CN207037968U - A kind of aircraft flight attitude apparatus for demonstrating - Google Patents
A kind of aircraft flight attitude apparatus for demonstrating Download PDFInfo
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- CN207037968U CN207037968U CN201720614663.1U CN201720614663U CN207037968U CN 207037968 U CN207037968 U CN 207037968U CN 201720614663 U CN201720614663 U CN 201720614663U CN 207037968 U CN207037968 U CN 207037968U
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Abstract
The utility model provides a kind of aircraft flight attitude apparatus for demonstrating, including model aircraft, model-controlled system, operating system and the controller of link model control system and operating system；Model-controlled system includes live spindle, two expansion links, spindle motor and posture motor；One end of live spindle is connected with model aircraft belly close to the side of head, and its other end is connected with spindle motor；One end of two expansion links is connected with model aircraft belly close to the side of tail respectively, its other end and posture motor connection；The angular transducer and two displacement transducers that operating system includes handle, is connected with handle base；Two displacement transducers are arranged on the same plane vertical with handle axial direction and orthogonal, and are connected with handle.The utility model structure is simplified, small volume, is made simply, can effectively save cost；Run smooth, operating handle is preferable, effectively increases the operating experience of operator.
Description
Technical field
The utility model belongs to demonstration equipment technical field, more particularly to a kind of aircraft flight attitude apparatus for demonstrating.
Background technology
The control demonstration equipment of simulation aircraft flight attitude can simulate the various flight attitudes of aircraft, and spectators are grasped by manipulating
Control device controls the flight attitude of model aircraft, experiences the state change of aircraft, make spectators for aircraft under various regimes
Flight attitude can there is one intuitively to experience, existing certain sight can be used for education demonstration.Existing aircraft
The apparatus for demonstrating control structure of flight attitude is complicated, and the requirement to precision is higher, causes to make difficulty；There is also operation simultaneously to imitate
The problem of fruit is bad, the operating handle and model aircraft of actuation means and the inductive effects of actuation means have much room for improvement, sternly
Ghost image rings the operating experience of spectators.
Utility model content
In order to solve the above-mentioned technical problem, the utility model provides a kind of aircraft flight attitude apparatus for demonstrating, including aircraft
Model, model-controlled system, operating system and the connection model-controlled system and the controller of the operating system；
The model-controlled system includes live spindle, two expansion links, spindle motor and posture motor；The rotation master
One end of axle is connected with the model aircraft belly close to the side of head, and its other end is connected with the spindle motor；Two
One end of the expansion link is connected with the model aircraft belly close to the side of tail respectively, its other end and posture electricity
Machine connects；
The angular transducer and two displacement transducers that the operating system includes handle, is connected with the handle；Institute
State the bottom that angular transducer is arranged on the handle；Two institute's displacement sensors are arranged on to hang down with the handle axial direction
On straight same plane, and it is connected with the handle, two orthogonal settings of institute's displacement sensors.
Further, the point and two expansion links that the live spindle is connected with the model aircraft fly with described
The point of machine model connection forms isosceles triangle.
Further, between the live spindle and the model aircraft and the expansion link and the model aircraft it
Between connected by universal joint.
Further, the expansion link includes telescoping tube, leading screw and the lead screw pair nut of one end open；The telescoping tube
Closed end is connected with the model aircraft, and the lead screw pair nut is connected with the openend of the telescoping tube, and the one of the leading screw
End is stretched into the telescoping tube through the lead screw pair nut, its other end and the posture motor connection.
Further, the model-controlled system also includes pedestal, and the posture motor is arranged on the upper table of the pedestal
Face, the spindle motor are arranged in the pedestal, and the live spindle is electric with the main shaft through the upper surface of the pedestal
Machine connects.
Further, the operating system also includes handle set, and the handle set is provided with perforate, set in the perforate
Have a bulb bearing, the handle include handle, the connecting rod that one end is connected with the handle, one end by the bulb bearing and
The buffering rotating shaft that the driving flexible axle of the other end connection of the connecting rod and one end are connected with the other end of the driving flexible axle,
The other end of the buffering rotating shaft is connected with the angular transducer.
Further, the operating system also includes handle case, and spacing hole is offered on the top plate of the handle case, described
Connecting rod is located in the spacing hole.
Further, slide unit and the pressure spring plate being arranged on the slide unit are provided with the handle case, is opened on the slide unit
Provided with slide unit hole, the pressure spring plate is provided with stage clip plate hole, and the connecting rod passes through the slide unit hole and the stage clip plate hole, and two
Individual institute's displacement sensors are connected with the pressure spring plate respectively.
Further, stage clip is also arranged with the connecting rod, the stage clip is arranged on top plate and the institute of the handle case
State between pressure spring plate.
Further, it is arranged with torsion spring on the handle.
Compared with prior art, the beneficial effects of the utility model are：
Aircraft flight attitude apparatus for demonstrating structure provided by the utility model is simplified, and small volume, machining accuracy is wanted
Ask relatively low, manufacture craft is simple, can effectively save cost；Run smooth, operating handle is preferable, effectively increases operator
Operating experience.
Brief description of the drawings
Fig. 1 is the structural representation of model aircraft of the present utility model and model-controlled system；
Fig. 2 is the structural representation of operating system of the present utility model；
Fig. 3 is the connection relationship diagram of model-controlled system of the present utility model, operating system and controller；
Wherein：1 model aircraft；2 live spindles；3 expansion links；301 telescoping tubes；302 leading screws；303 lead screw pair nuts；4 masters
Spindle motor；5 posture motors；6 handles；601 handles；602 connecting rods；603 driving flexible axles；604 buffering rotating shafts；7 angular transducers；
8 displacement transducers；9 universal joints；10 pedestals；11 handle sets；12 bulb bearings；13 handle cases；14 spacing holes；15 slide units；16
Pressure spring plate；17 slide unit holes；18 stage clips；19 torsion springs；20 fixed plates.
Embodiment
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " is based on accompanying drawing institutes
The orientation or position relationship shown, it is for only for ease of description the utility model and simplifies description, rather than indicates or imply and be signified
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this practicality
The limitation of novel protected scope.
A kind of aircraft flight attitude apparatus for demonstrating, as Figure 1-3, including model aircraft 1, model-controlled system, operation
System and the controller of link model control system and operating system；
Model-controlled system includes 2, two expansion links 3 of live spindle, spindle motor 4 and posture motor 5；Live spindle 2
It is connected with belly of the one end of two expansion links 3 with model aircraft 1, wherein, live spindle 2 and the tie point of model aircraft 1
Belly positioned at model aircraft 1 is located at model aircraft 1 close to the side of head, the tie point of two expansion links 3 and model aircraft 1
Belly is close to the side of tail；The one end of live spindle 2 away from model aircraft 1 is connected with spindle motor 4；Two expansion links 3 are remote
One end from model aircraft 1 is connected with posture motor 5；Spindle motor 4 and two posture motors 5 are connected with controller；
The angular transducer 7 and two displacement transducers 8 that operating system includes handle 6, is connected with the bottom of handle 6；Two
Individual displacement transducer 8 is separately positioned in X-direction and Y-direction；The axial direction of the original position of handle 6 is located in Z-direction, and
The movement in X-direction and Y-direction can be rotated and carried out as fulcrum using the tie point of handle 6 and angular transducer 7；Two
Individual displacement transducer 8 is connected with handle 6；Angular transducer 7 and two displacement transducers 8 are connected with controller.
In the utility model, the axial direction of the initial position of handle 6 is located in Z-direction, and its bottom connection angle passes
Sensor 7, angular transducer 7 collect handle 6 and rotate caused directional information and angle information and pass to controller, and controller leads to
The rotation that spindle motor 4 controls live spindle 2 is crossed, model aircraft 1 is made the action turned accordingly；Handle 6 in X-direction and
A displacement transducer 8 is all connected with Y-direction, the displacement transducer 8 in X-direction collects the direction that handle 6 moves left and right
Information and displacement information simultaneously pass to controller, and the displacement transducer 8 in Y-direction collects the movable direction of handle 6
Information and displacement information simultaneously pass to controller, the directional information and displacement information that controller moves the front, rear, left and right of handle 6
Two posture motors 5 are passed to, control two expansion links 3 flexible by two posture motors 5, and model aircraft 1 is done respectively
Go out underriding, pull-up, "Left"-deviationist, the action of Right deviation.
During using aircraft flight attitude apparatus for demonstrating provided by the utility model, operator's control handle 6 rotated with
And carry out movement in X-direction and Y-direction, you can make that model aircraft 1 makes turning and underridings, pull-up, "Left"-deviationist, Right deviation are moved
Make.
Controller in the utility model can select the controller of the models such as STM32 series；Spindle motor 4 can be selected
The stepper motor of the models such as 42 series；Posture motor 5 can select the stepper motor of the models such as 35 series；Angular transducer 7 can
To select rotary encoder or potentiometer, such as ALPS27 types potentiometer；Displacement transducer 8 can select KPM hinge type displacements
The displacement transducer of the models such as sensor.
In the utility model, because the belly of model aircraft 1 is cambered, therefore model aircraft 1 is fixed on fixed plate 20
On, then live spindle 2 and expansion link 3 be connected with the relevant position of the bottom of fixed plate 20, can effectively it reduce by live spindle 2
The difficulty of the change of flight posture of model aircraft 1 is controlled with expansion link 3, makes that preparation technology is simpler, operation is also more accurate.
In the utility model, live spindle 2 and the tie point of model aircraft 1 and two expansion links 3 and model aircraft 1
The point of connection forms an isosceles triangle.Such design can reduce the difficulty that operational control is carried out to model aircraft 1, and
And the requirement to the apparatus for demonstrating accuracy of manufacture can be reduced.
In the utility model, connected between live spindle 2 and expansion link 3 and model aircraft 1 by universal joint 9,
Allow live spindle 2 and expansion link 3 rotation and it is flexible while arbitrarily change angle between model aircraft 1, make to fly
The change of the flight attitude of machine model 1 is more accurate and smooth, and the operating experience of operator is more preferably.
Expansion link 3 in the utility model can select the rod member of common retractable.The specific implementation of expansion link 3
Scheme can be to be made up of the telescoping tube 301, leading screw 302 and lead screw pair nut 303 of one end open；The closed end of telescoping tube 301
It is connected with model aircraft 1, lead screw pair nut 303 is connected with the openend of telescoping tube 301, and one end of leading screw 302 passes through lead screw pair
Nut 303 is stretched into telescoping tube 301, and its other end is connected with posture motor 5.When telescoping tube 301 extends, posture motor 5 drives
Leading screw 302 stretches out out of telescoping tube 301；When telescoping tube 301 shortens, posture motor 5 is driven in the retraction telescoping tube 301 of leading screw 302.
In the utility model, model-controlled system also includes the interior pedestal 10 for having cavity, and posture motor 5 is arranged on pedestal
10 upper surface, spindle motor 4 are arranged in the cavity of pedestal 10, and live spindle 2 is electric with main shaft through the upper surface of pedestal 10
Machine 4 connects.
In the utility model, handle 6 from top to bottom includes handle 601, connecting rod 602, driving flexible axle 603 and eased up red switch
604 4 parts of axle；Wherein connecting rod 602 and driving flexible axle 603 is connected by bulb bearing 12；It is additionally provided with operating system
Handle set 11, handle set 11 are provided with perforate, and bulb bearing 12 is arranged in perforate.Handle 6 is designed to that above-mentioned structure can be with
Handle 6 and the Hard link of angular transducer 7 are avoided, plays a part of degree of protection sensor 7.
Handle case 13 is additionally provided with operating system, spacing hole 14 is offered on the top plate of handle case 13, connecting rod 602 is worn
It is located in spacing hole 14, handle 601 is located at the outside of handle case 13, and the driving flexible axle 603 red switch axle 604 that eases up is located at handle case 13
It is interior.Spacing hole 14 can limit the moving displacement of handle 6 in the x-direction and the z-direction, avoid because displacement is excessive caused to drilling
The damage of showing device.
Slide unit 15 and the pressure spring plate 16 on slide unit 15 are provided with handle case 13, slide unit hole 17 is opened up on slide unit 15,
Stage clip plate hole is opened up on pressure spring plate 16, the diameter of stage clip plate hole is less than the diameter in slide unit hole 17, and connecting rod 602 passes through slide unit hole 17
With stage clip plate hole, two displacement transducers 7 are connected with pressure spring plate 16 respectively.The diameter of stage clip plate hole is with slightly larger than connecting rod 602
Diameter be preferred.When connecting rod 602 moves in slide unit hole 17 to front, rear, left and right, pressure spring plate 16 can be driven to move, so that
The displacement transducer 7 being connected with pressure spring plate 16 receives displacement information.
Handle set 11 and slide unit 15 can be fixed by the way of supporting support is set, and can also be used its side
While the mode being fixedly attached on the medial surface of handle case is fixed.
Stage clip 18 is also arranged with connecting rod 602, stage clip 18 is fastened on lower surface and the stage clip of the top plate of handle case 13
Between the upper surface of plate 16.Stage clip 18 plays a part of preventing pressure spring plate 16 produces from moving up and down.
In the utility model, torsion spring 19 is arranged with connecting rod 602.Torsion spring 19 not only can be such that handle 6 replys in time
Original position, the operating handle of operator can also be improved.
Finally it should be noted that embodiment of above is only unrestricted to illustrate the technical solution of the utility model, to the greatest extent
The utility model is described in detail with reference to better embodiment for pipe, it will be understood by those within the art that, can
To be modified to the technical solution of the utility model or equivalent substitution, without departing from the spirit of technical solutions of the utility model
And scope, it all should cover among right of the present utility model.
Claims (10)
1. a kind of aircraft flight attitude apparatus for demonstrating, it is characterised in that described device includes model aircraft (1), model cootrol system
System, operating system and the connection model-controlled system and the controller of the operating system；
The model-controlled system includes live spindle (2), two expansion links (3), spindle motor (4) and posture motor (5)；Institute
The one end for stating live spindle (2) is connected with the model aircraft (1) belly close to the side of head, its other end and the main shaft
Motor (4) connects；One end of two expansion links (3) connects with the model aircraft (1) belly close to the side of tail respectively
Connect, its other end is connected with the posture motor (5)；
The angular transducer (7) and two displacement sensings that the operating system includes handle (6), is connected with the handle (6)
Device (8)；The angular transducer (7) is arranged on the bottom of the handle (6)；Two institute's displacement sensors (8) be arranged on
On the vertical same plane of handle (6) axial direction, and it is connected with the handle (6), two displacement sensings
Device (8) orthogonal setting.
2. apparatus for demonstrating according to claim 1, it is characterised in that the live spindle (2) and the model aircraft (1)
The point of connection and two expansion links (3) form isosceles triangle with the point that the model aircraft (1) is connected.
3. apparatus for demonstrating according to claim 1, it is characterised in that the live spindle (2) and the model aircraft (1)
Between and the expansion link (3) and the model aircraft (1) between be connected by universal joint (9).
4. apparatus for demonstrating according to claim 1, it is characterised in that the expansion link (3) includes the flexible of one end open
Manage (301), leading screw (302) and lead screw pair nut (303)；The closed end of the telescoping tube (301) connects with the model aircraft (1)
Connect, the lead screw pair nut (303) is connected with the openend of the telescoping tube (301), and one end of the leading screw (302) passes through institute
State lead screw pair nut (303) to stretch into the telescoping tube (301), its other end is connected with the posture motor (5).
5. apparatus for demonstrating according to claim 1, it is characterised in that the model-controlled system also includes pedestal (10),
The posture motor (5) is arranged on the upper surface of the pedestal (10), and the spindle motor (4) is arranged on the pedestal (10)
Interior, the live spindle (2) is connected through the upper surface of the pedestal (10) with the spindle motor (4).
6. apparatus for demonstrating according to claim 1, it is characterised in that the operating system also includes handle set (11), institute
State handle set (11) and be provided with perforate, be provided with bulb bearing (12) in the perforate, the handle (6) include handle (601),
Connecting rod (602) that one end is connected with the handle (601), one end pass through the bulb bearing (12) and the connecting rod
(602) buffering that the driving flexible axle (603) of other end connection and one end are connected with the other end of the driving flexible axle (603)
Rotating shaft (604), the other end of the buffering rotating shaft (604) are connected with the angular transducer (7).
7. apparatus for demonstrating according to claim 6, it is characterised in that the operating system also includes handle case (13), institute
State and spacing hole (14) is offered on the top plate of handle case (13), the connecting rod (602) is located in the spacing hole (14).
8. apparatus for demonstrating according to claim 7, it is characterised in that slide unit (15) is provided with the handle case (13) and is set
The pressure spring plate (16) on the slide unit (15) is put, slide unit hole (17), the pressure spring plate (16) are offered on the slide unit (15)
Stage clip plate hole is provided with, the connecting rod (602) passes through the slide unit hole (17) and the stage clip plate hole, and two displacements pass
Sensor (7) is connected with the pressure spring plate (16) respectively.
9. apparatus for demonstrating according to claim 8, it is characterised in that be also arranged with stage clip on the connecting rod (602)
(18), the stage clip (18) is arranged between the top plate of the handle case (13) and the pressure spring plate (16).
10. apparatus for demonstrating according to claim 1, it is characterised in that be arranged with torsion spring (19) on the handle (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720614663.1U CN207037968U (en) | 2017-05-27 | 2017-05-27 | A kind of aircraft flight attitude apparatus for demonstrating |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720614663.1U CN207037968U (en) | 2017-05-27 | 2017-05-27 | A kind of aircraft flight attitude apparatus for demonstrating |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207037968U true CN207037968U (en) | 2018-02-23 |
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ID=61470035
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720614663.1U Active CN207037968U (en) | 2017-05-27 | 2017-05-27 | A kind of aircraft flight attitude apparatus for demonstrating |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207037968U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107038927A (en) * | 2017-05-27 | 2017-08-11 | 合肥磐石自动化科技有限公司 | A kind of aircraft flight attitude apparatus for demonstrating |
-
2017
- 2017-05-27 CN CN201720614663.1U patent/CN207037968U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107038927A (en) * | 2017-05-27 | 2017-08-11 | 合肥磐石自动化科技有限公司 | A kind of aircraft flight attitude apparatus for demonstrating |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 230000 southwest of the intersection of Yunhu road and Jixian Road, Feixi Economic Development Zone, Hefei City, Anhui Province Patentee after: Hefei Panshi Intelligent Technology Co.,Ltd. Address before: 231200 West A-13, industrial investment Liheng industrial Plaza (phase II), prosperous Avenue, Taohua Industrial Park, economic development zone, Hefei, Anhui Patentee before: HEFEI PANSHI AUTOMATION TECHNOLOGY Co.,Ltd. |
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| CP03 | Change of name, title or address |