CN208459032U - Unmanned plane during flying simulator and system - Google Patents
Unmanned plane during flying simulator and system Download PDFInfo
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- CN208459032U CN208459032U CN201820373811.XU CN201820373811U CN208459032U CN 208459032 U CN208459032 U CN 208459032U CN 201820373811 U CN201820373811 U CN 201820373811U CN 208459032 U CN208459032 U CN 208459032U
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- unmanned plane
- during flying
- plane during
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Abstract
The utility model relates to a kind of unmanned plane during flying simulator and systems, the device includes base mechanism and supporting mechanism, supporting mechanism includes support frame and the carrying platform for carrying unmanned plane, support frame is set on base mechanism and rotates around first axle relative to base mechanism, and carrying platform, which is set on support frame, to be rotated around the second axis intersected with first axle relative to support frame.In above-mentioned unmanned plane during flying simulator, unmanned plane is installed on carrying platform, synchronous drive is set to the carrying platform rotation on support frame when support frame is rotated around first axle relative to base mechanism, and carrying platform is rotated around second axis relative to support frame simultaneously, carrying platform is set to rotate around first axle and/or rotate around second axis, there are two rotational freedoms for unmanned plane tool i.e. on carrying platform, and a variety of different flight attitudes may be at by the drive unmanned plane of above-mentioned carrying platform, so can accurate simulation unmanned plane during flying when posture.
Description
Technical field
The utility model relates to unmanned plane fields, more particularly to unmanned plane during flying simulator and system.
Background technique
With the continuous development of unmanned plane industry and the continuous advancement of technology, the application field of unmanned plane is more and more extensive,
And it is very big using the space of potential demand, especially in agricultural plant protection, electric inspection process, air remote sensing, forest fire protection and
The fields such as police patrol.Unmanned plane industry to push relevant industries transition and upgrade development play the role of it is important and energetically, and
And as the further in-depth and the continuous renewal of technology, the development of unmanned plane industry of civil-military inosculation development also keep good
The impetus.With the continuous expansion of unmanned plane industry application field, application environment and application conditions are also more and more diversified, nobody
Requirement of the machine in terms of reliability is also higher and higher, therefore seems especially heavy to unmanned plane development relevant environment and reliability test
It wants.
At present when carrying out unmanned plane environment and reliability test, unmanned plane is directly generally fixed on testing stand pedestal
On, it is tested under fixed pose, specific inclination angle.But unmanned plane can have hovering in flight course, advance, and rise,
Various state of flights, the different state of flights such as decline correspond to the different flight attitude of unmanned plane, but generally can not accurate mould
Posture when quasi- unmanned plane during flying.
Utility model content
Based on this, it is necessary to generally can not accurate simulation unmanned plane during flying when posture aiming at the problem that, providing one kind can be with
The unmanned plane during flying simulator and system of posture when accurate simulation unmanned plane during flying.
A kind of unmanned plane during flying simulator, including base mechanism and supporting mechanism, the supporting mechanism include support frame
With the carrying platform for carrying unmanned plane, support frame as described above is set on the base mechanism and around the relatively described bottom of first axle
Seat mechanism rotation, the carrying platform are set on support frame as described above and around the second axis intersected with the first axle with respect to institute
State support frame rotation.
Above-mentioned unmanned plane during flying simulator is used to carry out relevant environment and reliability test to unmanned plane, in test process
In, unmanned plane is installed on carrying platform, synchronous drive is set to branch when support frame is rotated around first axle relative to base mechanism
Carrying platform rotation on support, and carrying platform is rotated around second axis relative to support frame simultaneously, makes carrying platform around first
Axis is rotated and/or is rotated around second axis, i.e., there are two rotational freedoms for the unmanned plane tool on carrying platform, and by above-mentioned
The drive unmanned plane of carrying platform may be at a variety of different flight attitudes, so can accurate simulation unmanned plane during flying when
Posture.
The first axle is vertically arranged with the second axis in one of the embodiments,.
The base mechanism includes pedestal and the first driving assembly, first driving group in one of the embodiments,
Part includes the first actuator and first rotating shaft, and first actuator is set in the pedestal, and the first rotating shaft is along described the
The direction of one axis is connected between first actuator and support frame as described above, and first actuator passes through described first turn
Axis drives support frame as described above to rotate around the first axle.
The base mechanism further includes the first brake in one of the embodiments, and first brake is sheathed on
Outside the first rotating shaft.
The supporting mechanism further includes the second driving assembly in one of the embodiments, and support frame as described above includes bottom plate
And two side plates at the bottom plate both ends are relatively arranged on, the bottom plate is rotatably connected with the base mechanism, the load
Platform is rotatably arranged between two side plates along the direction of the second axis, and second driving assembly is born with described
Carrying platform connects and it is driven to rotate around the second axis.
Opposite end of the load platform along the second axis direction is respectively arranged in one of the embodiments,
Two the second rotation axis, two second rotation axis can be rotatably set along the setting of the direction of the second axis and respectively
In on two side plates.
Support frame as described above further includes support plate in one of the embodiments, in the support plate and two side plates
The setting of any one interval and be fixed on the bottom plate, second driving assembly is fixed on the support plate far from described
The side of side plate is provided between the support plate and the side plate and is connected to the second driving assembly output shaft and described the
Second shaft coupling between two shafts.
It in one of the embodiments, further include the first controller and second controller, first controller is for controlling
The first actuator rotation is made, the second controller is for controlling the second driving assembly rotation.
A kind of unmanned plane during flying simulation system, including environmental chamber and above-mentioned unmanned plane during flying simulator, the nothing
Man-machine aerolog is set in the environmental chamber, and the environmental chamber is used to simulate the flight environment of vehicle of unmanned plane.
The environmental chamber is high-low temperature test chamber in one of the embodiments, and the high-low temperature test chamber includes
First cabinet and the temperature conditioning unit on first cabinet, the temperature conditioning unit is for raising and reducing first cabinet
Interior temperature, the unmanned plane during flying simulator are contained in first cabinet；Or
The environmental chamber is typhoon rainproof box, and the typhoon rainproof box includes the second cabinet and is respectively arranged on described
Drench with rain unit and blowing unit on second box top wall and side wall, unit and the blowing unit of drenching with rain is respectively to described
It drenches with rain and dries in second cabinet, the unmanned plane during flying simulator is contained in second cabinet.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of unmanned plane during flying simulator in an embodiment of the present invention；
Fig. 2 is the diagrammatic cross-section of unmanned plane during flying simulator shown in Fig. 1；
Fig. 3 is the control schematic diagram of unmanned plane during flying simulator shown in Fig. 1；
Fig. 4 is the structural scheme of mechanism of unmanned plane during flying simulation system in an embodiment of the present invention；
Fig. 5 is the structural scheme of mechanism of unmanned plane during flying simulation system in another embodiment of the utility model.
Specific embodiment
The utility model is more fully retouched below with reference to relevant drawings for the ease of understanding the utility model,
It states.The preferred embodiment of the utility model is given in attached drawing.But the utility model can come in many different forms
It realizes, however it is not limited to embodiment described herein.On the contrary, purpose of providing these embodiments is makes to the utility model
The understanding of disclosure is more thorough and comprehensive.
It should be noted that it can directly on the other element when element is referred to as " being fixed on " another element
Or there may also be elements placed in the middle.When an element is considered as " connection " another element, it, which can be, is directly connected to
To another element or it may be simultaneously present centering elements.Term as used herein " vertical ", " horizontal ", " left side ",
" right side " and similar statement are for illustrative purposes only.
Unless otherwise defined, all technical and scientific terms used herein are led with the technology for belonging to the utility model
The normally understood meaning of the technical staff in domain is identical.Terminology used in the description of the utility model herein only be
The purpose of description specific embodiment, it is not intended that in limitation the utility model.Term " and or " used herein includes
Any and all combinations of one or more related listed items.
As shown in Figs. 1-2, the unmanned plane during flying simulator 100 in an embodiment of the present invention includes base mechanism 10
With supporting mechanism 30, supporting mechanism 30 includes that support frame 32 and the carrying platform 34 for carrying unmanned plane, support frame 32 are set to
On base mechanism 10 and around first axle relative to base mechanism 10 rotate, carrying platform 34 be set to support frame 32 on around with first axle
The second axis of line intersection is rotated relative to support frame 32.
Above-mentioned unmanned plane during flying simulator 100 is used to carry out relevant environment and reliability test to unmanned plane, is testing
In the process, unmanned plane is installed on carrying platform 34, support frame 32 is synchronous when rotating around first axle relative to base mechanism 10
The carrying platform 34 being set on support frame 32 is driven to rotate, and carrying platform 34 is around second axis with respect to 32 turns of support frame simultaneously
It is dynamic, so that carrying platform 34 is rotated around first axle and/or is rotated around second axis, i.e., the unmanned plane on carrying platform 34 has two
A rotational freedom, and a variety of different flight attitudes may be at by the drive unmanned plane of above-mentioned carrying platform 34, so
Can accurate simulation unmanned plane during flying when posture.
Specifically, first axle is vertically arranged with second axis, by rotating around orthogonal two axis, can be incited somebody to action
Unmanned plane on carrying platform 34 is adjusted to suitable tilt angle.In Fig. 2, the direction of first axle is vertical direction, the
The direction of two axis is horizontal direction.Also, a certain number of through-holes and threaded hole are offered in support platform 34, for fixing
Unmanned plane and other relevant devices.Fixed unmanned plane quantity, is not limited to one, can set according to actual needs in support platform 34
Load platform 34 is counted, to increase the quantity of test unmanned plane.
Base mechanism 10 includes pedestal 12 and the first driving assembly 14, and the first driving assembly 14 includes the first actuator 141
With first rotating shaft 143, the first actuator 141 is set in pedestal 12, and first rotating shaft 143 is connected to first along the direction of first axle
Between driving mechanism 141 and support frame 32, the first actuator 141 drives support frame 32 around first axle by first rotating shaft 143
Rotation applies the torque rotated around first axle to supporting mechanism 30 by the first actuator 141.Specifically, the first driving
Part 141 is first servo motor, and the output shaft of first servo motor is connect with the first retarder 15, is adjusted by the first retarder 15
The output torque of first servo motor is saved, it, will then by first retarder of the connection of first shaft coupling 16 15 and first rotating shaft 143
Torque transfer after adjusting drives supporting mechanism 30 to rotate to first rotating shaft 143.
Base mechanism 10 further includes the first brake 17, and the first retainer 17 is sheathed on outside first rotating shaft 143, for preventing
The trend of rotation or the rotation of first rotating shaft 143.
Supporting mechanism 30 further includes the second driving assembly 36, and support frame 32 is including bottom plate 321 and is relatively arranged on bottom plate 321
Two side plates 323 at both ends, bottom plate 321 are rotatably connected with base mechanism 10, and load platform 34 can along the direction of second axis
It is rotatably arranged between two side plates 323, the second driving assembly 36 connect with load platform 34 and it is driven to turn around second axis
It is dynamic.Two side plates 323 being oppositely arranged are used to support the opposite both ends of load platform 34, and the second driving assembly 36 and load are flat
The connection of platform 34 simultaneously applies the torque rotated around second axis to load platform 34.Specifically, the second driving assembly 36 includes second
Servo motor 361 and the second retarder 363 connecting with the second servo motor 361, the second retarder 363 is by the second servo motor
The torque of 361 outflows is transferred to load platform 34 after adjusting.
The both ends opposite along second axis direction of load platform 34 are respectively set there are two the second rotation axis 341, and two the
Two rotation axis 341 along the setting of the direction of second axis and are rotatablely arranged on two side plates 323, the second rotation axis respectively
Load platform 34 is rotatably supported between two side plates 323 by 341 rotating fulcrum as load platform 34.
Support frame 32 further includes support plate 325, the setting of any one interval in support plate 325 and two side plates 323 and
It is fixed on bottom plate 321, the second driving assembly 36 is fixed on side of the support plate 325 far from side plate 323, support plate 325 and side
The second shaft coupling 38 being connected between 36 output shaft of the second driving assembly and the second shaft 341 is provided between plate 323.The bottom of at
With the setting of the interval of side plate 323 for installing the support plate 325 of the second driving assembly 36 on plate 321, and by the second driving assembly
36 are fixed on side of the support plate 325 far from side plate 323, can so set in the gap between side plate 323 and support plate 325
Second shaft coupling 38 is set, in the torque transfer to the second shaft 341 for exporting the second driving assembly 36.
Supporting mechanism 30 further includes second brake 33, and second brake 33 is sheathed on outside the second shaft 341, for preventing
The trend of rotation or the rotation of second shaft 341.Specifically, second brake 33 is sheathed on the far from 325 side of support plate
Outside two shafts 341.
As shown in figure 3, unmanned plane during flying simulator 100 further includes the first controller 50 and second controller 60, first
Controller 50 is for controlling the rotation of the first actuator 141, and second controller 60 is for controlling the rotation of the second driving assembly 36.Pass through
First controller 50 and 60 intelligentized control method the first actuator 141 of second controller and the second driving assembly 36, according to actual
Test demand reasonably accurate controls the rotation of load platform 34, and then can accurately control the appearance of unmanned plane on load platform
State.
As illustrated in figures 4-5, the utility model also provides a kind of unmanned plane during flying simulation system, which includes environmental simulation
Case and above-mentioned unmanned plane is non-determines simulator 100, unmanned plane during flying simulator 100 is set in environmental chamber, environmental simulation
Case is used to simulate the flight environment of vehicle of unmanned plane, so simulates unmanned plane during flying pose by unmanned plane during flying simulator 100
Meanwhile different flight environment of vehicle is generated to unmanned plane by environmental chamber, it can further simulate the live flying of unmanned plane
Situation, so can the reliability to unmanned plane more accurately detected and judged.
As shown in figure 4, in one embodiment, environmental chamber is high-low temperature test chamber 70, high-low temperature test chamber 70 is wrapped
The first cabinet 72 and the temperature conditioning unit 74 on the first cabinet 72 are included, temperature conditioning unit 74 is for raising and reducing the first cabinet 72
Interior temperature, unmanned plane during flying simulator 100 are set in the first cabinet 72.It is a variety of by the offer of high-low temperature test chamber 70 one
The experimental enviroment of temperature, unmanned plane during flying simulator 100 are contained in the first cabinet 72, are put on carrying platform 34 wherein
Unmanned plane is set, unmanned plane can be made to be in the experimental enviroment of various temperature while carrying out flight simulation to unmanned plane, it can be with
Adaptive capacity to environment during unmanned plane during flying is tested.
As shown in figure 5, in another embodiment, environmental chamber is typhoon rainproof box 90, typhoon rainproof box 90 includes
Second cabinet 92 and drench with rain unit 94 and the blowing unit 96 being respectively arranged on 92 roof of the second cabinet and side wall, unit of drenching with rain
94 and blowing unit 96 drench with rain and dry into the second cabinet 92 respectively.The examination for providing typhoon by typhoon rainproof box 90 and drenching with rain
Environment is tested, unmanned plane during flying simulator 100 is contained in the second cabinet 92, places nobody on carrying platform 34 wherein
Machine can be such that unmanned plane is in typhoon and the experimental enviroment drenched with rain while carrying out flight simulation to unmanned plane, can be to nothing
Adaptive capacity to environment in man-machine flight course is tested.It is to be appreciated that in some other embodiment, environmental chamber
Other kinds of experimental enviroment can also be provided, it is not limited here.
Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, all should be considered as described in this specification.
Above-described embodiments merely represent several embodiments of the utility model, the description thereof is more specific and detailed,
But it cannot be understood as the limitations to utility model patent range.It should be pointed out that for the common skill of this field
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
The protection scope of the utility model.Therefore, the scope of protection shall be subject to the appended claims for the utility model patent.
Claims (10)
1. a kind of unmanned plane during flying simulator, which is characterized in that including base mechanism and supporting mechanism, the supporting mechanism packet
Support frame and the carrying platform for carrying unmanned plane are included, support frame as described above is set on the base mechanism and around first axle phase
The base mechanism is rotated, the carrying platform is set on support frame as described above and around the second axis intersected with the first axle
Line is rotated relative to support frame as described above.
2. unmanned plane during flying simulator according to claim 1, which is characterized in that the first axle and described second
Axis is vertically arranged.
3. unmanned plane during flying simulator according to claim 1 or 2, which is characterized in that the base mechanism includes bottom
Seat and the first driving assembly, first driving assembly include the first actuator and first rotating shaft, and first actuator is set to
In the pedestal, the first rotating shaft along the direction of the first axle be connected to first actuator and support frame as described above it
Between, first actuator drives support frame as described above to rotate around the first axle by the first rotating shaft.
4. unmanned plane during flying simulator according to claim 3, which is characterized in that the base mechanism further includes first
Brake, first brake are sheathed on outside the first rotating shaft.
5. unmanned plane during flying simulator according to claim 3, which is characterized in that the supporting mechanism further includes second
Driving assembly, support frame as described above include bottom plate and two side plates for being relatively arranged on the bottom plate both ends, the bottom plate with it is described
Base mechanism is rotatably connected, the carrying platform along the direction of the second axis be rotatably arranged in two side plates it
Between, second driving assembly connect with the carrying platform and it is driven to rotate around the second axis.
6. unmanned plane during flying simulator according to claim 5, which is characterized in that the carrying platform is along described second
The opposite end of axis direction is respectively set there are two the second rotation axis, and two second rotation axis are along the second axis
Direction setting and be rotatablely arranged on two side plates respectively.
7. unmanned plane during flying simulator according to claim 6, which is characterized in that support frame as described above further includes support
Plate, the support plate are arranged with any one interval in two side plates and are fixed on the bottom plate, and described second drives
Dynamic component is fixed on side of the support plate far from the side plate, is provided with and is connected between the support plate and the side plate
Second shaft coupling between the second driving assembly output shaft and second rotation axis.
8. unmanned plane during flying simulator according to claim 5, which is characterized in that further include the first controller and second
Controller, first controller is for controlling first actuator rotation, and the second controller is for controlling described the
The rotation of two driving assemblies.
9. a kind of unmanned plane during flying simulation system, which is characterized in that including environmental chamber and claim 1-8 any one institute
The unmanned plane during flying simulator stated, the unmanned plane during flying simulator are set in the environmental chamber, the environment mould
Quasi- case is used to simulate the flight environment of vehicle of unmanned plane.
10. unmanned plane during flying simulation system according to claim 9, which is characterized in that the environmental chamber is height
Temperature test box, the high-low temperature test chamber include the first cabinet and the temperature conditioning unit on first cabinet, the temperature control
For unit for raising and reducing described first case intracorporal temperature, the unmanned plane during flying simulator is contained in first case
In vivo；Or
The environmental chamber is typhoon rainproof box, and the typhoon rainproof box includes the second cabinet and is respectively arranged on described second
Drench with rain unit and blowing unit on box top wall and side wall, unit and the blowing unit of drenching with rain is respectively to described second
It drenches with rain and dries in cabinet, the unmanned plane during flying simulator is contained in second cabinet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820373811.XU CN208459032U (en) | 2018-03-19 | 2018-03-19 | Unmanned plane during flying simulator and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820373811.XU CN208459032U (en) | 2018-03-19 | 2018-03-19 | Unmanned plane during flying simulator and system |
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| Publication Number | Publication Date |
|---|---|
| CN208459032U true CN208459032U (en) | 2019-02-01 |
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ID=65156277
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820373811.XU Active CN208459032U (en) | 2018-03-19 | 2018-03-19 | Unmanned plane during flying simulator and system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108827670A (en) * | 2018-03-19 | 2018-11-16 | 中国电子产品可靠性与环境试验研究所（（工业和信息化部电子第五研究所）（中国赛宝实验室）） | Unmanned plane during flying simulator and system |
-
2018
- 2018-03-19 CN CN201820373811.XU patent/CN208459032U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108827670A (en) * | 2018-03-19 | 2018-11-16 | 中国电子产品可靠性与环境试验研究所（（工业和信息化部电子第五研究所）（中国赛宝实验室）） | Unmanned plane during flying simulator and system |
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