CN207683776U - Power system and control system disconnect-type aircraft - Google Patents
Power system and control system disconnect-type aircraft Download PDFInfo
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- CN207683776U CN207683776U CN201721565999.XU CN201721565999U CN207683776U CN 207683776 U CN207683776 U CN 207683776U CN 201721565999 U CN201721565999 U CN 201721565999U CN 207683776 U CN207683776 U CN 207683776U
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- control panel
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- propeller
- unmanned plane
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- 239000000575 pesticide Substances 0.000 claims abstract description 33
- 230000005540 biological transmission Effects 0.000 claims abstract description 19
- 238000002347 injection Methods 0.000 claims abstract description 17
- 239000007924 injection Substances 0.000 claims abstract description 17
- 238000005183 dynamical system Methods 0.000 claims description 20
- 239000000446 fuel Substances 0.000 claims description 15
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 6
- 239000003814 drug Substances 0.000 claims description 4
- 229940079593 drug Drugs 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 3
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- 244000025254 Cannabis sativa Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000037396 body weight Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000003337 fertilizer Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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Abstract
The utility model relates to a power system and control system separated aircraft, which comprises a base frame, a horizontal beam, an oil power system, an oil power transmission mechanism, a propeller, a Y-direction control panel, an X-direction control panel, a pesticide box, a pesticide conveying conduit and a pesticide injection pipeline, wherein the base frame supports the horizontal beam, and the propeller is arranged on the horizontal beam; the oil power system comprises an oil storage tank and an oil-driven engine, and the oil-driven engine drives the propeller to rotate through the oil power transmission mechanism; the Y-direction control panel and the X-direction control panel are arranged below the propeller. The utility model discloses a separate driving system and the control system who adjusts unmanned aerial vehicle flight attitude, adopt the energy supply of oil driving system, realize unmanned aerial vehicle's big load and long continuation of the journey, improved agricultural unmanned aerial vehicle's work efficiency, set up X simultaneously and realize unmanned aerial vehicle flight state's adjustment to control panel and Y to simple structure reduces unmanned aerial vehicle's cost and fault rate.
Description
Technical field
The utility model is related to aircraft field more particularly to a kind of dynamical system and control system separate type aircraft.
Background technology
With the development of unmanned air vehicle technique, also answered in the sprinkling of the drug and liquid chemical fertilizer of crops
With.During pesticide spraying, national standard has particular provisions for the spray concentration of unit tree and grass coverage, and this requires nothings
The man-machine flying speed when spraying drug cannot be too fast, and in extensive sprinkling, unmanned plane will have heavy－duty and long continuation of the journey energy
Power.
It is recorded according to the prior art, the unmanned plane applied to pesticide spraying is mostly multi-rotor unmanned aerial vehicle, but when using electric power
When driving agricultural multi-rotor unmanned aerial vehicle, payload and cruising ability wretched insufficiency, when using oily power drive, generally
Variable-pitch propeller is used to adjust unmanned plane during flying state, but variable-pitch propeller complicated, of high cost, high failure rate.
Utility model content
In order to solve the above technical problems, a kind of dynamical system of the utility model offer and control system separate type aircraft,
Utilize the device of the utility model, it will thus provide the dynamical system of power and the control system of control unmanned plane during flying state are divided
From, it realizes the heavy－duty of agricultural unmanned plane with simple structure and grows and continue a journey, reduction unmanned plane cost and failure rate.
Technical solution is used by the utility model solves above-mentioned technical problem：
A kind of dynamical system and control system separate type aircraft, including：Pedestal, horizontal gird, oily dynamical system, oil are dynamic
Force transmission mechanism, propeller, Y-direction control panel, X are to control panel, pesticide box, pesticide delivery conduit and pesticide injection pipe
Road；The pedestal supports the horizontal gird, the propeller to be mounted on the horizontal gird；It is described oil dynamical system include
Fuel reserve tank and the dynamic engine of oil, the dynamic engine of oil drive the propeller to rotate by the oily power drive mechanism；Institute
Y is stated to be mounted below the propeller to control panel to control panel and the X.
In a preferred embodiment, the horizontal gird is Y-direction horizontal gird, several described propellers are in institute
It states and is uniformly distributed in "-" type on Y-direction horizontal gird, and the midpoint of the relatively described Y-direction horizontal gird of several described propellers is left
It is right symmetrical.
In a preferred embodiment, Y-direction horizontal rotating shaft, the Y-direction are provided with below the Y-direction horizontal gird
Horizontal rotating shaft includes the just half section of shaft being mutually rotatablely connected and minus half section of shaft；Just half section of shaft turns with described minus half section
Axis is respectively fixedly connected with one piece of Y-direction control panel；Just half section of shaft and minus half section of shaft by different servo drivings, into
And drive the forward and reverse rotation of Y-direction control panel respectively connected.
In a preferred embodiment, the centre of the Y-direction horizontal gird, Y-direction horizontal rotating shaft, Y-direction control panel
Position is both provided with folding fastener.
In a preferred embodiment, the oily power drive mechanism includes shaft, driving wheel, driven wheel and transmission
Band, the dynamic engine of oil by the shaft drive the driving wheel, by drive the driven wheel rotation, the driving wheel
Be respectively arranged with rotary middle spindle with the center of the driven wheel, the rotary middle spindle in the closest propeller
The transmission belt is socketed between heart shaft；The Y into the left and right sides of horizontal gird, the adjacent propeller of homonymy
The transmission belt is socketed between central rotating shaft.
In a preferred embodiment, the dynamic engine of the setting oil below the oily power drive mechanism, it is described
For setting X to fuel reserve tank bottom plate, the X is symmetrically set with oil storage to fuel reserve tank bottom plate upper edge midpoint below the dynamic engine of oil
Case.
In a preferred embodiment, the X is provided with two pieces in collinear to fuel reserve tank bottom plate lower section
The X is to control panel.
In a preferred embodiment, the pesticide box is arranged in the centre position of the Y-direction horizontal gird, described
Pesticide injection pipe is arranged below unmanned plane, and the pesticide delivery conduit is arranged along unmanned plane surrounding and connects the pesticide box
With the pesticide injection pipe, the pesticide injection pipe lower section is provided with injection trepanning.
In a preferred embodiment, it is cavity body structure below the Y-direction horizontal gird, it is the driving wheel, driven
Wheel and the transmission belt are built in the cavity body structure.
In a preferred embodiment, when unmanned plane hovers vertically, the Y rotates in same direction to control panel around Y-axis
Realize that rotary balance of the complete machine around Y-axis, the incorgruous rotation of Y-direction control panel realize the rotary balance of complete machine about the z axis, the X
The rotary balance for realizing complete machine around X-axis is rotate in same direction around X-axis to control panel；When unmanned plane is moved along X-direction, the Y-direction
Control panel substantially rotates in same direction with the Y-direction horizontal rotating shaft around Y-axis；When unmanned plane is moved along Y direction, the X is to control
Panel substantially rotates in same direction around X-axis；Unmanned plane is in VTOL, by the throttle tune for increasing or reducing the dynamic engine of the oil
Save revolution speed of propeller.
The utility model has the beneficial effects that：
The utility model is by detaching dynamical system with the control structure of adjustment unmanned plane during flying posture, using oily power
System energizes, and realizes the heavy－duty of unmanned plane and long continuation of the journey, has improved the working efficiency of agriculture unmanned plane, while X is arranged
The adjustment that unmanned plane during flying state is realized to control panel and Y-direction control panel, with simple structure reduce the cost of unmanned plane with
And failure rate.
Description of the drawings
The utility model is described further with reference to the accompanying drawings and examples.
Fig. 1 is the composed structure schematic diagram of the utility model one embodiment；
Fig. 2 is the composed structure schematic diagram of another angle of the utility model Fig. 1 embodiments；
Fig. 3 is the schematic diagram of one embodiment of the utility model oil power drive mechanism.
Specific implementation mode
The technique effect of the design of the utility model, concrete structure and generation is carried out below with reference to embodiment and attached drawing
Clear, complete description, to be completely understood by the purpose of this utility model, scheme and effect.It should be noted that not conflicting
In the case of, the features in the embodiments and the embodiments of the present application can be combined with each other.
It should be noted that unless otherwise specified, when a certain feature is referred to as " fixing ", " connection " is in another feature,
It can directly fix, be connected in another feature, can also fix, be connected in another feature indirectly.In addition, this
The descriptions such as the upper and lower, left and right used in utility model are only the phase relative to each component part of the utility model in attached drawing
For mutual position relationship.
In addition, unless otherwise defined, the technology of all of technologies and scientific terms used here by the article and the art
The normally understood meaning of personnel is identical.Term used in the description is intended merely to description specific embodiment herein, without
It is to limit the utility model.Term " and or " used herein includes appointing for one or more relevant Listed Items
The combination of meaning.
Fig. 1 is the composed structure schematic diagram of the utility model one embodiment, and referring to Fig.1, which is with control
System separate type aircraft include：
Pedestal 1, Y-direction horizontal gird 2, fuel reserve tank 3, the dynamic engine 4 of oil, oily power drive mechanism 5, propeller 6, Y-direction control
Panel 7 processed, X are rolled over to control panel 8, pesticide box 9, pesticide delivery conduit 10, pesticide injection pipe 11, Y-direction horizontal rotating shaft 12
Folded 13, the X that detains is to fuel reserve tank bottom plate 14, annular duct 15, cavity body structure 16 and controller 17.
X-axis, Y-axis and Z-direction mentioned in the utility model is as shown in fig. 1.
In the present invention, as shown in Figure 1,1 support level crossbeam of pedestal, propeller 6 are mounted on horizontal gird；Oil
Dynamical system includes fuel reserve tank 3 and the dynamic engine 4 of oil, and the dynamic engine 4 of oil drives propeller 6 to revolve by oily power drive mechanism 5
Turn, the VTOL of unmanned plane is realized by the rotation of propeller 6；Y-direction control panel 7 and X is mounted on spiral to control panel 8
6 lower section of paddle, Y-direction control panel 7 and X is rotated to control panel 8 under the driving effect of steering engine (not shown), and then is adjusted
The flight attitude of whole unmanned plane.
The utility model is by detaching dynamical system with the control system of adjustment unmanned plane during flying posture, using oily power
System energizes, and realizes the heavy－duty of unmanned plane and long continuation of the journey, has improved the working efficiency of agriculture unmanned plane, while X is arranged
To control panel and Y-direction control panel, realize the adjustment of unmanned plane during flying state, with simple structure reduce the cost of unmanned plane with
And failure rate.
In the present embodiment, it is preferable that as shown in Figure 1, horizontal gird is Y-direction horizontal gird 2, several propellers 6 are in Y-direction
It is uniformly distributed in "-" type on horizontal gird 2, and several propellers 6 are symmetrical with respect to the midpoint of Y-direction horizontal gird 2.It is excellent
Selection of land is provided with even number propeller 6 (propeller quantity is greater than or equal to 2n, and n takes positive integer), the list of Y-direction horizontal gird 2
Side is provided with n propeller, and the propeller 6 that Y is arranged on horizontal gird is with respect to the symmetrical distribution in midpoint).It selects herein
The sprinkling demand that a horizontal gird disclosure satisfy that agricultural unmanned plane is arranged in one specific direction, and simplifies structure, mitigates
Unmanned plane body weight；Certainly the distribution of horizontal gird is not specifically limited with quantity herein, as long as can guarantee unmanned plane machine
The basic stability of equilibrium of body.Several propellers 6 word order and opposite Y-direction level on Y-direction horizontal gird 2
The symmetrical distribution in midpoint of crossbeam 2 can ensure that fuselage balances to the full extent.In the present embodiment, propeller 6 is provided with 4
It is a, along the midpoint of Y-direction horizontal gird 2 symmetrically respectively distribution there are two.
It is preferred that being provided with annular duct 15 in the top of each propeller 6, annular duct 15 can be in spiral
The lift of bigger is promoted in the rotation process of paddle 6 for unmanned plane.
In the present embodiment, it is preferable that 2 lower section of Y-direction horizontal gird is provided with Y-direction horizontal rotating shaft 12, and Y-direction horizontal rotating shaft 12 wraps
The just half section of shaft 121 and minus half section of shaft 122, just half section of shaft 121 for including rotation connection are fixedly connected with one piece of Y-direction control plane
Plate 7, minus half section of shaft 122 are fixedly connected with another piece of Y-direction control panel 7；Just half section of shaft 121 is distinguished with minus half section of shaft 122
By different servo drivings, and then drive 7 positive and negative rotation of Y-direction control panel respectively connected.
The rotating manner of Y-direction control panel 7 is not specifically limited herein, as long as Y-direction control panel 7 can be made to be adjusted by rotating
The state of flight of whole unmanned plane, it is simple in structure herein in such a way that shaft is driven control panel 7 to rotate by servo driving.
Herein, it is preferable that just half section of shaft 121, minus half section of shaft 122 are respectively integrally formed with one piece of Y-direction control panel 7,
The globality of structure is promoted.
In the present embodiment, it is preferable that Y-direction horizontal gird 2, Y-direction horizontal rotating shaft 12, Y-direction control panel 7 intermediate position
It is both provided with folding fastener, makes unmanned plane is foldable in transportational process to pack up, storage and transportation is more convenient, opens again when in use solid
It is fixed.
In the present embodiment, as shown in Figure 3, it is preferable that oily power drive mechanism 5 include shaft 501, driving wheel 502, from
Driving wheel 503 and transmission belt 504, the dynamic engine 4 of oil rotate, and drive driving wheel 502 to rotate by shaft 501, driving wheel 502 with
Driven wheel 503 engages, and driven wheel 503 rotates；Driving wheel 502 and the center of driven wheel 503 are respectively arranged with rotary middle spindle
505, it is socketed with transmission belt 504 between rotary middle spindle 505 and the central rotating shaft 601 of closest propeller 6；Y is horizontal to level
In the left and right sides of beam 2, transmission belt 504 is socketed between the central rotating shaft 601 of homonymy adjoining spiral paddle 6.
The structure and mode of oily power transmission arrangment 5 are not specifically limited herein, the modes such as chain drive can also be passed through
It is driven.
In the present embodiment, it is preferable that the 5 dynamic engine 4 of lower section setting oil of oily power drive mechanism, dynamic 4 lower section of engine of oil
X is set to fuel reserve tank bottom plate 14, X is symmetrically set with fuel reserve tank 3 to 14 upper edge midpoint of fuel reserve tank bottom plate.It can so make oil dynamic
Engine 4 and 501 direct-drive of shaft in oily power drive mechanism 5.Fuel reserve tank 3, which is symmetrical arranged, to be conducive to ensure unmanned plane
The balance of fuselage.
In the present embodiment, it is preferable that X is provided with two pieces to 14 lower section of fuel reserve tank bottom plate and is in collinear X to control
Panel 8, control panel 8 can be rotated by the driving of motor (not shown) around X-axis, and then adjust the state of flight of unmanned plane.
In the present embodiment, Y-direction control panel 7 and X is respectively positioned on the underface of propeller 6 to control panel 8, and propeller 6 produces
Raw air-flow makes the control panel of unmanned plane regulate and control unhinderedly directly through Y to control panel 7 and X to control panel 8
When it is more efficient also more flexible.
In the present embodiment, it is preferable that pesticide box 9 is arranged in the centre position of Y-direction horizontal gird 2, pesticide injection pipe 11
It is arranged below unmanned plane, pesticide delivery conduit 10 is arranged along unmanned plane surrounding, connection pesticide box 9 and pesticide injection pipe 11；
11 lower section of pesticide injection pipe is provided with injection trepanning.Pesticide injection pipe 11 is arranged below unmanned plane, pesticide can be made to exist
Under the collective effect for the downdraught that dead weight and propeller 6 generate, directly it is sprayed onto on crops；10 edge of pesticide delivery conduit
Unmanned plane surrounding is arranged, rather than between interspersed propeller 6 and control panel, it can be to avoid the interference to air-flow.
In the present embodiment, it is preferable that the lower section of Y-direction horizontal gird 2 is cavity body structure 16, driving wheel 502, driven wheel 503
And transmission belt 504 is built in cavity body structure 16.Cavity body structure 16 is to internal driving wheel 502, driven wheel 503 and passes
Dynamic band 504 plays a protective role, and prevents above-mentioned transmission parts from working in the weather to expose to the sun and rain for a long time, and corrosion and damage occurs
It is bad.
In the present embodiment, the state of flight of unmanned plane is as follows：
During taking off vertically, oil moves engine 4 and starts unmanned plane, increases the throttle that oil moves engine 4, and oil moves hair
Motivation 4 drives propeller 6 to rotate by oily power drive mechanism 5, when the lift that propeller 6 generates, which is more than unmanned plane, conducts oneself with dignity,
Unmanned plane takes off vertically；When unmanned plane wants vertical landing, the throttle of engine 4 is moved by reducing oil, the rotating speed of propeller 6 becomes
Slowly, the lift of generation reduces, when lift is gradually less than dead weight, the gradual vertical landing of unmanned plane；Y-direction horizontal gird 2 is along midpoint
Symmetrical propeller 6 rotates backward, to offset the turning moment of unmanned plane complete machine.
When the lift that propeller 6 generates, which is equal to unmanned plane, conducts oneself with dignity, unmanned plane hovering, Y-direction control panel 7 is around Y-axis at this time
It rotates synchronously, realizes that rotary balance of the complete machine around Y-axis, Y-direction control panel 7 realize the rotation of complete machine about the z axis around the incorgruous rotation of Y-axis
Balance, X rotate in same direction to control panel 8, realize rotary balance of the complete machine around X-axis；Entire balance and stability process passes through controller
17 are adjusted, it is preferable that controller 17 is located at drone center of unmanned aerial vehicle position.
When unmanned plane is moved along X-axis positive direction, Y-direction control panel 7 substantially rotates in same direction with Y-direction horizontal rotating shaft 12 around Y-axis,
Rotation direction is to be rotated counterclockwise in terms of Y-axis positive direction, and unmanned plane is integrally by from the torsion clockwise in terms of Y-axis positive direction at this time
Square, unmanned plane generate inclination, and the lift that propeller 6 generates can generate a component in X-axis positive direction, drive unmanned plane along X-axis
Forward direction is mobile；Unmanned plane moves similarly along X-axis negative direction.
When unmanned plane is moved along Y-axis positive direction, X substantially rotates in same direction to control panel 8 around X-axis；Rotation direction is from X-axis
Positive direction, which is seen, to be rotated counterclockwise, and unmanned plane integrally by from the clockwise torque in terms of X-axis positive direction, incline by unmanned plane generation at this time
Tiltedly, the lift that propeller 6 generates can generate a component in Y-axis positive direction, and unmanned plane is driven to be moved along Y-axis forward direction；Unmanned plane
It is moved similarly along Y-axis negative direction.
It is to be illustrated to the preferable implementation of the utility model, but the utility model creation is not limited to institute above
Embodiment is stated, those skilled in the art can also make various be equal without departing from the spirit of the present invention
Deformation is replaced, these equivalent deformations or replacement are all contained in the application claim limited range.
Claims (10)
1. a kind of dynamical system and control system separate type aircraft, which is characterized in that including：Pedestal, horizontal gird, oily power
System, oily power drive mechanism, propeller, Y-direction control panel, X are to control panel, pesticide box, pesticide delivery conduit and agriculture
Medicine injection pipe；The pedestal supports the horizontal gird, the propeller to be mounted on the horizontal gird；The oil power
System includes fuel reserve tank and the dynamic engine of oil, and the dynamic engine of oil drives the propeller by the oily power drive mechanism
Rotation；The Y-direction control panel is mounted on to control panel below the propeller with the X.
2. dynamical system according to claim 1 and control system separate type aircraft, it is characterised in that：It is described horizontal horizontal
Beam is Y-direction horizontal gird, several described propellers are uniformly distributed on the Y-direction horizontal gird in "-" type, and several
The midpoint of the relatively described Y-direction horizontal gird of the propeller is symmetrical.
3. dynamical system according to claim 2 and control system separate type aircraft, it is characterised in that：The Y-direction water
Flat below the crossbeam is provided with Y-direction horizontal rotating shaft, and the Y-direction horizontal rotating shaft includes the just half section of shaft and negative half being mutually rotatablely connected
Section shaft；Just half section of shaft is respectively fixedly connected with one piece of Y-direction control panel with minus half section of shaft；Described just half section turns
Axis and minus half section of shaft are driven forward and reverse turn of the Y-direction control panel respectively connected by different servo drivings
It is dynamic.
4. dynamical system according to claim 3 and control system separate type aircraft, it is characterised in that：The Y-direction water
Flat crossbeam, Y-direction horizontal rotating shaft, Y-direction control panel intermediate position be both provided with folding fastener.
5. dynamical system according to claim 4 and control system separate type aircraft, it is characterised in that：The oil power
Transmission mechanism includes shaft, driving wheel, driven wheel and transmission belt, and the dynamic engine of oil drives the active by the shaft
It takes turns and then the driven wheel rotation, the center of the driving wheel and the driven wheel is driven to be respectively arranged with rotary middle spindle, institute
It states and is socketed with the transmission belt between rotary middle spindle and the central rotating shaft of the closest propeller；The Y-direction is horizontal horizontal
In the left and right sides of beam, the transmission belt is socketed between the central rotating shaft of the adjacent propeller of homonymy.
6. dynamical system according to claim 5 and control system separate type aircraft, it is characterised in that：The oil power
The dynamic engine of the setting oil below transmission mechanism, setting X is to fuel reserve tank bottom plate below the dynamic engine of oil, and the X is to storage
Oil tank bottom plate upper edge midpoint is symmetrically set with fuel reserve tank.
7. dynamical system according to claim 6 and control system separate type aircraft, it is characterised in that：The X is to storage
It is provided with two pieces below oil tank bottom plate and is in the collinear X to control panel.
8. the dynamical system and control system separate type aircraft, feature according to any one of claim 2 to 7 exist
In：The pesticide box is arranged in the centre position of the Y-direction horizontal gird, and the pesticide injection pipe is arranged under unmanned plane
Side, the pesticide delivery conduit are arranged along unmanned plane surrounding and connect the pesticide box and the pesticide injection pipe, the agriculture
It is provided with injection trepanning below medicine injection pipe.
9. dynamical system according to claim 5 and control system separate type aircraft, it is characterised in that：The Y-direction water
Flat below the crossbeam is cavity body structure, and the driving wheel, driven wheel and the transmission belt are built in the cavity body structure.
10. according to claim 1 to 7, the dynamical system described in any one of claim 9 is flown with control system separate type
Device, it is characterised in that：When unmanned plane hovers vertically, the Y-direction control panel rotates in same direction around Y-axis realizes that complete machine turns around Y-axis
Dynamic balancing, the incorgruous rotation of Y-direction control panel realize that the rotary balance of complete machine about the z axis, the X are same around X-axis to control panel
Rotary balance of the complete machine around X-axis is realized to rotation；When unmanned plane is moved along X-direction, the Y-direction control panel is with the Y-direction
Horizontal rotating shaft substantially rotates in same direction around Y-axis；When unmanned plane is moved along Y direction, the X is substantially in the same direction around X-axis to control panel
Rotation；Unmanned plane is in VTOL, by the throttle adjustment revolution speed of propeller for increasing or reducing the dynamic engine of the oil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721565999.XU CN207683776U (en) | 2017-11-21 | 2017-11-21 | Power system and control system disconnect-type aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721565999.XU CN207683776U (en) | 2017-11-21 | 2017-11-21 | Power system and control system disconnect-type aircraft |
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| Publication Number | Publication Date |
|---|---|
| CN207683776U true CN207683776U (en) | 2018-08-03 |
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ID=62998282
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| Application Number | Title | Priority Date | Filing Date |
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| CN201721565999.XU Active CN207683776U (en) | 2017-11-21 | 2017-11-21 | Power system and control system disconnect-type aircraft |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108001672A (en) * | 2017-11-21 | 2018-05-08 | 南方科技大学 | Power system and control system disconnect-type aircraft |
| CN113289812A (en) * | 2021-06-08 | 2021-08-24 | 合肥工业大学 | Suspension type spraying robot for spraying complex surface |
-
2017
- 2017-11-21 CN CN201721565999.XU patent/CN207683776U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108001672A (en) * | 2017-11-21 | 2018-05-08 | 南方科技大学 | Power system and control system disconnect-type aircraft |
| CN113289812A (en) * | 2021-06-08 | 2021-08-24 | 合肥工业大学 | Suspension type spraying robot for spraying complex surface |
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