CN206885335U - A kind of unmanned plane undercarriage and unmanned plane - Google Patents
A kind of unmanned plane undercarriage and unmanned plane Download PDFInfo
- Publication number
- CN206885335U CN206885335U CN201720512168.XU CN201720512168U CN206885335U CN 206885335 U CN206885335 U CN 206885335U CN 201720512168 U CN201720512168 U CN 201720512168U CN 206885335 U CN206885335 U CN 206885335U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- expansion link
- undercarriage
- motor
- telescopic component
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
A kind of unmanned plane undercarriage and unmanned plane provided by the utility model, including at least one telescopic component and at least one fixation kit；The telescopic component includes motor and at least expansion link of two-stage；The expansion link is by the driving of the motor and axial stretching；The telescopic component is connected with the fixation kit, for being fixed by the fixation kit with unmanned plane.In the above-mentioned technical solutions, the undercarriage of unmanned plane is regarded using expansion link, instead of T-shaped unmanned plane undercarriage of the prior art, the shielded area of undercarriage can be reduced, making unmanned plane, camera, which can capture, can more shoot area when shooting.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, more particularly, to a kind of unmanned plane undercarriage and unmanned plane.
Background technology
Undercarriage is exactly that aircraft is parked on ground, slided, takeoff and anding is slided and is used to support aircraft gravity when running, and is born corresponding
The device of load.Any artificial aircraft has a process to lift off, and except disposable rocket-powered missile and
Outside the spacecraft that need not be reclaimed, most aircraft suffer from land or recovery stage.For aircraft, aircraft is realized
Taking-off and landing process, main is exactly to utilize undercarriage.
And for unmanned plane, rising and falling for unmanned plane is typically aided in using T-shaped undercarriage in the prior art.But
It is that T-shaped unmanned plane undercarriage can have the shortcomings that blocking unmanned plane shooting composition during flight.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane undercarriage and unmanned plane, to solve to deposit in the prior art
T-shaped unmanned plane undercarriage blocked during unmanned plane during flying unmanned plane shooting composition technical problem.
A kind of unmanned plane undercarriage provided by the utility model, including at least one telescopic component and at least one fixation
Component；
The telescopic component includes motor and at least expansion link of two-stage；The expansion link by the driving of the motor and
Axial stretching；
The telescopic component is connected with the fixation kit, for being fixed by the fixation kit with unmanned plane.
In the above-mentioned technical solutions, the undercarriage of unmanned plane is regarded using expansion link, instead of T-shaped nothing of the prior art
Man-machine undercarriage, the shielded area of undercarriage can be reduced, making unmanned plane, camera can capture more when shooting
Area can be shot.
Further, in embodiment of the present utility model, in addition to controller；
The controller electrically connects with the motor, for controlling stretching for telescopic component according to the flight progress of unmanned plane
Contracting.
In the above-mentioned technical solutions, the controller can automatically control the flexible situation of expansion link, root by motor
Realize that unmanned plane freely rises and falls according to default program, automaticity is higher.
Further, in embodiment of the present utility model, in addition to speed regulator；
The speed regulator electrically connects with the controller and the motor, for being adjusted according to the control command of the controller
The rotating speed of whole motor.
In the above-mentioned technical solutions, the speed regulator realizes the speed governing of motor, to adapt to the current state of rising and falling of unmanned plane
Or height of rising and falling, so as to more smoothly realize the takeoff and landing process of unmanned plane.
Further, in embodiment of the present utility model, in addition to remote control；
The remote control is connected with the motor wireless telecommunications, controls the telescopic component to stretch for being sent to the motor
The control command of contracting.
In the above-mentioned technical solutions, by remote control input order, can taking human as control expansion link telescopic process, this
Kind of mode can be such that user is made according to the flight progress of reality targetedly to judge, have more the takeoff and landing of unmanned plane
Reasonability and freedom.
Further, in embodiment of the present utility model, the fixation kit includes fixed seat and is detachably arranged at
The support arm of the fixed seat side wall；
The support arm is used to be connected with the telescopic component.
In the above-mentioned technical solutions, after the fixed seat is fixed on unmanned plane, by support arm can set one or
Multiple telescopic components, and when be connected with unmanned plane, it is only necessary to the fixed fixed seat, make dismounting and assembling more square
Just.
Further, in embodiment of the present utility model, the fixation kit includes being used for the card for being plugged on unmanned plane
Fixed block in groove；
The expansion link is connected with the fixed block, and by the clamping of the fixed block and the neck and then with nobody
Machine connects.
Further, in embodiment of the present utility model, the expansion link includes Pyatyi expansion link.
Further, in embodiment of the present utility model, the final stage expansion link of the telescopic component is made using rubber.
In the above-mentioned technical solutions, the final stage expansion link employs rubber making, when the unmanned plane is landed, is stretching
The impulsive force to unmanned plane applied when contracting bar touches ground to ground forms buffering effect.
Further, in embodiment of the present utility model, it is provided between the fixation kit and the telescopic component
Beam.
In the above-mentioned technical solutions, when there is provided the beam unmanned plane can be made to land, touch ground in expansion link
The impulsive force to unmanned plane applied when face to ground forms buffering effect.
Present invention also provides a kind of unmanned plane, including described unmanned plane undercarriage.
Brief description of the drawings
, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
The required accompanying drawing used is briefly described in embodiment or description of the prior art, it should be apparent that, describe below
In accompanying drawing be some embodiments of the present utility model, for those of ordinary skill in the art, do not paying creativeness
On the premise of work, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is that the structure of the unmanned plane undercarriage for the expansion link with two-stage that the utility model one embodiment provides is shown
It is intended to；
Fig. 2 is that the structure of the unmanned plane undercarriage for the expansion link with Pyatyi that the utility model one embodiment provides is shown
It is intended to；
Fig. 3 is the exploded perspective view for the unmanned plane undercarriage that the utility model one embodiment provides；
Fig. 4 is that the assembling of the unmanned plane undercarriage for the expansion link with two-stage that the utility model one embodiment provides is shown
It is intended to；
Fig. 5 is that the assembling of the unmanned plane undercarriage for the expansion link with Pyatyi that the utility model one embodiment provides is shown
It is intended to；
Fig. 6 is the fixed block and neck grafting cooperation schematic diagram that the utility model one embodiment provides；
Fig. 7 is the fixed block and neck exploded perspective view that the utility model one embodiment provides；
Fig. 8 is the structural representation of the fixed seat that the utility model one embodiment provides and support arm；
Fig. 9 is the schematic diagram of circuit connection structure of the controller that the utility model one embodiment provides and speed regulator；
Figure 10 is the wireless connection schematic diagram for the remote control that the utility model one embodiment provides.
Reference：
1- telescopic components；2- fixation kits；3- unmanned planes；
4- controllers；5- speed regulators；6- remote controls；
11- motors；12- expansion links；13- final stage expansion links；
21- fixed seats；22- support arms；23- fixed blocks；24- necks.
Embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described
Embodiment is the utility model part of the embodiment, rather than whole embodiments.Based on the embodiment in the utility model, sheet
The every other embodiment that field those of ordinary skill is obtained under the premise of creative work is not made, belongs to this practicality
Novel protected scope.
, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation of the instruction such as " level ", " interior ", " outer " or position relationship are based on orientation shown in the drawings or position relationship, are only
Described for the ease of description the utility model and simplifying, rather than instruction or imply signified device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " the
One ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that instruction or hint relative importance.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
Concrete meaning of the language in the utility model.
Fig. 1 is the knot of the undercarriage of unmanned plane 3 for the expansion link 12 with two-stage that the utility model one embodiment provides
Structure schematic diagram；
Fig. 3 is the exploded perspective view for the undercarriage of unmanned plane 3 that the utility model one embodiment provides；
Fig. 4 is the dress of the undercarriage of unmanned plane 3 for the expansion link 12 with two-stage that the utility model one embodiment provides
With schematic diagram.
As shown in Figure 1 and Figure 4, a kind of undercarriage of unmanned plane 3 provided by the utility model that the present embodiment provides, including extremely
Few a telescopic component 1 and at least one fixation kit 2；The shown telescopic component 1 and the fixation kit in Fig. 1
2 connections, the telescopic component 1 are fixed by the fixation kit 2 with unmanned plane 3, are arranged on bottom or the side wall of unmanned plane 3
Deng position, to play the action that auxiliary unmanned plane 3 rises and falls, its effect as undercarriage is realized.
Wherein, the telescopic component 1 includes motor 11 and at least expansion link 12 of two-stage；The expansion link 12 is by described
The driving of motor 11 and axial stretching；With reference to shown in Fig. 1 and Fig. 3, show respectively with two-stage stretch expansion link 12 and
The expansion link 12 to be stretched with Pyatyi.Certainly, can also be according to the weight, model, knot of unmanned plane 3 among specific manufacture
The particular situations such as structure set the expansion link 12 of different series, realize what telescopic component 1 was risen and fallen with stretching to aid in unmanned plane 3
Purpose.
Here, the function of telescopic component 1 is situated between by the expansion link 12 with two-stage described in Fig. 1 first
Continue.
When unmanned plane 3 will land, the motor 11 can drive the gear mechanism in the expansion link 12, by motor 11
Be changed into the action that every grade of expansion link 12 can be driven to stretch along its length, and then make expansion link 12 described in two-stage relative
Elongation, realize the telescopic effect of expansion link 12.Specifically refer to the operation principle of electric expansion bar 12.
The distance on when landing with unmanned plane 3 and ground reduces, and the expansion link 12 also realizes the effect of elongation, for propping up
Support the unmanned plane 3 and be still in ground.
When unmanned plane 3 will take off, it is (relative that the motor 11 can drive the gear mechanism in the expansion link 12 to invert
For above-described embodiment), and then make every grade of the relative constriction of expansion link 12, make unmanned plane 3 when flight, it is described nobody
The undercarriage of machine 3 can obtain a less volume, in the hope of reducing the influence degree that the visual field can be shot to camera.
It is described above it is specifically used during embodiment, a kind of also only use of the undercarriage of unmanned plane 3
Form.
The technical scheme of the undercarriage of unmanned plane 3 is understood by above-described embodiment, is worked as using expansion link 12
The undercarriage of unmanned plane 3 is done, instead of the T-shaped undercarriage of unmanned plane 3 of the prior art, the screening of the undercarriage of unmanned plane 3 can be reduced
Block face accumulates, and making unmanned plane 3, camera, which can capture, can more shoot area when shooting.
Fig. 2 is the knot of the undercarriage of unmanned plane 3 for the expansion link 12 with Pyatyi that the utility model one embodiment provides
Structure schematic diagram；
Fig. 5 is the dress of the undercarriage of unmanned plane 3 for the expansion link 12 with Pyatyi that the utility model one embodiment provides
With schematic diagram；
As shown in Figure 2 and Figure 5, it is preferred that the expansion link 12 includes Pyatyi expansion link 12.
When unmanned plane 3 lands, as unmanned plane 3 is more and more nearer apart from ground, the expansion link 12 can be with
The close of distance gradually extends expansion link 12, to adapt to the landing of unmanned plane 3.And expansion link 12 is this with unmanned plane 3
Subaerial distance and progressive lengthening of smart, and gradually increase and determine with the flexible series of expansion link 12,
But if this flexible series sets too many, although higher smart can be obtained, whole unmanned plane 3 can be influenceed
The volume size of undercarriage after shrinking.
So flexible group as the undercarriage of unmanned plane 3 of the expansion link 12 of the preferred dilatability that Pyatyi is set of the application
The basic structure of part 1.
Fig. 9 is the schematic diagram of circuit connection structure of the controller 4 that the utility model one embodiment provides and speed regulator 5.
Further, as shown in figure 9, also including controller 4；Wherein, the controller 4 electrically connects with the motor 11,
User can the pre-designed controllable undercarriage of unmanned plane 3 program, and targetedly fitted with the state of flight of unmanned plane 3
Match somebody with somebody, enable the takeoff and landing process of the good assistance unmanned plane 3 of the undercarriage of unmanned plane 3, so the can of the controller 4
The flexible of telescopic component 1 is controlled according to the flight progress of unmanned plane 3, realizes the purpose of support unmanned plane 3.According to default journey
Sequence realizes that unmanned plane 3 freely rises and falls, and its automaticity is higher.
Specifically, the flight progress of unmanned plane 3 described above should comprise at least landing and the unmanned plane 3 of unmanned plane 3
Take off, and be not limited to the takeoff and landing state of unmanned plane 3.
For example, unmanned plane 3 during flight, runs into obstacle, or avoids blocking situations such as camera shoots the visual field,
Should belong to the undercarriage of unmanned plane 3 can foundation flight progress, and then make the structure change of adaptability.
In a specific embodiment, the landing state of unmanned plane 3 is directed to, when unmanned plane 3 lands, control
After device 4 has known the current flight state of unmanned plane 3, the telescopic component 1 can be controlled to extend, and the elongation speed for passing through adaptation
To be adapted to the descent altitude of unmanned plane 3, when unmanned plane 3 will contact ground, expansion link 12 can extend, and followed by unmanned plane 3
Gradual expansion link 12 is elongated to larger or maximum degree when dropping to ground, for adaptation to the ground and to support unmanned plane
3。
Further, with continued reference to Fig. 9, in addition to speed regulator 5；Wherein, the speed regulator 5 and the controller 4 and institute
State motor 11 to electrically connect, user can adjust the rotating speed of motor 11 according to the control command of the controller 4, pass through speed regulator 5
Come after the rotating speed of controlled motor 11 to adapt to the elongation speed of the part of expansion link 12 in the undercarriage of unmanned plane 3.
For example, when the situation exception that unmanned plane 3 lands, such as decrease speed is too fast, and motor 11 is normally to set
Constant speed degree can not timely extend expansion link 12, so, such case unmanned plane 3 may not obtain unmanned plane when reaching ground
The support of 3 undercarriages.
But after carrying out speed governing to motor 11 by speed regulator 5, can be targetedly to make change to the rotating speed of motor 11
Change, unmanned plane 3 still can be enough obtained the stretching speed of expansion link 12 in the undercarriage of unmanned plane 3 during falling extremely
Matching, when the unmanned plane 3 is fallen earthward under, the expansion link 12 can extend out, to support unmanned plane 3.
For the above situation, the speed regulator 5 can match with height sensor, to obtain the decrease speed of unmanned plane 3
Abnormal conditions, and feed back to the reaction that speed regulator 5 makes adaptation.
So the speed regulator 5 realizes the speed governing of motor 11, to adapt to unmanned plane 3 current rise and fall state or a drop height
Degree, so as to more smoothly realize the takeoff and landing process of unmanned plane 3.
Figure 10 is the wireless connection schematic diagram for the remote control 6 that the utility model one embodiment provides.
In addition to remote control 6 further, as shown in Figure 10,；The remote control 6 is used for holding to user, the remote control 6
It is connected with the wireless telecommunications of motor 11, user can send control command by remote control 6 to the motor 11, pass through hair
The control command seen off controls the telescopic component 1 flexible.
The mode of remote control can taking human as control expansion link 12 telescopic process, so, user can according to reality feelings
Condition targetedly controls the work of the lifting lever of unmanned plane 3, this artificial distant for the working forms for the automated procedures that compare
The mode of control is more flexible, the takeoff and landing of unmanned plane 3 is had more reasonability.
Fig. 8 is the structural representation of the fixed seat 21 that the utility model one embodiment provides and support arm 22.
Further, four even other numbers may be provided with structure as shown in Figure 5, on a unmanned plane 3
The undercarriage of unmanned plane 3, unmanned plane 3 is supported in the form of overall co-ordination.
For the above situation, the fixation kit 2 can include fixed seat 21 as shown in Figure 8 and be detachably arranged at institute
State the support arm 22 of the side wall of fixed seat 21；When in use, the fixed seat 21 is arranged on unmanned plane 3, is then attached to institute
State and a undercarriage of unmanned plane 3 can be set on other four support arms 22 in fixed seat 21, by multiple undercarriages of unmanned plane 3
Be formed as the supporting construction of an entirety.
After the fixed seat 21 is fixed on unmanned plane 3, it is only necessary to the fixed fixed seat 21, make dismounting and dress
With more convenient.
Fig. 6 is the fixed block 23 and the grafting cooperation schematic diagram of neck 24 that the utility model one embodiment provides；
Fig. 7 is the fixed block 23 and the exploded perspective view of neck 24 that the utility model one embodiment provides.
Further, as shown in Figure 6 and Figure 7, the fixation kit 2 includes being used to be plugged in the neck 24 of unmanned plane 3
Fixed block 23；After the appropriate location on unmanned plane 3 is provided with neck 24, it is only necessary to by the fixation on the undercarriage of unmanned plane 3
Block 23 is plugged in the neck 24；The expansion link 12 is connected with the fixed block 23, the fixed block 23 with it is described
The clamping of neck 24 can be to be easily and effectively connected with unmanned plane 3.
Further, in embodiment of the present utility model, the final stage expansion link 13 of the telescopic component 1 uses rubber system
Make.Herein it is to be appreciated that the final stage expansion link 13 is also one of expansion link 12 in the telescopic component 1, only not
Cross the expression of final stage expansion link 13 is that expansion link 12 in the most termination of telescopic component 1.
Illustrate, when in the descent of unmanned plane 3, when multistage expansion link 12 carries out elongation action, the final stage is stretched
Contracting bar 13 can contact with ground first, and this grade of expansion link 12 is represented as final stage expansion link 13, and multistage expansion link 12
In one of them.Its label in Fig. 1 represents to clash with the expression of expansion link 12.
In the above-mentioned technical solutions, the final stage expansion link 13 employs rubber making, when can make the landing of unmanned plane 3,
The impulsive force to unmanned plane 3 applied when expansion link 12 touches ground to ground forms buffering effect.
Further, in embodiment of the present utility model, set between the fixation kit 2 and the telescopic component 1
There is beam.
In the above-mentioned technical solutions, when can make the landing of unmanned plane 3 there is provided the beam, touched in expansion link 12
The impulsive force to unmanned plane 3 applied when ground to ground forms buffering effect.
Present invention also provides a kind of unmanned plane 3, including the described undercarriage of unmanned plane 3.
Because concrete structure, the principle of work and power and the technique effect of the undercarriage of unmanned plane 3 are in detailed hereinbefore,
This is just repeated no more.
Finally it should be noted that：Various embodiments above is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, either to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type.
Claims (10)
1. a kind of unmanned plane undercarriage, it is characterised in that including at least one telescopic component (1) and at least one fixation kit
(2)；
The telescopic component (1) includes motor (11) and at least expansion link (12) of two-stage；The expansion link (12) is by described
The driving of motor (11) and axial stretching；
The telescopic component (1) is connected with the fixation kit (2), for solid by the fixation kit (2) and unmanned plane (3)
It is fixed.
2. unmanned plane undercarriage according to claim 1, it is characterised in that also including controller (4)；
The controller (4) electrically connects with the motor (11), for controlling telescopic component according to the flight progress of unmanned plane (3)
(1) flexible.
3. unmanned plane undercarriage according to claim 2, it is characterised in that also including speed regulator (5)；
The speed regulator (5) electrically connects with the controller (4) and the motor (11), for according to the controller (4)
Control command adjusts the rotating speed of the motor (11).
4. unmanned plane undercarriage according to claim 1, it is characterised in that also including remote control (6)；
The remote control (6) is connected with the motor (11) wireless telecommunications, is stretched for being sent to the motor (11) described in control
The flexible control command of contracting component (1).
5. the unmanned plane undercarriage according to any one of claim 1-4, it is characterised in that fixation kit (2) bag
Include fixed seat (21) and be detachably arranged at the support arm (22) of the fixed seat (21) side wall；
The support arm (22) is used to be connected with the telescopic component (1).
6. the unmanned plane undercarriage according to any one of claim 1-4, it is characterised in that fixation kit (2) bag
Include the fixed block (23) for being plugged in the neck (24) of unmanned plane (3)；
The expansion link (12) is connected with the fixed block (23), and passes through the fixed block (23) and the card of the neck (24)
Tap into and be connected with unmanned plane (3).
7. the unmanned plane undercarriage according to any one of claim 1-4, it is characterised in that the expansion link (12) includes
Pyatyi expansion link.
8. the unmanned plane undercarriage according to any one of claim 1-4, it is characterised in that the telescopic component (1)
Final stage expansion link (13) is made using rubber.
9. the unmanned plane undercarriage according to any one of claim 1-4, it is characterised in that the fixation kit (2) with
Beam is provided between the telescopic component (1).
10. a kind of unmanned plane, it is characterised in that including unmanned plane undercarriage as claimed in any one of claims 1-9 wherein.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720512168.XU CN206885335U (en) | 2017-05-09 | 2017-05-09 | A kind of unmanned plane undercarriage and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720512168.XU CN206885335U (en) | 2017-05-09 | 2017-05-09 | A kind of unmanned plane undercarriage and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206885335U true CN206885335U (en) | 2018-01-16 |
Family
ID=61341232
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720512168.XU Active CN206885335U (en) | 2017-05-09 | 2017-05-09 | A kind of unmanned plane undercarriage and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206885335U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106945824A (en) * | 2017-05-09 | 2017-07-14 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane undercarriage and method of rising and falling |
| WO2020063631A1 (en) * | 2018-09-28 | 2020-04-02 | 杭州零零科技有限公司 | Handheld remote control device and flight system kit |
-
2017
- 2017-05-09 CN CN201720512168.XU patent/CN206885335U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106945824A (en) * | 2017-05-09 | 2017-07-14 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane undercarriage and method of rising and falling |
| WO2020063631A1 (en) * | 2018-09-28 | 2020-04-02 | 杭州零零科技有限公司 | Handheld remote control device and flight system kit |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106945824A (en) | A kind of unmanned plane undercarriage and method of rising and falling | |
| WO2017016096A1 (en) | Novel vertical take-off and landing aircraft and control method therefor | |
| CN203318676U (en) | Coaxial double-wing aircraft with moving centre-of-gravity ball | |
| CN107128479A (en) | Unmanned plane undercarriage and its control system | |
| CN206885335U (en) | A kind of unmanned plane undercarriage and unmanned plane | |
| CN108706099B (en) | Tilting triaxial composite wing unmanned aerial vehicle and control method thereof | |
| CN103101621B (en) | Parafoil aircraft applicable to cylindrical space loading | |
| CN110182352B (en) | Air-floating unpowered long-endurance aircraft and control method thereof | |
| CN106043686A (en) | Vertical take-off and landing fixed wing aircraft | |
| CN110614891A (en) | Method for cross-dimension movement of flying robot | |
| CN106802659A (en) | The control method of feather multi-rotor aerocraft | |
| CN112357047A (en) | Unmanned aerial vehicle with telescopic arm variable rotor wing | |
| CN106477043A (en) | A kind of bionical Apiss | |
| CN107458593B (en) | Duct propulsion system based on multi-rotor unmanned aerial vehicle | |
| CN104503426A (en) | Parafoil control law test commissioning platform and commissioning method | |
| CN205613032U (en) | Wearable model airplane wireless remote control system | |
| CN203264283U (en) | Inertial posture balancer for model airplane | |
| CN105749563A (en) | Wearable model airplane wireless remote control system | |
| CN111516850B (en) | Control method for flight attitude and buoyancy of airship | |
| CN205730366U (en) | A kind of wing horizontal tail full dynamic formula aircraft model plane | |
| CN207773463U (en) | Power source system applied to unmanned plane | |
| CN105539815A (en) | Posture-adjusting balance-weight control system of water-air-amphibious unmanned aerial vehicle | |
| CN105314107A (en) | Method of achieving vertical take-off and landing of existing unmanned airplane | |
| CN205750340U (en) | A kind of six rotorcraft control circuit thrown in for disaster relief supplies | |
| CN104240552A (en) | Rotary wing type carrier operating system and operating method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230629 Address after: 215300 room 4, No. 388, Zhengwei East Road, Jinxi Town, Kunshan City, Suzhou City, Jiangsu Province Patentee after: Kunshan Helang Aviation Technology Co.,Ltd. Address before: 215300 Zhengwei Road, Jinxi Town, Kunshan City, Suzhou City, Jiangsu Province, 388 Patentee before: HAOXIANG ELECTRIC ENERGY (KUNSHAN) Co.,Ltd. |
|
| TR01 | Transfer of patent right |