CN207994897U - Governor, aircraft governing system and aircraft - Google Patents
Governor, aircraft governing system and aircraft Download PDFInfo
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- CN207994897U CN207994897U CN201820512942.1U CN201820512942U CN207994897U CN 207994897 U CN207994897 U CN 207994897U CN 201820512942 U CN201820512942 U CN 201820512942U CN 207994897 U CN207994897 U CN 207994897U
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Abstract
The utility model is related to vehicle technology fields, more particularly, to a kind of governor, aircraft governing system and aircraft.The governor, including magnetic conduction stator, active magnetic conduction rotor, passive magnetic conduction rotor；It is provided with magnetic coil on the magnetic conduction stator, the first magnetizer is provided on the active magnetic conduction rotor, the second magnetizer is provided on the passive magnetic conduction rotor；The active magnetic conduction rotor can drive the passive magnetic conduction rotor rotation.The aircraft governing system, including the governor.The aircraft, including the aircraft governing system.Contactless torque transmission may be implemented in the utility model, reduces mechanical loss.
Description
Technical field
The utility model is related to vehicle technology fields, more particularly, to a kind of governor, aircraft governing system and fly
Row device.
Background technology
Existing aircraft, in rotor wing unmanned aerial vehicle, the speed governing to paddle shaft is realized by contact torque transfer mostly
, but this transfer mode be easy to cause the mechanical loss of transmission parts.
Utility model content
It is existing to solve the purpose of this utility model is to provide a kind of governor, aircraft governing system and aircraft
In rotor wing unmanned aerial vehicle present in technology, the speed governing of paddle shaft is realized by contact torque transfer mostly, but this biography
The mode of passing be easy to cause the technical issues of mechanical loss of transmission parts.
The utility model provides a kind of governor, including magnetic conduction stator, active magnetic conduction rotor, passive magnetic conduction rotor；Institute
It states and is provided with magnetic coil on magnetic conduction stator, the first magnetizer is provided on the active magnetic conduction rotor, the passive magnetic conduction turns
The second magnetizer is provided on son；The active magnetic conduction rotor can drive the passive magnetic conduction rotor rotation.
In any of the above-described technical solution, further, the active magnetic conduction rotor in a tubular form, and first magnetizer
It is fixed on the active magnetic conduction rotor；In a tubular form, and second magnetizer is fixed on the quilt to the passive magnetic conduction rotor
On dynamic magnetic conduction rotor.
In any of the above-described technical solution, further, the passive magnetic conduction rotor is sheathed on the active magnetic conduction rotor
On, the active magnetic conduction rotor is sheathed on the magnetic conduction stator；
Or, the magnetic conduction stator is around the circumferentially disposed of the active magnetic conduction rotor, the active magnetic conduction rotor is around the quilt
Move the circumferentially disposed of magnetic conduction rotor.
Further include active rotating shaft further, the active rotating shaft is led with the active in any of the above-described technical solution
Magnet rotor is fixedly connected, and the active rotating shaft is for driving the active magnetic conduction rotor to rotate.
Further include output shaft further in any of the above-described technical solution, the output shaft turns with the passive magnetic conduction
Son is fixedly connected, and the passive magnetic conduction rotor is for driving the output shaft to rotate.
In any of the above-described technical solution, further, the material of the active magnetic conduction rotor is plastics or light-weight metal；
The material of the passive magnetic conduction rotor is plastics or light-weight metal.
In any of the above-described technical solution, further, the plastics are ABS plastic；The light-weight metal is aluminium, aluminium U.S.
Alloy, magnesium alloy or titanium alloy.
Further include shell further in any of the above-described technical solution, the magnetic conduction stator, the active magnetic conduction turn
The sub and described passive magnetic conduction rotor may be contained in the inner cavity of the shell.
The utility model additionally provides a kind of aircraft governing system, including the governor.
The utility model additionally provides a kind of aircraft, including the aircraft governing system.
Compared with prior art, the beneficial effects of the utility model are：
Governor provided by the utility model, including magnetic conduction stator, active magnetic conduction rotor, passive magnetic conduction rotor；It is described to lead
It is provided with magnetic coil on magnetic stator, is provided with the first magnetizer on the active magnetic conduction rotor, on the passive magnetic conduction rotor
It is provided with the second magnetizer；The active magnetic conduction rotor can drive the passive magnetic conduction rotor rotation.By making magnetic coil
It is powered, so that it generates magnetic field, magnetic attraction force is conducted to active magnetic conduction rotor, and active magnetic conduction rotor leans on magnetic attraction force in the running
Effect drive the operating of driven magnetic conduction rotor, to realize contactless torque transmission, reduce mechanical loss.In addition, due to master
Dynamic magnetic conduction rotor be realize magnetic conduction in such a way that the first magnetizer is installed, therefore can reduce on active magnetic conduction rotor the
The weight of one magnetizer and light material may be used active magnetic conduction rotor is made；On passive magnetic conduction rotor can be reduced
The weight of two magnetizers and light material may be used passive magnetic conduction rotor is made, so as to mitigate and optimize governor entirety
Weight.
The aircraft governing system that the utility model also provides, including the governor.It is found that it should based on above-mentioned analysis
Aircraft governing system may be implemented contactless torque transmission, reduce mechanical loss.
The aircraft that the utility model also provides, including the aircraft governing system.It is found that it should based on above-mentioned analysis
Aircraft may be implemented contactless torque transmission, reduce mechanical loss.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific implementation mode or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, other drawings may also be obtained based on these drawings.
Fig. 1 is that governor is installed on the sectional view on horn in the utility model embodiment；
Fig. 2 is the enlarged drawing at A in Fig. 1；
Fig. 3 is that governor is installed on the structural schematic diagram on horn in the utility model embodiment；
Fig. 4 is the enlarged drawing at B in Fig. 3；
Fig. 5 is the internal structure schematic diagram of governor in the utility model embodiment；
Fig. 6 is the enlarged drawing at C in Fig. 5；
Fig. 7 is the structural schematic diagram of active magnetic conduction rotor in the utility model embodiment；
Fig. 8 is the structural schematic diagram of passive magnetic conduction rotor in the utility model embodiment；
Fig. 9 is structural schematic diagram when being equipped with the first magnetizer in the utility model embodiment on active magnetic conduction rotor；
Figure 10 is structural schematic diagram when being equipped with the second magnetizer in the utility model embodiment on passive magnetic conduction rotor；
Figure 11 is the structural schematic diagram of the first magnetizer in the utility model embodiment；
Figure 12 is the structural schematic diagram of magnetic conduction stator in the utility model embodiment.
In figure：
101- magnetic conduction stators；102- active magnetic conduction rotors；The passive magnetic conduction rotors of 103-；104- magnetic coils；105- first
Embedded groove；106- arc convex；The second embedded grooves of 107-；108- arc grooves；109- protecgulums；110- rear covers；111- shells；
112- first bearings；113- second bearings；114- active rotating shafts；115- output shafts；116- drive bevel gears；117- horns；
118- power supply connectors；The first magnetizers of 119-；The second magnetizers of 120-；121- limits the shaft shoulder.
Specific implementation mode
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.
It usually here can be with a variety of different with the component of the utility model embodiment shown described in attached drawing
It configures to arrange and design.Therefore, the detailed description of the embodiments of the present invention to providing in the accompanying drawings is not purport below
In the claimed the scope of the utility model of limitation, but it is merely representative of the selected embodiment of the utility model.
Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.In addition, term " the
One ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, can also be electrical connection；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, it can understand above-mentioned art with concrete condition
The concrete meaning of language in the present invention.
Embodiment one
Shown in Fig. 1 to Figure 12, the utility model embodiment one provides a kind of governor, including magnetic conduction stator 101,
Active magnetic conduction rotor 102, passive magnetic conduction rotor 103；Magnetic coil 104, active magnetic conduction rotor are provided on magnetic conduction stator 101
It is provided with the first magnetizer on 102, the second magnetizer is provided on passive magnetic conduction rotor 103；Active magnetic conduction rotor 102 being capable of band
Dynamic passive magnetic conduction rotor 103 rotates.
Specifically, magnetic coil 104 is wound on magnetic conduction stator 101, magnetic coil 104 after powered up, can generate
Magnetic field.Magnetic coil 104 is multigroup, that is to say, that is wound on magnetic conduction stator 101 is 104 groups of magnetic coil.
It should be noted that canoe of the magnetic coil 104 on magnetic conduction stator 101 can twine according to actual needs
Around.
The tune governor that the embodiment provides, by making magnetic coil 104 be powered, so that it generates magnetic field, magnetic attraction force
It is conducted to active magnetic conduction rotor 102, active magnetic conduction rotor 102 leans on the effect of magnetic attraction force to drive driven magnetic conduction rotor in the running
Operating reduces mechanical loss to realize contactless torque transmission.In addition, since active magnetic conduction rotor 102 is to pass through installation
The mode of first magnetizer realizes magnetic conduction, therefore can reduce the weight of the first magnetizer on active magnetic conduction rotor 102 simultaneously
And light material may be used, active magnetic conduction rotor 102 is made；The second magnetizer on passive magnetic conduction rotor 103 can be reduced
Weight and light material may be used passive magnetic conduction rotor 103 is made, so as to mitigate and optimize the weight of governor entirety
And reduce the volume of governor.
In the optional scheme of the embodiment, in a tubular form, and the first magnetizer is fixed on active magnetic conduction to active magnetic conduction rotor 102
On rotor 102；In a tubular form, and the second magnetizer is fixed on passive magnetic conduction rotor 103 passive magnetic conduction rotor 103.
Specifically, the circumferential direction of active magnetic conduction rotor 102 has multiple first embedded grooves 105, multiple first embedded grooves 105
Between be evenly spaced on, that is to say, that the angle of circumference between two neighboring first embedded groove 105 is identical；First magnetizer is embedding
Enter in the first embedded groove 105, the length extending direction of the first embedded groove 105 is parallel with the axial direction of active magnetic conduction rotor 102；The
All have arc convex 106 on two opposite side arms of one embedded groove 105, the arc convex 106 in the first embedded groove 105 with
Arc groove 108 on first magnetizer matches；The length extending direction of arc convex 106 in first embedded groove 105 with
The length extending direction of first embedded groove 105 is parallel.
The circumferential direction of passive magnetic conduction rotor 103 has multiple second embedded grooves 107, between multiple second embedded grooves 107 uniformly
It is spaced apart, that is to say, that the angle of circumference between two neighboring second embedded groove 107 is identical；The insertion second of second magnetizer is embedding
Enter in slot 107, the length extending direction of the second embedded groove 107 is parallel with the axial direction of passive magnetic conduction rotor 103；Second embedded groove
Arc convex 106, the arc convex 106 in the second embedded groove 107 and the second magnetic conduction are all had on 107 two opposite side arms
Arc groove 108 on body matches；The length extending direction of arc convex 106 in second embedded groove 107 and the second insertion
The length extending direction of slot 107 is parallel.
In the optional scheme of the embodiment, the quantity of the first embedded groove 105 is 6~10；The quantity of second embedded groove 107
It is 6~10.The quantity of first embedded groove 105 is equal with the quantity of the first magnetizer；The quantity and second of second embedded groove 107
The quantity of magnetizer is equal.
In the optional scheme of the embodiment, passive magnetic conduction rotor 103 is sheathed on active magnetic conduction rotor 102, active magnetic conduction
Rotor 102 is sheathed on magnetic conduction stator 101, that is to say, that active guide sleeve rotor is sleeved on the outside of magnetic conduction stator 101, passively leads
Magnet rotor 103 is sleeved on the outside of active magnetic conduction rotor 102.It should be noted that in the embodiment, magnetic conduction stator can also be made
101 around the circumferentially disposed of active magnetic conduction rotor 102, and active magnetic conduction rotor 102 is circumferentially disposed around passive magnetic conduction rotor 103, that is,
Active magnetic conduction rotor 102 is sleeved on the outside of passive magnetic conduction rotor 103, and magnetic conduction stator 101 is sleeved on the outer of active magnetic conduction rotor 102
Portion.
In the optional scheme of the embodiment, governor further includes shell 111, magnetic conduction stator 101, active magnetic conduction rotor 102
In the inner cavity that may be contained within shell 111 with passive magnetic conduction rotor 103.
Specifically, the front end of shell 111 is equipped with protecgulum 109, the rear end of shell 111 is equipped with rear cover 110, Yi Jibian
Closing chamber is formed in the inside of shell 111, the inside of shell 111 can be entered to avoid impurity such as dusts in this way.Protecgulum 109 with it is outer
It is provided with gasket between shell 111, gasket is provided between rear cover 110 and shell 111.
In the optional scheme of the embodiment, governor further includes active rotating shaft 114, and active rotating shaft 114 turns with active magnetic conduction
Son 102 is fixedly connected, and active rotating shaft 114 is for driving active magnetic conduction rotor 102 to rotate.
Specifically, magnetic conduction stator 101 is in a tubular form, active rotating shaft 114 passes through the inside of magnetic conduction stator 101, and actively
After shaft 114 is pierced by from the inside of magnetic conduction stator 101, active rotating shaft 114 is fixedly connected with the end of active magnetic conduction rotor 102.
In order to improve the stability in 114 rotation process of active rotating shaft, it is arranged between active rotating shaft 114 and the inside of magnetic conduction stator 101
There is first bearing 112, wherein the outer ring of first bearing 112 is fixedly connected with the inside of magnetic conduction stator 101, first bearing 112
Inner ring is fixedly connected with active rotating shaft 114.The quantity of first bearing 112 can be multiple, to further increase stability.Magnetic conduction
Stator 101 is fixedly connected by screw with rear shell.
In the optional scheme of the embodiment, governor further includes output shaft 115, output shaft 115 and passive magnetic conduction rotor 103
It is fixedly connected, and passive magnetic conduction rotor 103 is for driving output shaft 115 to rotate.
Specifically, after output shaft 115 passes through rear cover 110, output shaft 115 and the end of passive magnetic conduction rotor 103 are fixed
Connection.In order to improve the stability in 115 rotation process of output shaft, second bearing is provided between output shaft 115 and protecgulum 109
113, wherein the outer ring of second bearing 113 is fixedly connected with protecgulum 109, and inner ring and the output shaft 115 of second bearing 113 are fixed
Connection.The quantity of second bearing 113 can be multiple, to further increase stability.Second bearing 113 is embedded in protecgulum 109.
In the optional scheme of the embodiment, the material of active magnetic conduction rotor 102 is plastics or light-weight metal；Passive magnetic conduction turns
The material of son 103 is plastics or light-weight metal.
Specifically, plastics are ABS plastic；Light-weight metal is aluminium, aluminium U.S. alloy, magnesium alloy or titanium alloy.
It should be noted that plastics can be with any one in POM, PS, PMMA, PC, PET, PBT or PPO.Actively lead
The material of magnet rotor 102 can also be ceramics, and the material of passive magnetic conduction rotor 103 can also be ceramics, and ceramics are that zirconium oxide is made pottery
Porcelain.
In the optional scheme of the embodiment, when the material of active magnetic conduction rotor 102 is light-weight metal and passive magnetic conduction rotor
When 103 material is light-weight metal, the first magnetizer can be linked together with active magnetic conduction rotor 102 by casting craft；
Second magnetizer is linked together with passive magnetic conduction rotor 103 by casting craft.The structure of first magnetizer and the second magnetic conduction
The structure of body is identical.
Specifically, active magnetic conduction rotor 102 is high temperature aluminum water to be poured in mold or other metal waters are formed, and first
Magnetizer is embedded in mold in advance, is passed through together after the completion of pouring, then active magnetic conduction rotor 102 and the first pre-buried magnetizer
Mechanical processing forming.It should be noted that the formation process that the second magnetizer links together with passive magnetic conduction rotor 103, with
Active magnetic conduction rotor 102 is identical as the formation process that the first magnetizer links together, and is not repeated to illustrate；In addition, first leads
Magnet can also be that screw is connect with the connection type of active magnetizer rotor, the company of the second magnetizer and passive magnetizer rotor
The mode of connecing can also be that screw connects, and be conveniently replaceable the first magnetizer or the second magnetizer in this way.
In the optional scheme of the embodiment, the material of the first magnetizer is iron or steel.Magnetic coil 104 is the copper wire magnetic line of force
Circle 104.Magnetic conduction stator 101 is made of magnetic conductive metal.Shell 111, rear cover 110 and protecgulum 109 are made of aluminum or aluminum alloy.
Shown in Figure 12, in the optional scheme of the embodiment, in a tubular form, the both ends of magnetic conduction stator have magnetic conduction stator 101
There is the limit shaft shoulder, for magnetic coil to be limited in magnetic conduction stator.
In the optional scheme of the embodiment, power supply connector 118 is installed on rear cover 110,104 groups of magnetic coil connects with power supply
Head electrical connection.
In the embodiment, the electric current on 104 groups of the magnetic coil of governor is bigger, and the magnetic attraction force of magnetic conduction stator 101 is got over
By force, magnetic attraction force is conducted to active magnetic conduction rotor 102, and active magnetic conduction rotor 102 leans on the effect of magnetic attraction force to drive in the running
Passive magnetic conduction rotor 103 operates, and when electric current maximum on 104 groups of magnetic coil, the magnetic field of governor active magnetic conduction rotor 102 is inhaled
Power is also maximum, and governor active magnetic conduction rotor 102 will be operated synchronously with the driven magnetic conduction rotor of governor；Conversely, governor winding
On electric current it is smaller, the magnetic attraction force on governor magnetic conduction is fixed is weaker, is conducted to 102 magnetic attraction force of active magnetic conduction rotor with regard to weak,
Low-intensity magnetic field suction is being conducted on passive magnetic conduction rotor 103 by the active magnetic conduction rotor 102 with low-intensity magnetic field suction, is passively being led
For magnet rotor 103 in the case where this weak magnetic attraction force drives, rotating speed will be many slowly.
It should be noted that in the embodiment, after the different size of electric current of governor input, active rotating shaft 114
It is little with relevance of the utility model the problem of solved with the rotating ratio between output shaft 115, no longer it is specifically described.
Embodiment two
It includes the governor that embodiment one provides that the utility model embodiment two, which provides a kind of aircraft governing system,.
Shown in Figure 2, in the embodiment, the protecgulum 109 of governor is fixedly connected with horn 117；Output shaft 115 it is another
One end is connected with drive bevel gear 116, wherein one end of output shaft 115 is connected with passive magnetic conduction rotor 103.
In the embodiment.It is connected between active rotating shaft 114 and engine, that is to say, that for unmanned plane, single engine
It can simultaneously be imparted power on the active rotating shaft of multiple and different governors by gear drive, it such as can be by power
On the active rotating shaft for passing to 8 different governors.
The aircraft governing system that the embodiment provides, can be used as power by monomotor or monomotor, pass through
Transmission mechanism passes to power on multiple and different governors, then the drive bevel gear 116 connected by different governors is transmitted to
Each positive paddle shaft or anti-paddle shaft.
It should be noted that the embodiment advantage is：One power can drive multiple paddle shafts by multiple governors
Speed governing can make each paddle shaft obtain different rotating speed in the case where the rotating speed that power source generates is constant by governor,
To control the flight of complete machine, when magnetic force reaches some strength, power transmission loss is almost nil.
Embodiment three
It includes the aircraft governing system that embodiment two provides that the utility model embodiment three, which provides a kind of aircraft,.
In conclusion governor, aircraft governing system and aircraft that the utility model embodiment provides realize nothing
Torque transfer is contacted, the mechanical loss of transmission parts is reduced.Engine or motor operation generate power, pass through transmission mechanism
Power is passed on governor, using governor adjust to setting speed, then the speed mixed up by output shaft 115,
It is transmitted to paddle shaft after drive bevel gear 116 and driven wheel of differential.
Finally it should be noted that：The above various embodiments is only to illustrate the technical solution of the utility model, rather than limits it
System；Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should
Understand：It still can be with technical scheme described in the above embodiments is modified, either to which part or whole
Technical characteristic carries out equivalent replacement；And these modifications or replacements, this practicality that it does not separate the essence of the corresponding technical solution are new
The range of each embodiment technical solution of type.In the instructions provided here, numerous specific details are set forth.However, can
Understand, the embodiments of the present invention can be put into practice without these specific details.In some instances, not in detail
Well known method, structure and technology are carefully shown, so as not to obscure the understanding of this description.In addition, those skilled in the art
It is understood that although some embodiments described herein include certain features included in other embodiments rather than other spies
Sign, but the combination of the feature of different embodiments means within the scope of the utility model and forms different implementation
Example.For example, in the following claims, the one of arbitrary of embodiment claimed can side in any combination
Formula uses.
Claims (10)
1. a kind of governor, which is characterized in that including magnetic conduction stator, active magnetic conduction rotor, passive magnetic conduction rotor；The magnetic conduction is fixed
It is provided with magnetic coil on son, the first magnetizer is provided on the active magnetic conduction rotor, is arranged on the passive magnetic conduction rotor
There is the second magnetizer；The active magnetic conduction rotor can drive the passive magnetic conduction rotor rotation.
2. governor according to claim 1, which is characterized in that the active magnetic conduction rotor in a tubular form, and described first
Magnetizer is fixed on the active magnetic conduction rotor；In a tubular form, and second magnetizer is fixed on the passive magnetic conduction rotor
On the passive magnetic conduction rotor.
3. governor according to claim 2, which is characterized in that the passive magnetic conduction rotor is sheathed on the active magnetic conduction
On rotor, the active magnetic conduction rotor is sheathed on the magnetic conduction stator；
Or, the magnetic conduction stator, around the circumferentially disposed of the active magnetic conduction rotor, the active magnetic conduction rotor is passively led around described
Magnet rotor it is circumferentially disposed.
4. governor according to any one of claim 1-3, which is characterized in that further include active rotating shaft, the active
Shaft is fixedly connected with the active magnetic conduction rotor, and the active rotating shaft is for driving the active magnetic conduction rotor to rotate.
5. governor according to any one of claim 1-3, which is characterized in that further include output shaft, the output shaft
It is fixedly connected with the passive magnetic conduction rotor, and the passive magnetic conduction rotor is for driving the output shaft to rotate.
6. governor according to any one of claim 1-3, which is characterized in that the material of the active magnetic conduction rotor is
Plastics or light-weight metal；The material of the passive magnetic conduction rotor is plastics or light-weight metal.
7. governor according to claim 6, which is characterized in that the plastics are ABS plastic；The light-weight metal is
Aluminium, aluminium U.S. alloy, magnesium alloy or titanium alloy.
8. governor according to any one of claim 1-3, which is characterized in that further include shell, the magnetic conduction stator,
The active magnetic conduction rotor and the passive magnetic conduction rotor may be contained in the inner cavity of the shell.
9. a kind of aircraft governing system, which is characterized in that include the governor as described in any one of claim 1-8.
10. a kind of aircraft, which is characterized in that including aircraft governing system as claimed in claim 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820512942.1U CN207994897U (en) | 2018-04-10 | 2018-04-10 | Governor, aircraft governing system and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820512942.1U CN207994897U (en) | 2018-04-10 | 2018-04-10 | Governor, aircraft governing system and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207994897U true CN207994897U (en) | 2018-10-19 |
Family
ID=63830782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820512942.1U Active CN207994897U (en) | 2018-04-10 | 2018-04-10 | Governor, aircraft governing system and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207994897U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108462367A (en) * | 2018-04-10 | 2018-08-28 | 辽宁壮龙无人机科技有限公司 | Governor, aircraft governing system and aircraft |
-
2018
- 2018-04-10 CN CN201820512942.1U patent/CN207994897U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108462367A (en) * | 2018-04-10 | 2018-08-28 | 辽宁壮龙无人机科技有限公司 | Governor, aircraft governing system and aircraft |
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Address after: No. 76-45, Shenbei Road, Shenbei New District, Shenyang City, Liaoning Province 110000 Patentee after: Liaoning Dazhuang UAV Technology Co.,Ltd. Address before: No. 76-43, Shenbei Road, Shenyang City, Liaoning Province 110000 (Gate A) Patentee before: LIAONING ZHUANGLONG UNMANNED AERIAL VEHICLE TECHNOLOGY Co.,Ltd. |