CN203870839U - Rotating device for aircraft simulation training - Google Patents
Rotating device for aircraft simulation training Download PDFInfo
- Publication number
- CN203870839U CN203870839U CN201420231084.5U CN201420231084U CN203870839U CN 203870839 U CN203870839 U CN 203870839U CN 201420231084 U CN201420231084 U CN 201420231084U CN 203870839 U CN203870839 U CN 203870839U
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- CN
- China
- Prior art keywords
- wheelwork
- rotating device
- simulation training
- driving cabin
- aircraft simulation
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- 238000012549 training Methods 0.000 title claims abstract description 31
- 238000004088 simulation Methods 0.000 title claims abstract description 21
- 230000004323 axial length Effects 0.000 claims description 4
- 230000000694 effects Effects 0.000 abstract description 8
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 108010066278 cabin-4 Proteins 0.000 description 10
- 230000000007 visual effect Effects 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000005669 field effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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Abstract
The utility model discloses a rotating device for aircraft simulation training, comprising a first rotating device and a second rotating device. One end of the first rotating device is rotationally connected to a support, and the other end of the first rotating device extends out of the support. The second rotating device and the first rotating device are communicated and connected. The second rotating device is arranged at the end part, far away from the support, of the first rotating device. The second rotating device comprises a sleeve communicated and fixedly connected with the first rotating device, and a rotating shaft arranged in the sleeve. One end of the rotating shaft is connected with a rotation driving deice, and the other end of the rotating shaft is connected with a cockpit. The cockpit is arranged in one end part of the first rotating device, which enables trainees to have a greater scope of vision, offers trainees a better flight experience and enhances the training effect. The rotating device has the advantages of simple structure, low manufacturing cost, and wide range of application.
Description
Technical field
The utility model relates to multidimensional simulation training technique field, particularly relates to a kind of wheelwork of aircraft simulation training use.
Background technology
Growing along with China's aeronautical technology, needs badly and cultivates more aircrew.In view of the consideration of the singularity of airmanship and safety, cost aspect, aircrew all needs just can carry out prototype flight by a large amount of equipment simulated trainings later.For Flight Simulator Trainers material, first to ensure that it has multidimensional rotating function, can simulated flight the horizontal stroke of device in flight course, longitudinally overturn, climb, dive, climbing the action such as turns to, to strengthen trainer's flight impression; Meanwhile, also want to ensure that trainer has enough large field range, to strengthen aerial synthetic flight training effect as far as possible.
As Chinese patent literature CN102779438A discloses the full action emulation of a kind of simulated aircraft flight mechanical execution system, it mainly comprises basis, always configures group, girder, gas-holder and air-control device, the first telecontrol equipment, the second telecontrol equipment, the 3rd telecontrol equipment, power electric transmitting device and cabin analogue means; First telecontrol equipment one end is arranged in basis, and the other end runs through girder and holds up cabin analogue means, is provided with power electric transmitting device on the first telecontrol equipment, and the other end is provided with the second cylinder; The 3rd telecontrol equipment one end is provided with the 3rd motor and the 3rd cylinder, and the other end has been realized along X, Y, tri-weeks rectilinear motions of Z and rotatablely moved along X, Y, Z tri-axles by rational structural design through the longitudinal axis axle sleeve and the executive system that are arranged on the second telecontrol equipment.Although the disclosed technical scheme of this patent documentation can be simulated vacuum flight, but due to complicated integral structure, accessory is more, and its driving cabin is arranged on the centre position of transverse axis, the left and right sides visual field of trainee in training process is limited, when side-looking, even can be blocked by miscellaneous equipments such as the transverse axis of its left back or right back, greatly reduce vacuum experience effect, impact training actual effect; In addition, because these simulation trainer parts are more, bulky, cost of manufacture is higher, is difficult to be applied to amateur fly simulation training, as aerolog on recreation ground etc.
Utility model content
For this reason, the technical problems to be solved in the utility model is that existing specialty is limited for the flight simulator left and right sides visual field effect of synthetic flight training or public place of entertainment, affects flight training or amusement, and complicated integral structure, cost of manufacture are higher.
For achieving the above object, the utility model provides the aircraft simulation trainer that a kind of visual field effect is better, simple in structure, cost of manufacture is low, analog training device of the present utility model not only can be used for professional flight training, can also be used for the flight experience of public place of entertainment etc. simultaneously.
The utility model is by the following technical solutions:
A wheelwork for aircraft simulation training use, comprises the first wheelwork and the second wheelwork; One end of described the first wheelwork is connected on bearing rotationally, the other end of described the first wheelwork extends described bearing, described the second wheelwork connects and is connected with described the first wheelwork, described the second wheelwork is arranged on the end away from described bearing of described the first wheelwork, described the second wheelwork comprises the sleeve that connects and be fixedly connected with described the first wheelwork, and be arranged at the turning axle in described sleeve, one end of described turning axle is connected with drive rotating device, and the other end of described turning axle is connected with driving cabin.
Further, described driving cabin is fixedly connected on the end of described turning axle.
Further, described driving cabin is hinged on the end of described turning axle by bearing pin, and the axle center of described bearing pin is perpendicular to the plane at described the first wheelwork and described the second wheelwork place; On described driving cabin, be provided with the drive rotating device that drives described driving cabin to rotate around described bearing pin.
Further, described the first wheelwork is vertical with the axis of described the second wheelwork.
Further, described support comprises the bearing seat for connecting described the first wheelwork and supports the base of described bearing seat.
Further, at least two described bearing seats are set on described base, at a distance of farthest two described in distance between bearing seat substantially equal the half of described the first wheelwork axial length.
Further, on described base, offer several for by bolt hole fixing described support.
Further, the part of extending described support of described the first wheelwork, and described the second wheelwork, driving cabin are all arranged on the inner side for the vault curtain of video picture.
The beneficial effects of the utility model:
1. the second wheelwork of the present utility model is arranged on the end away from bearing of the first wheelwork, and the second steering gear is fixedly connected with the first steering gear by sleeve, the turning axle of the second steering gear is arranged in sleeve, the first wheelwork body is extended at the two ends of turning axle, and one end of turning axle is connected with driving cabin, the other end is connected with driving rotation mechanism.Because driving cabin of the present utility model is arranged on the end position of the first steering gear, therefore trainee has larger field range, and can not blocked by mechanism itself, can give trainee a better flight impression, strengthens training effect; Wheelwork of the present utility model is simple in structure in addition, and cost of manufacture is lower, and usable range is wider.
2. driving cabin of the present utility model is hinged on the end of turning axle, and make the axle center of its jointed shaft perpendicular to the plane at the first wheelwork and the second wheelwork place, and on driving cabin, be provided with the drive rotating device that drives it to rotate around self jointed shaft, this design can realize three dimensionality rotation substantially, and then simulate the more flight attitude of multi-aircraft, strengthen simulation impression, improve training effect and recreational.
3. the first wheelwork of the present utility model is fixed by least two bearing seats that are arranged on support; At a distance of farthest two described in distance between bearing seat substantially equal the half of the first wheelwork axial length.Support because whirligig of the present utility model only depends on one end of the first turning axle, and be fixed the stability that can further strengthen whole device by least two bearing seats are set on the first turning axle, also can not affect trainee's the visual field simultaneously.
4. on the base of the below of the utility model support, offer several for support bracket fastened bolt hole.This design is convenient to whole wheelwork to position, and no matter wheelwork of the present utility model is applied to professional flight training or recreational simulated flight experience, is all easy to wheelwork of the present utility model accurately to locate.
Brief description of the drawings
For the content that makes utility model is more likely to be clearly understood, according to specific embodiment of the utility model also by reference to the accompanying drawings, the utility model is described in further detail, wherein below
Fig. 1 is vertical view of the present utility model;
Fig. 2 is the front view of utility model;
Fig. 3 is right view of the present utility model.
In figure, Reference numeral is expressed as:
1-the first wheelwork; 2-the second wheelwork; 21-sleeve; 22-turning axle; 3-bearing; 31-bearing seat; 32-base; 4-driving cabin; 5-motor; 6-bearing pin; 7-vault curtain.
Embodiment
Referring to Fig. 1-3, a kind of wheelwork of aircraft simulation training use, comprises the first wheelwork 1 and the second wheelwork 2; One end of described the first wheelwork 1 is connected on bearing 3 rotationally, the other end of described the first wheelwork 1 extends described bearing 3, described the second wheelwork 2 connects and is connected with described the first wheelwork 1, described the second wheelwork 2 is arranged on the end away from described bearing 3 of described the first wheelwork 1, described the first wheelwork 1 is vertical with the axis of described the second wheelwork 2, and the substantially L-shaped structural arrangement of two wheelworks; Described the second wheelwork 2 comprises the sleeve 21 that connects and be fixedly connected with described the first wheelwork 1, and be arranged at the turning axle 22 in described sleeve 21, one end of described turning axle 22 is connected with drive rotating device 5, and the other end of described turning axle 22 is connected with driving cabin 4.Because driving cabin 4 of the present utility model is arranged on the end position of the first steering gear 1, therefore trainee has larger field range, and can not blocked by mechanism itself, can give trainee a better flight impression, strengthens training effect; Wheelwork of the present utility model is simple in structure in addition, and cost of manufacture is lower, and usable range is wider.
In the present embodiment, be hinged on the end of described turning axle 22 by bearing pin 6 at described driving cabin 4, and the axle center of described bearing pin 6 is perpendicular to the plane at described the first wheelwork 1 and described the second wheelwork 2 places; On described driving cabin 4, be provided with the drive rotating device that drives described driving cabin 4 to rotate around described bearing pin 6.By described driving cabin 4 being hinged on to the axle head of described the second wheelwork 2, and be provided with and drive the drive rotating device that rotates around described bearing pin 6 of described driving cabin 4, can make driving cabin 4 can realize full freedom degree rotating in virtual space, adopt external panoramic view grenade instrumentation simultaneously, and then can simulate the more flight attitude of multi-aircraft, strengthen simulation impression, improve training effect and recreational.
In the present embodiment, described support 3 comprises the bearing seat 31 for connecting described the first wheelwork 1 and supports the base 32 of described bearing seat 31.At least two described bearing seats 31 are set on described base 32, at a distance of farthest two described in distance between bearing seat 31 substantially equal the half of described the first wheelwork 1 axial length, this supporting way can ensure that the first wheelwork 1 and the second wheelwork 2 have better stability in the time of work, and then guarantees personal safety.
In the present embodiment, offer several for by bolt hole 33 fixing described support 3 on described base 32, described bolt hole 33 is arranged on the edge of described base 33, when fixing, can easily whole bearing be positioned on bottom surface or miscellaneous equipment by bolt.
In the present embodiment, the part of extending described support 3 of described the first wheelwork 1, and described the second wheelwork 2, driving cabin 4 be all arranged on the inner side for the vault curtain 7 of video picture, by throw in corresponding scenery picture on vault curtain 7, to strengthen visual effect.
In other embodiments, described driving cabin 4 also can be fixedly connected on the end of described turning axle 22.Also be that driving cabin in the present embodiment only has the simulation of two-dimensional direction to rotate, be particularly suitable for the places such as amusement, can certainly be used for simulated training, that this design has advantages of is simple in structure, cost is low, be convenient to install, the visual field is good.
Above-mentioned embodiment is just explained in detail the technical solution of the utility model; the utility model has more than and is only confined to above-described embodiment; those skilled in the art should be understood that; the above-mentioned principle of every foundation and the improvement of spirit on the utility model basis, substitute, all should be within protection domain of the present utility model.
Claims (8)
1. a wheelwork for aircraft simulation training use, comprises the first wheelwork (1) and the second wheelwork (2); One end of described the first wheelwork (1) is connected on bearing (3) rotationally, the other end of described the first wheelwork (1) extends described bearing (3), described the second wheelwork (2) connects and is connected with described the first wheelwork (1), it is characterized in that:
Described the second wheelwork (2) is arranged on the end away from described bearing (3) of described the first wheelwork (1), described the second wheelwork (2) comprises the sleeve (21) that connects and be fixedly connected with described the first wheelwork (1), and be arranged at the turning axle (22) in described sleeve (21), one end of described turning axle (22) is connected with drive rotating device (5), and the other end of described turning axle (22) is connected with driving cabin (4).
2. the wheelwork of a kind of aircraft simulation training use according to claim 1, is characterized in that: described driving cabin (4) is fixedly connected on the end of described turning axle (22).
3. the wheelwork of a kind of aircraft simulation training use according to claim 1, it is characterized in that: described driving cabin (4) is hinged on the end of described turning axle (22) by bearing pin (6), and the axle center of described bearing pin (6) is perpendicular to the plane at described the first wheelwork (1) and described the second wheelwork (2) place; On described driving cabin (4), be provided with the drive rotating device that drives described driving cabin (4) to rotate around described bearing pin (6).
4. according to the wheelwork of the arbitrary described a kind of aircraft simulation training use of claim 1-3, it is characterized in that: described the first wheelwork (1) is vertical with the axis of described the second wheelwork (2).
5. the wheelwork of a kind of aircraft simulation training use according to claim 4, is characterized in that: described support (3) comprises the bearing seat (31) for connecting described the first wheelwork (1) and supports the base (32) of described bearing seat (31).
6. the wheelwork of a kind of aircraft simulation training use according to claim 5, it is characterized in that: upper at least two the described bearing seats (31) that arrange of described base (32), at a distance of farthest two described in distance between bearing seat (31) substantially equal the half of described the first wheelwork (1) axial length.
7. the wheelwork of a kind of aircraft simulation training use according to claim 6, is characterized in that: on described base (32), offer several for by bolt hole (33) fixing described support (3).
8. the wheelwork of a kind of aircraft simulation training use according to claim 7, it is characterized in that: the part of extending described support (3) of described the first wheelwork (1), and described the second wheelwork (2), driving cabin (4) are all arranged on the inner side for the vault curtain (7) of video picture.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420231084.5U CN203870839U (en) | 2014-05-07 | 2014-05-07 | Rotating device for aircraft simulation training |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420231084.5U CN203870839U (en) | 2014-05-07 | 2014-05-07 | Rotating device for aircraft simulation training |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203870839U true CN203870839U (en) | 2014-10-08 |
Family
ID=51651767
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420231084.5U Expired - Fee Related CN203870839U (en) | 2014-05-07 | 2014-05-07 | Rotating device for aircraft simulation training |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203870839U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104464441A (en) * | 2014-12-24 | 2015-03-25 | 喻明 | Flight simulation training device |
| CN104658361A (en) * | 2015-02-03 | 2015-05-27 | 北京理工大学 | Semi-physical simulation cockpit |
-
2014
- 2014-05-07 CN CN201420231084.5U patent/CN203870839U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104464441A (en) * | 2014-12-24 | 2015-03-25 | 喻明 | Flight simulation training device |
| CN104658361A (en) * | 2015-02-03 | 2015-05-27 | 北京理工大学 | Semi-physical simulation cockpit |
| CN104658361B (en) * | 2015-02-03 | 2017-10-10 | 北京理工大学 | Cabin is driven in a kind of HWIL simulation |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141008 Termination date: 20180507 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |