CN209493248U - A kind of unmanned plane electric winch - Google Patents
A kind of unmanned plane electric winch Download PDFInfo
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- CN209493248U CN209493248U CN201822217389.1U CN201822217389U CN209493248U CN 209493248 U CN209493248 U CN 209493248U CN 201822217389 U CN201822217389 U CN 201822217389U CN 209493248 U CN209493248 U CN 209493248U
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- hook
- rack
- unmanned plane
- electric winch
- locking
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Abstract
Unmanned plane electric winch disclosed in the present application, compared with prior art, comprising: rack；The power capstan being set in rack；It is set in rack, the driving motor for driving power capstan to rotate；The hooking device being set in rack, hooking device have the locking state for loosening state and hook reset of opening of hook.Unmanned plane electric winch provided by the present application, suitable for unmanned machine operation, hooking device can carry out rapid-releasing, abandon weight to save aircraft, compared to existing technologies, security reliability is higher at the necessary moment in unmanned plane operation process.
Description
Technical field
This application involves air vehicle technique fields, more specifically more particularly to a kind of unmanned plane electric winch.
Background technique
Currently, unmanned plane needs a kind of miniaturization, the big winch of lifting force when implementing to hang operation.It is existing electronic
Winch is all industrial use, and not only volume is big, and weight is also big, for example, electric industrial cucurbit: being driven using 220V ac motor
It is dynamic, drive capstan winch to hang weight by retarder.Main screw lift is in 20kg or so；Electirc capstan for vehicles is straight using 12V high current
Motor driven is flowed, winching operations are driven by retarder, complete machine lifting force is big, but weight is also greater than 15kg.Therefore, existing skill
The electric winch of industrial use can be suitable for unmanned plane well in art.
Therefore, how a kind of unmanned plane electric winch is provided, unmanned plane can be preferably suitable for, and is linked up with reliable
Safety, when necessary, can abandon weight with rapid-releasing to save aircraft, have become those skilled in the art and urgently solve
Certainly the technical issues of.
Utility model content
In order to solve the above technical problems, the application provides a kind of unmanned plane electric winch, can preferably be suitable for
Unmanned plane, and hook is reliable and secure, when necessary, can abandon weight with rapid-releasing to save aircraft.
Technical solution provided by the present application is as follows:
The application provides a kind of unmanned plane electric winch, comprising: rack；The power capstan being set in rack；Setting
In the driving motor in rack, for driving power capstan to rotate；The hooking device being set in rack, hooking device, which has, to be hung
What hook was opened loosens the locking state of state and hook reset.
Further, in a kind of preferred mode of the utility model, hooking device includes: the fixation being set in rack
Hook；The first articulated shaft being installed on fixed hook；The Removable hook being articulated on the first articulated shaft；For controlling movable extension
The hook controller that hook is rotated along articulated shaft.
Further, in a kind of preferred mode of the utility model, hook controller includes: to be articulated with fixed hook
On locking hook；Rolling bearing on Removable hook；In rack, for controlling locking hook contact or far from the axis of rolling
The power drive mechanism held.
Further, in a kind of preferred mode of the utility model, power drive mechanism includes: to be installed in rack
Steering engine；It is connect with steering engine, by the shackle rod of servo driving, shackle rod is hinged with locking hook.
Further, in a kind of preferred mode of the utility model, locking hook is equipped with from lock crossbeam；From lock crossbeam
It is equipped with: the first confined planes that can be contacted with the rolling bearing upper half, and the second limit that can be contacted with rolling bearing lower half
Face.
Further, in a kind of preferred mode of the utility model, hooking device includes: the fixation being set in rack
Hook；The first articulated shaft being installed on fixed hook；The Removable hook being articulated on the first articulated shaft；On fixed hook
The second articulated shaft；The locking hook being articulated on the second articulated shaft；Rolling bearing on Removable hook；Locking hook have with
The second state that the first state and rolling bearing that rolling bearing is in contact are detached from；The steering engine being installed in rack；Connect with steering engine
It connects, by the shackle rod of servo driving, shackle rod is hinged with locking hook, for driving locking hook to rotate around the second articulated shaft.
Further, in a kind of preferred mode of the utility model, locking hook is equipped with from lock crossbeam；From lock crossbeam
It is equipped with: the first confined planes that can be contacted with the rolling bearing upper half, and the second limit that can be contacted with rolling bearing lower half
Face.
Further, in a kind of preferred mode of the utility model, power capstan is specifically set to frame lower.
Further, in a kind of preferred mode of the utility model, fixed hook includes: the extension for being installed on upper rack
Hook mounting portion；The hanger bulk being connected with hook mounting portion；It is connected with hook mounting portion, and the auxiliary far from hanger bulk side
Mounting portion；Mounting portion, hanger bulk and auxiliary mounting portion is linked up with to be integrally formed.
Further, in a kind of preferred mode of the utility model, locking hook includes: the hook being articulated on fixed hook
Main body；Limiting section with the first confined planes and the second confined planes；The hinged hinge position with shackle rod；Hook main body, limiting section
And hinge position is integrally formed.
A kind of unmanned plane electric winch provided by the utility model, compared with prior art, comprising: rack, in rack
It is provided with power capstan, and the driving motor for driving the power capstan rotation, in addition, being additionally provided with extension in rack
Hook device, hooking device have the locking state for loosening state and hook reset of opening of hook.In this way, unmanned machine operation exists
When necessary, hooking device can abandon weight with rapid-releasing to save aircraft.Compared to existing technologies, safely may be used
It is higher by property.
Detailed description of the invention
In order to illustrate the technical solutions in the embodiments of the present application or in the prior art more clearly, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of application for those of ordinary skill in the art without creative efforts, can be with
It obtains other drawings based on these drawings.
Fig. 1 is the main view of unmanned plane electric winch provided by the embodiment of the utility model；
Fig. 2 is the partial enlarged view of hooking device part in Fig. 1；
Fig. 3 is the schematic perspective view of unmanned plane electric winch provided by the embodiment of the utility model；
Fig. 4 is the stereochemical structure signal at another visual angle of unmanned plane electric winch provided by the embodiment of the utility model
Figure.
Specific embodiment
In order to make those skilled in the art more fully understand the technical solution in the application, below in conjunction with the application reality
The technical scheme in the embodiment of the application is clearly and completely described for the attached drawing for applying in example, it is clear that described embodiment
Only a part of the embodiment of the application, instead of all the embodiments.Based on the embodiment in the application, this field is common
Technical staff's every other embodiment obtained without making creative work belongs to the model of the application protection
It encloses.
It should be noted that it can directly exist when element is referred to as on " being fixed on " or " being set to " another element
On another element or indirectly setting on the other element；When an element is known as " being connected to " another element,
It can be directly to another element or be indirectly connected on another element.
It is to be appreciated that term " length ", " width ", "upper", under ", "front", "rear", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "top", "bottom" "inner", "outside" is that orientation based on the figure or position are closed
System is merely for convenience of description the application and simplifies description, rather than the device or element of indication or suggestion meaning must have
Specific orientation is constructed and operated in a specific orientation, therefore should not be understood as the limitation to the application.
In addition, term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance
Or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include one or more of the features.It is multiple in the description of the present application ", " several " be meant that two or
Two or more, unless otherwise specifically defined.
It should be clear that structure depicted in this specification attached drawing, ratio, size etc., only to cooperate specification revealed
Content is not limited to the enforceable qualifications of the application, therefore does not have so that those skilled in the art understands and reads
Technical essential meaning, the modification of any structure, the change of proportionate relationship or the adjustment of size are not influencing the application institute energy
Under the effect of generation and the purpose that can reach, it should all still fall in techniques disclosed in this application content and obtain the range that can cover
It is interior.
Please be as shown in Figures 1 to 4, unmanned plane electric winch provided by the embodiments of the present application, comprising: rack 1；It is set to
Power capstan 2 in rack 1；It is set in rack 1, the driving motor 3 for driving power capstan 2 to rotate；It is set to rack 1
On hooking device 4, hooking device 4 have opening of hook loosen state and hook reset locking state.
The utility model embodiment provides a kind of unmanned plane electric winch, compared with prior art, comprising: rack 1, machine
Power capstan 2, and the driving motor 3 for driving power capstan 2 to rotate are provided on frame 1, in addition, also setting in rack 1
It is equipped with hooking device 4, hooking device 4 has the locking state for loosening state and hook reset of opening of hook.In this way, nobody
When necessary, hooking device 4 can abandon weight with rapid-releasing to save aircraft to machine operation.Compared to the prior art and
Speech, security reliability are higher.
Specifically, in the utility model embodiment, hooking device 4 includes: the fixed hook 41 being set in rack 1；
The first articulated shaft 43 being installed on fixed hook 41；The Removable hook 42 being articulated on the first articulated shaft 43；For controlling work
Hook controller 44 of the dynamic hook 42 along articulated shaft rotation.
Specifically, in the utility model embodiment, hook controller 44 includes: the lock being articulated on fixed hook 41
Only hook 46；Rolling bearing 47 on Removable hook 42；In rack 1, for controlling the contact of locking hook 46 or far from rolling
The power drive mechanism 48 of dynamic bearing 47.
Specifically, in the utility model embodiment, power drive mechanism 48 includes: the steering engine being installed in rack 1
481；It is connect with steering engine 481, the shackle rod 482 driven by steering engine 481, shackle rod 482 and locking hook 46 are hinged.
Wherein, in unmanned plane operation process, when hooking device 4 is in the locking state that hook resets, 4 hook of hooking device
It is located in the hanging parts of unmanned plane, electric winch runs with unmanned plane and carries out operation, when hooking device 4 is in opening of hook
When loosening state, electric winch is detached from the hanging parts on unmanned plane；Specifically, when hooking device 4 is in the lock that hook resets
When tight state, locking hook 46 resists rolling bearing 47, to maintain the relative position of fixed hook 41 Yu Removable hook 42, keeps
Fixed hook 41 and the common hook of Removable hook 42 are located in the hanging parts of unmanned plane, when hooking device 4 is in opening of hook
When loosening state, steering engine 481 drives shackle rod 482 to move, and shackle rod 482 pulls locking hook 46 around locking hook 46 and fixes
The hinge joint of hook 41 is rotated, and locking hook 46 is far from rolling bearing 47, and rolling bearing 47 is no longer by the constraint of locking hook 46
Power effect, Removable hook 42 are rotated around the hinge joint of itself and fixed hook 41 under external force, and Removable hook 42 is far from fixed
Hook 41, when fixed hook 41 and Removable hook 42, opening of hook, hooking device 4 is in and loosens state, twists so as to cause entire
Disc system fast-falling.
Specifically, in the utility model embodiment, locking hook 46 is equipped with from lock crossbeam 461；It is set from lock crossbeam 461
Have: the first confined planes that can be contacted with 47 upper half of rolling bearing, and the second limit that can be contacted with 47 lower half of rolling bearing
Plane.
Specifically, in the utility model embodiment, hooking device 4 includes: the fixed hook 41 being set in rack 1；
The first articulated shaft 43 being installed on fixed hook 41；The Removable hook 42 being articulated on the first articulated shaft；Set on fixed hook
The second articulated shaft 45 on 41；The locking hook 46 being articulated on the second articulated shaft 45；Rolling bearing on Removable hook 42
47；The second state that locking hook 46 has the first state being in contact with rolling bearing 47, is detached from rolling bearing 47；It is installed on
Steering engine 481 in rack 1；It is connect with steering engine 481, the shackle rod 482 driven by steering engine 481, shackle rod 482 and locking hook
46 is hinged, for driving locking hook 46 to rotate around the second articulated shaft 45.More specifically, fixed hook 41 includes: set on rack 1
On first hook branch 411 and second hook branch 412, Removable hook 42 be located at first hook branch 411 and second hook
Between branch 412.
Specifically, in the utility model embodiment, locking hook 46 is equipped with from lock crossbeam 461；From lock crossbeam, 461 are set
Have: the first confined planes that can be contacted with 47 upper half of rolling bearing, and the second limit that can be contacted with 47 lower half of rolling bearing
Plane.
Specifically, in the utility model embodiment, power capstan 2 is specifically set to 1 lower part of rack.
Specifically, in the utility model embodiment, fixed hook 41 includes: the hook installation for being installed on 1 top of rack
Portion；The hanger bulk being connected with hook mounting portion；It is connected with hook mounting portion, and the auxiliary far from hanger bulk side is installed
Portion；Mounting portion, hanger bulk and auxiliary mounting portion is linked up with to be integrally formed.
Specifically, in the utility model embodiment, locking hook 46 includes: the hook main body being articulated on fixed hook 41；
Limiting section with the first confined planes and the second confined planes；The hinged hinge position with shackle rod 482；Hook main body, limiting section with
And hinge position is integrally formed.
It illustrates in more detail, unmanned plane electric winch includes: rack 1；The power capstan 2 being installed in rack 1；Peace
Loaded on the low-voltage direct drive motor in rack 1, low-voltage direct drive motor is connected with capstan winch, for driving capstan winch to revolve
Turn.Wherein, fixed hook 41 is fixed in rack 1, and Removable hook 42 is hinged on fixed hook 41 by hinged shaft, and can be around hinge
Axis rotation.Rolling bearing 47 is installed, locking hook is hinged on fixed hook 41 by secondary hinged shaft, and living on Removable hook 42
Groove on dynamic hook 42 is withstood on rolling bearing 47.Steering engine 481 is mounted in rack 1, and can be with by shackle rod 482
Locking hook 46 is pulled, can be opened so as to cause Removable hook 42, so as to cause entire capstan system fast-falling.Locking hook 46
On rolling bearing 47 can be pushed away inward when Removable hook 42 disengages outward from lock crossbeam, lead to activity by special designing
Hook 42 has the tendency that slightly locking, and so as to effectively prevent entire hook system voluntarily to loosen under gravity, and is having
It in the case where carry weight, the more can draw the more tight.
More specifically, in the present embodiment, unmanned plane is driven with electric winch using low-voltage power, and driving voltage is preferred
For 12V, and unmanned plane involved in the present embodiment is miniaturization, electric winch small in size, integrated level is high with electric winch, is fitted
For unmanned plane, and anti-reverse driving can be twisted, carry self-locking function, hooking device is reliable, and it is highly-safe, in unmanned machine operation
When necessary, weight can be abandoned to save aircraft with rapid-releasing.
The foregoing description of the disclosed embodiments can be realized professional and technical personnel in the field or using originally practical new
Type.Various modifications to these embodiments will be readily apparent to those skilled in the art, and determine herein
The General Principle of justice can be realized in other embodiments without departing from the spirit or scope of the present utility model.Cause
This, the present invention will not be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The widest scope consistent with features of novelty.
Claims (10)
1. a kind of unmanned plane electric winch characterized by comprising
Rack；
The power capstan being set in the rack；
It is set in the rack, for driving the driving motor of the power capstan rotation；
The hooking device being set in the rack, the hooking device loosen state and hook reset with opening of hook
Locking state.
2. unmanned plane electric winch according to claim 1, which is characterized in that the hooking device includes: to be set to
Fixed hook in the rack；The first articulated shaft being installed on the fixed hook；The work being articulated on the articulated shaft
Dynamic hook；The hook controller rotated for controlling the Removable hook along the articulated shaft.
3. unmanned plane electric winch according to claim 2, which is characterized in that the hook controller includes: hinge
The locking hook being connected on the fixed hook；Rolling bearing on the Removable hook；In the rack, for controlling
Make the locking hook contact or the power drive mechanism far from the rolling bearing.
4. unmanned plane electric winch according to claim 3, which is characterized in that the power drive mechanism includes: peace
Loaded on the steering engine in the rack；It is connect with the steering engine, by the shackle rod of the servo driving, the shackle rod and institute
It is hinged to state locking hook.
5. unmanned plane electric winch according to claim 4, which is characterized in that the locking hook is equipped with self-locking recessed
Slot；It is described to be equipped with from lock crossbeam: the first confined planes that can be contacted with the rolling bearing upper half, and can be with the rolling
Second confined planes of bearing lower half contact.
6. unmanned plane electric winch according to claim 1, which is characterized in that the hooking device includes: to be set to
Fixed hook in the rack；The first articulated shaft being installed on the fixed hook；The work being articulated on the articulated shaft
Dynamic hook；The second articulated shaft on the fixed hook；The locking hook being articulated on second articulated shaft；Set on described
Rolling bearing on Removable hook；The locking hook has the first state being in contact with the rolling bearing and the rolling
The second state that bearing is detached from；The steering engine being installed in the rack；It is connect with the steering engine, by the transmission of the servo driving
Pull rod, the shackle rod and the locking hook are hinged, for driving the locking hook to rotate around second articulated shaft.
7. unmanned plane electric winch according to claim 6, which is characterized in that the locking hook is equipped with self-locking recessed
Slot；It is described to be equipped with from lock crossbeam: the first confined planes that can be contacted with the rolling bearing upper half, and can be with the rolling
Second confined planes of bearing lower half contact.
8. according to claim 1 to unmanned plane electric winch described in 7 any one, which is characterized in that the power capstan
Specifically it is set to the frame lower.
9. according to unmanned plane electric winch described in claim 2 to 7 any one, which is characterized in that the fixed hook
It include: the hook mounting portion for being installed on the upper rack；The hanger bulk being connected with the hook mounting portion；With the hook
Mounting portion is connected, and the auxiliary mounting portion far from the hanger bulk side；The hook mounting portion, the hanger bulk and
The auxiliary mounting portion is integrally formed.
10. the unmanned plane electric winch according to claim 5 or 7, which is characterized in that the locking hook includes: hinged
In the hook main body on the fixed hook；Limiting section with first confined planes and second confined planes；With the biography
The hinged hinge position of dynamic pull rod；The hook main body, the limiting section and the hinge position are integrally formed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822217389.1U CN209493248U (en) | 2018-12-27 | 2018-12-27 | A kind of unmanned plane electric winch |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822217389.1U CN209493248U (en) | 2018-12-27 | 2018-12-27 | A kind of unmanned plane electric winch |
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| Publication Number | Publication Date |
|---|---|
| CN209493248U true CN209493248U (en) | 2019-10-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822217389.1U Active CN209493248U (en) | 2018-12-27 | 2018-12-27 | A kind of unmanned plane electric winch |
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| Country | Link |
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| CN (1) | CN209493248U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109437034A (en) * | 2018-12-27 | 2019-03-08 | 湖南省库塔科技有限公司 | A kind of unmanned plane electric winch |
| CN111071946A (en) * | 2019-12-24 | 2020-04-28 | 太重（天津）滨海重型机械有限公司 | Automatic hanging and releasing device and using method thereof |
-
2018
- 2018-12-27 CN CN201822217389.1U patent/CN209493248U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109437034A (en) * | 2018-12-27 | 2019-03-08 | 湖南省库塔科技有限公司 | A kind of unmanned plane electric winch |
| CN111071946A (en) * | 2019-12-24 | 2020-04-28 | 太重（天津）滨海重型机械有限公司 | Automatic hanging and releasing device and using method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211216 Address after: 410000 room 52, door 5, building 30, No. 114, xinkaipu Road, Tianxin District, Changsha City, Hunan Province Patentee after: Li Jun Address before: 3 / F, Zhongchuang building, Sany industrial city, No.1 Sany Road, Changsha Economic and Technological Development Zone, Hunan 410000 (cluster registration) Patentee before: HUNAN KUTA TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230625 Address after: 110000 Shenyang General Aviation Industrial Base, Liaoning Province Patentee after: Faku Zhongjun Wing UAV Technology Co.,Ltd. Address before: 410000 room 52, door 5, building 30, No. 114, xinkaipu Road, Tianxin District, Changsha City, Hunan Province Patentee before: Li Jun |