CN208932717U - Unmanned electro-mechanical force payingoff mechanism - Google Patents
Unmanned electro-mechanical force payingoff mechanism Download PDFInfo
- Publication number
- CN208932717U CN208932717U CN201821711581.XU CN201821711581U CN208932717U CN 208932717 U CN208932717 U CN 208932717U CN 201821711581 U CN201821711581 U CN 201821711581U CN 208932717 U CN208932717 U CN 208932717U
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- Prior art keywords
- mechanical force
- unmanned
- heating wire
- fixed
- payingoff mechanism
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- 230000007246 mechanism Effects 0.000 title claims abstract description 25
- 238000009434 installation Methods 0.000 claims abstract description 10
- 238000010438 heat treatment Methods 0.000 claims description 34
- 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 21
- 206010037660 Pyrexia Diseases 0.000 claims description 18
- 239000004020 conductor Substances 0.000 claims description 9
- 239000007787 solid Substances 0.000 claims 1
- 238000013016 damping Methods 0.000 abstract description 7
- 230000009286 beneficial effect Effects 0.000 abstract description 3
- 238000004880 explosion Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned electro-mechanical force payingoff mechanism, comprising: the control system of bracket, line wheel, damper, steering engine, wire installation and fuse, fuse and unmanned plane connects.The utility model provides a kind of unmanned electro-mechanical force payingoff mechanism, the electric power payingoff mechanism is mounted on unmanned plane, unmanned plane is along route flying overhead and discharges draught line, the utility model has the following beneficial effects: draught line is placed on unmanned plane, overcomes unmanned plane and more leaps slow problem；This unmanned electro-mechanical force payingoff mechanism is equipped with damper, staff can adjust the size of damping according to flying speed and payingoff speed from remote controler, prevent from damping too small, payingoff speed is too fast and the problem of cause coiling, damp that excessive, payingoff speed is excessively slow and the problem that causes unmanned plane during flying unstable；This unmanned electro-mechanical force payingoff mechanism is equipped with fuse, can quickly break when draught line is wound, guarantee the safety of unmanned plane.
Description
Technical field
The utility model relates to unmanned plane field more particularly to a kind of unmanned electro-mechanical force payingoff mechanisms.
Background technique
Electric power construction of power transmission and transformation is often in severe feelings such as marsh, lake surface, farmland, highway, mountainous region, steep cliff overhead
It is carried out under condition, route payingoff construction work therein was to place the mode of draught line by manually upper Ji Ta in the past to complete, work
Make low efficiency, safety is low, is unfavorable for the life security of guarantor.Generally use now the mode of UAV flight's draught line into
Row unwrapping wire, traditional unmanned plane unwrapping wire mode is that draught line is placed on ground, is routed by unmanned plane draught line, such mode
The remoter unmanned plane load of winged distance can be caused heavier, so that payingoff speed is slower, and draught line is easy to be hung by trees
Firmly, unmanned plane is drawn motionless, is prone to accidents, is needed to cut off draught line at this time, and traditional mode is cut off using blade
Draught line, blade cutting speed is slow, and is prone to wear, and is not durable.
Therefore, the prior art is defective, needs to improve.
Utility model content
The purpose of the utility model is to overcome the deficiencies in the prior art, provide a kind of unmanned electro-mechanical force payingoff mechanism, can
Damping size is adjusted, and quickly cuts off draught line when draught line is tangled.
The technical solution of the utility model is as follows: providing a kind of unmanned electro-mechanical force payingoff mechanism, comprising: bracket is located at institute
State the line wheel in bracket, the damper for being fixed on the bracket one side, the steering engine connecting with the damper, installation admittedly
It is scheduled on the wire installation of the cradle bottom surface and is fixed on the fuse of the cradle bottom surface, the fuse and nothing
Man-machine control system connection, the fuse include: the interior heating wire pedestal equipped with a cavity, are located at the heating wire pedestal
The heating wire bracket of cavity two sides, is fastened on the tabletting and heating wire at the tabletting being fixed on the heating wire pedestal
The first fever tablet between bracket and the second fever tablet being fastened between the heating wire bracket and heating wire pedestal.
Further, the tabletting is equipped with a counterbore, and the heating wire pedestal corresponds to the counterbore equipped with threaded hole, spiral shell
Silk passes through the counterbore and lock on threaded hole, and the tabletting is fixed on heating wire pedestal.
Further, the bracket includes: that bottom plate, the both side plate being fixed on the bottom plate and installation are fixed
Upper mounted plate on the side plate, both side plate are respectively provided with first through hole.
Further, heating wire pedestal two sides are provided with the second through-hole, draught line pass through second through-hole and
Between first fever tablet and the second fever tablet.
Further, the wire installation includes: the gag lever post for being located at the plate upper surface, is located at the bottom plate following table
The conductor rod in face, the tension disk by the conductor rod and the guide roller for being fixed on the lower surface of base plate, traction
Line successively bypasses gag lever post, conductor rod, tension disk, fuse and guide roller.
Further, the line wheel includes I-beam wheel, across the shaft of the I-beam wheel, and draught line is wound on the I-beam wheel
On.
Further, the line wheel further include across the first through hole and the line wheel that is fixed on the side plate it is fixed
Position set, the both ends of the shaft are fixed on the line wheel positioning sleeve.
Further, the damper includes a turntable connecting with the steering engine and an output shaft.
Using the above scheme, the utility model provides a kind of unmanned electro-mechanical force payingoff mechanism, which is taken
It being loaded on unmanned plane, unmanned plane is along route flying overhead and discharges draught line, the utility model has the following beneficial effects:
(1) draught line is placed on unmanned plane, overcomes unmanned plane and more leaps slow problem；
(2) this unmanned electro-mechanical force payingoff mechanism is equipped with damper, staff can according to flying speed and payingoff speed from
The size that damping is adjusted on remote controler, prevent from damping too small, payingoff speed is too fast and the problem of cause coiling, damp it is excessive, put
Linear speed spends problem that is slow and causing unmanned plane during flying unstable；
(3) this unmanned electro-mechanical force payingoff mechanism is additionally provided with fuse, can quickly break when draught line is wound, and guarantees
The safety of unmanned plane.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model.
Fig. 2 is the perspective view of the explosion at one visual angle of the utility model.
Fig. 3 is the perspective view of the explosion at another visual angle of the utility model.
Fig. 4 is the perspective view of the explosion of the utility model fuse.
Specific embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.
It please refers to Fig.1 to Fig.3, the utility model provides a kind of unmanned electro-mechanical force payingoff mechanism, comprising: bracket 1 is located at institute
State the line wheel 2 in bracket 1, the damper 3 for being fixed on 1 one side of bracket, the steering engine 4 being connect with the damper 3,
It is fixed on the wire installation 5 of 1 bottom surface of bracket and is fixed on the fuse 6 of 1 bottom surface of bracket.It is described
Line wheel 2 includes I-beam wheel 21, the shaft 22 across 21 axle center of I-beam wheel, and draught line is wound in the I-beam wheel 21, I-shaped
Wheel 21 is rotated around shaft 22 to discharge draught line.The damper 3 includes that a turntable connecting with the steering engine 4 and one are defeated
Shaft, when discharging draught line, staff can manipulate remote controler with payingoff speed to control according to the flying speed of unmanned plane
The positive and negative rotation angle of steering engine 4 processed adjusts the elastic of 3 output shaft of damper by turntable, to control payingoff speed.
Please refer to Fig.1 to Fig.3, the bracket 1 include: bottom plate 11, the both side plate 12 being fixed on the bottom plate 11,
And it is fixed on the upper mounted plate 13 on the side plate 12, both side plate 12 is respectively provided with first through hole 131.The wire installation
5 include: the gag lever post 51 for being located at 11 upper surface of bottom plate, the conductor rod 52 for being located at 11 lower surface of bottom plate, set on described
The tension disk 53 on 52 side of conductor rod and the guide roller 54 for being fixed on 11 lower surface of bottom plate, draught line successively bypasses
Gag lever post 51, conductor rod 52, tension disk 53, fuse 6 and guide roller 54, draught line is tensioned and applies it swimmingly
It puts.
Fig. 3 and Fig. 4 are please referred to, the fuse 6 is connect with the control system of unmanned plane, and fuse 6 includes: interior equipped with one
The heating wire pedestal 61 of cavity, the heating wire bracket 62 for being located at the 61 cavity two sides of heating wire pedestal, be fixed on it is described
Tabletting 63 on heating wire pedestal 61, the first fever tablet 64 being fastened between the tabletting 63 and heating wire bracket 62 and
The second fever tablet 65 being fastened between the heating wire bracket 62 and heating wire pedestal 61.Fuse 6 be set to tension disk 53 with
Between guide roller 54,61 two sides of heating wire pedestal are provided with the second through-hole 611, and draught line is by 61 one side of heating wire pedestal
The second through-hole 611 penetrate, by the gap between the first fever tablet 64 and the second fever tablet 65, led to by the second of another side
Hole 611 is pierced by.When draught line is wound, staff can manipulate remote controler starting fuse 6, the first fever tablet 64 and second
The fever of fever tablet 65 avoids damage unmanned plane with quick fuse draught line.
Fig. 3 and Fig. 4 are please referred to, the tabletting 63 is equipped with a counterbore 631, the corresponding counterbore of the heating wire pedestal 61
631 are equipped with threaded hole, and screw passes through the counterbore 631 and lock on threaded hole, and the tabletting 63 is fixed on heating wire bottom
On seat 61.6 structure of this fuse is simple, when the first fever tablet 64 or the damage of the second fever tablet 65, can quickly replace to it, more
When changing, the screw 66 in tabletting 63 need to only be back-outed, remove tabletting 63, then successively take out out of heating wire pedestal 61 cavity the
Two heating wires 65, heating wire bracket 62 and the first fever tablet 64 after the completion of replacement, then each part are successively assembled, finally
Lock screw 66, it is very convenient, quick.
Fig. 1 and Fig. 2 are please referred to, the line wheel 2 further includes across the first through hole 131 and being fixed on the side plate
Line wheel positioning sleeve 23 on 12, the both ends of the shaft 22 are fixed on the line wheel positioning sleeve 23.
In conclusion the utility model provides a kind of unmanned electro-mechanical force payingoff mechanism, which is mounted in
On unmanned plane, unmanned plane is along route flying overhead and discharges draught line, the utility model has the following beneficial effects:
(1) draught line is placed on unmanned plane, overcomes unmanned plane and more leaps slow problem；
(2) this unmanned electro-mechanical force payingoff mechanism is equipped with damper, staff can according to flying speed and payingoff speed from
The size that damping is adjusted on remote controler, prevent from damping too small, payingoff speed is too fast and the problem of cause coiling, damp it is excessive, put
Linear speed spends problem that is slow and causing unmanned plane during flying unstable；
(3) this unmanned electro-mechanical force payingoff mechanism is additionally provided with fuse, can quickly break when draught line is wound, and guarantees
The safety of unmanned plane.
The above is only the preferred embodiments of the present utility model only, is not intended to limit the utility model, all practical at this
Made any modifications, equivalent replacements, and improvements etc., should be included in the guarantor of the utility model within novel spirit and principle
Within the scope of shield.
Claims (8)
1. a kind of unmanned electro-mechanical force payingoff mechanism characterized by comprising bracket, the line wheel being located in the bracket, installation are solid
The damper for being scheduled on the bracket one side, is fixed on leading for the cradle bottom surface at the steering engine connecting with the damper
The control system of line apparatus and the fuse for being fixed on the cradle bottom surface, the fuse and unmanned plane connects, institute
State fuse include: in equipped with a cavity heating wire pedestal, be located at heating wire base cavity pocket two sides heating wire bracket,
The tabletting that is fixed on the heating wire pedestal, the first fever tablet being fastened between the tabletting and heating wire bracket,
And it is fastened on the second fever tablet between the heating wire bracket and heating wire pedestal.
2. unmanned electro-mechanical force payingoff mechanism according to claim 1, which is characterized in that the tabletting is equipped with a counterbore,
The heating wire pedestal corresponds to the counterbore equipped with threaded hole, and screw passes through the counterbore and lock on threaded hole, will be described
Tabletting is fixed on heating wire pedestal.
3. unmanned electro-mechanical force payingoff mechanism according to claim 1, which is characterized in that the bracket includes: bottom plate, installation
The both side plate being fixed on the bottom plate and the upper mounted plate being fixed on the side plate, both side plate are respectively provided with first
Through-hole.
4. unmanned electro-mechanical force payingoff mechanism according to claim 1, which is characterized in that open heating wire pedestal two sides
There is the second through-hole, draught line is across second through-hole and the first fever tablet and the second fever tablet.
5. unmanned electro-mechanical force payingoff mechanism according to claim 3, which is characterized in that the wire installation includes: to be located at
The gag lever post of the plate upper surface, the conductor rod for being located at the lower surface of base plate, the tension disk by the conductor rod, with
And it is fixed on the guide roller of the lower surface of base plate, draught line successively bypasses gag lever post, conductor rod, tension disk, fuse
And guide roller.
6. unmanned electro-mechanical force payingoff mechanism according to claim 3, which is characterized in that the line wheel includes I-beam wheel, wears
The shaft of the I-beam wheel is crossed, draught line is wound in the I-beam wheel.
7. unmanned electro-mechanical force payingoff mechanism according to claim 6, which is characterized in that the line wheel further includes across described
First through hole and the line wheel positioning sleeve being fixed on the side plate, it is fixed that the both ends of the shaft are fixed on the line wheel
Position is put on.
8. unmanned electro-mechanical force payingoff mechanism according to claim 1, which is characterized in that the damper include one with it is described
The turntable and an output shaft of steering engine connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821711581.XU CN208932717U (en) | 2018-10-22 | 2018-10-22 | Unmanned electro-mechanical force payingoff mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821711581.XU CN208932717U (en) | 2018-10-22 | 2018-10-22 | Unmanned electro-mechanical force payingoff mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208932717U true CN208932717U (en) | 2019-06-04 |
Family
ID=66725418
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821711581.XU Expired - Fee Related CN208932717U (en) | 2018-10-22 | 2018-10-22 | Unmanned electro-mechanical force payingoff mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208932717U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115626520A (en) * | 2022-11-11 | 2023-01-20 | 山东英特力光通信开发有限公司 | Unmanned aerial vehicle pay-off rack and using method |
-
2018
- 2018-10-22 CN CN201821711581.XU patent/CN208932717U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115626520A (en) * | 2022-11-11 | 2023-01-20 | 山东英特力光通信开发有限公司 | Unmanned aerial vehicle pay-off rack and using method |
| CN115626520B (en) * | 2022-11-11 | 2023-08-15 | 山东英特力光通信开发有限公司 | Unmanned aerial vehicle pay-off rack and use method |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190604 |