motor (21) and a vertical plate (23), wherein the output end of the first motor (21) penetrates through one end fixedly connected with first gear (201) of the vertical plate (23), one end fixedly connected with connecting rod (29) of the first gear (201) back to the first motor (21), one end fixedly connected with support (28) of the connecting rod (29) back to the first gear (201), one side inner wall of the support (28) is rotationally connected with a first rotating rod (204), one end of the support (28) penetrates through to be provided with a second rotating rod (202), one end fixedly connected with belt pulley (27) of the second rotating rod, one end meshing of the first gear (201) is connected with a second gear (24), one end fixedly connected with round rod (25) of the second gear (24) is connected with a belt pulley (27) back to the one end fixedly connected with the round rod (25), and two outer surfaces of the belt pulleys (27) are sleeved with a belt (26) jointly.
2. A portable aircraft simulation test stand according to claim 1, wherein: lifting device (3) are including second motor (37), top one side fixedly connected with backup pad (31) of base (1), the output of second motor (37) runs through one end lower part fixedly connected with first bevel gear (35) of backup pad (31), the top meshing of first bevel gear (35) is connected with second bevel gear (34), the top fixedly connected with threaded rod (33) of second bevel gear (34), and the one end of threaded rod (33) dorsad second bevel gear (34) is rotated with the top internal surface of backup pad (31) and is connected, slider (32) have been cup jointed to the surface of threaded rod (33), and the one end lower part fixedly connected with of riser (23) of one end of slider (32), the bottom fixedly connected with second motor cabinet (36) of second motor (37), and the bottom of second motor cabinet (36) and the top fixedly connected with of base (1).
3. A portable aircraft simulation test stand according to claim 1, wherein: the bottom fixedly connected with four support columns (4) of base (1), and the bottom of four support columns (4) all fixedly connected with stops wheel (5) of stopping.
4. A portable aircraft simulation test stand according to claim 1, wherein: the bottom fixedly connected with first motor cabinet (22) of first motor (21), and the one end of first motor cabinet (22) is connected with one end fixed of riser (23).
5. A portable aircraft simulation test stand according to claim 1, wherein: the first gear (201) and the second gear (24) have the same tooth shape.
6. A portable aircraft simulation test stand according to claim 2, wherein: the supporting plate (31) is inverted L-shaped.
7. A portable aircraft simulation test stand according to claim 2, wherein: one end of the supporting plate (31) is provided with a chute (38) matched with the sliding block (32).
8. A portable aircraft simulation test stand according to claim 3, wherein: the four brake stopping wheels (5) are distributed in a rectangular array.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321958916.9U CN220164187U (en) | 2023-07-25 | 2023-07-25 | Portable aircraft simulation test stand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321958916.9U CN220164187U (en) | 2023-07-25 | 2023-07-25 | Portable aircraft simulation test stand |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220164187U true CN220164187U (en) | 2023-12-12 |
Family
ID=89054339
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321958916.9U Active CN220164187U (en) | 2023-07-25 | 2023-07-25 | Portable aircraft simulation test stand |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220164187U (en) |
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2023
- 2023-07-25 CN CN202321958916.9U patent/CN220164187U/en active Active
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