CN202840361U - Primary guide rope remote control unhooking device - Google Patents
Primary guide rope remote control unhooking device Download PDFInfo
- Publication number
- CN202840361U CN202840361U CN 201220519636 CN201220519636U CN202840361U CN 202840361 U CN202840361 U CN 202840361U CN 201220519636 CN201220519636 CN 201220519636 CN 201220519636 U CN201220519636 U CN 201220519636U CN 202840361 U CN202840361 U CN 202840361U
- Authority
- CN
- China
- Prior art keywords
- remote control
- pin
- primary guide
- guide rope
- unhook
- 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.)
- Expired - Fee Related
Links
- 230000033001 locomotion Effects 0.000 abstract description 2
- 230000007613 environmental effect Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Abstract
The utility model discloses a primary guide rope remote control unhooking device. The primary guide rope remote control unhooking device comprises a first releasing hook. The first releasing hook is connected on a steering engine of an aircraft through a connecting rod and a crank arm. The primary guide rope remote control unhooking device further comprises a pin. One end of the pin is movably connected on a fixed frame of the steering engine through a pin rotating shaft, and the other end of the pin is hooked by the releasing hook. The releasing hook is movably connected on the fixed frame of the steering engine through a releasing hook rotating shaft. According to the primary guide rope remote control unhooking device, a remote control unhooking method is adopted, a primary guide rope only needs to be knotted and sleeved on the pin, when the aircraft throws the rope, ground remote control operation is adopted, the steering engine on the aircraft is used for carrying out movement, the releasing hook is pulled open through the connecting rod, one end of the pin slips off, the primary guide rope slips off from the pin at the same time, and the purpose of unhooking is achieved. The primary guide rope remote control unhooking device is high in reliability, simple in structure, convenient to operate, and economical and environment-friendly.
Description
Technical field
The utility model relates to a kind of tripping gear, particularly relates to a kind of preliminary leading rope remote control tripping gear.
Background technology
In the power transmission sequence Poling Construction, adopting the aircraft unfolding preliminary leading rope is the first program of Poling Construction.Behind assigned address, will carry out the shooting rope operation at the aircraft unfolding preliminary leading rope, both need preliminary leading rope is come off from aircraft.Existing tripping gear is generally the detonator blasting form, for disposable, and waste material and not environmental protection, and need to again do fag end at every turn, reduced operating efficiency.
Summary of the invention
For the deficiencies in the prior art, the purpose of this utility model is, a kind of preliminary leading rope remote control tripping gear is provided, and adopts remote control unhook mode, high, simple in structure, easy to operate, the economic environmental protection of reliability.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: preliminary leading rope remote control tripping gear, comprise a unhook, and it is characterized in that: described unhook is connected on the steering wheel of aircraft with cranking arm by connecting rod; Also comprise a pin, of described pin is movably connected in by the pin rotating shaft on the fixed mount of steering wheel, and the other end is hooked by described unhook, and described unhook is movably connected on the fixed mount of steering wheel by the unhook rotating shaft.
Aforesaid preliminary leading rope remote control tripping gear is characterized in that: between described unhook and the connecting rod, described connecting rod and crank arm between be flexibly connected by axle.
Aforesaid preliminary leading rope remote control tripping gear is characterized in that: described cranking arm is movably connected on the steering wheel by the rotating shaft of cranking arm.
Aforesaid preliminary leading rope remote control tripping gear is characterized in that: be provided with the receiving system that receives remote signal in the described steering wheel and control the control system of cranking arm and moving, described receiving system is connected with described control system.
The beneficial effects of the utility model are: adopt remote control unhook mode, only needing that preliminary leading rope is made a call to a knot is enclosed within on the pin, during the aircraft shooting rope, the operation of employing ground remote control, utilize carry-on steering wheel to move, pull open unhook by connecting rod, pin one end is come off, preliminary leading rope comes off from pin simultaneously, reaches the purpose of unhook.High, simple in structure, easy to operate, the economic environmental protection of the utility model reliability.
Description of drawings
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the left view of Fig. 1.
Embodiment
For further disclosing the technical solution of the utility model, describe execution mode of the present utility model in detail below in conjunction with accompanying drawing: as depicted in figs. 1 and 2, preliminary leading rope remote control tripping gear, comprise that one breaks off relations 1, break off relations 1 by connecting rod 2 and crank arm and 3 be connected on the steering wheel 4 of aircraft, break off relations 1 and connecting rod 2 between, connecting rod 2 and cranking arm is flexibly connected by axle 5 between 3, crank arm 3 to be movably connected on the steering wheel 4 by the rotating shaft 6 of cranking arm.Also comprise a pin 7, of pin 7 is movably connected in by pin rotating shaft 8 on the fixed mount 9 of steering wheel 4, and 1 hook by breaking off relations the other end, breaks off relations 1 to be movably connected on the fixed mount 9 of steering wheel 4 by unhook rotating shaft 10.Be provided with the receiving system that receives remote signal in the steering wheel 4 and control 3 control system of moving of cranking arm, receiving system is connected with control system.
Only needing during use that preliminary leading rope is made a call to a knot is enclosed within on the pin 7, during the aircraft shooting rope, the operation of employing ground remote control utilizes carry-on steering wheel 4 to move, and the receiving system in the steering wheel 4 receives the remote signal of ground remote control device emission, remote signal is sent to control system, then control system is controlled 3 motions of cranking arm, and pulls open by connecting rod 2 and breaks off relations 1, and pin 7 one ends are come off, preliminary leading rope comes off from pin 7 simultaneously, reaches the purpose of unhook.High, simple in structure, easy to operate, the economic environmental protection of the utility model reliability.
More than by description of listed embodiment, basic conception of the present utility model and basic principle have been set forth.But the utility model never is limited to above-mentioned listed execution mode, and every equivalent variations, improvement and deliberately of inferior quality behavior of change of doing based on the technical solution of the utility model all should belong to protection range of the present utility model.
Claims (4)
1. preliminary leading rope remote control tripping gear comprises a unhook, it is characterized in that: described unhook is connected on the steering wheel of aircraft with cranking arm by connecting rod; Also comprise a pin, of described pin is movably connected in by the pin rotating shaft on the fixed mount of steering wheel, and the other end is hooked by described unhook, and described unhook is movably connected on the fixed mount of steering wheel by the unhook rotating shaft.
2. preliminary leading rope remote control tripping gear according to claim 1 is characterized in that: between described unhook and the connecting rod, described connecting rod and crank arm between be flexibly connected by axle.
3. preliminary leading rope remote control tripping gear according to claim 1, it is characterized in that: described cranking arm is movably connected on the steering wheel by the rotating shaft of cranking arm.
4. arbitrary described preliminary leading rope remote control tripping gear according to claim 1-3 is characterized in that: be provided with the receiving system that receives remote signal in the described steering wheel and control the control system of cranking arm and moving, described receiving system is connected with described control system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220519636 CN202840361U (en) | 2012-10-11 | 2012-10-11 | Primary guide rope remote control unhooking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220519636 CN202840361U (en) | 2012-10-11 | 2012-10-11 | Primary guide rope remote control unhooking device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202840361U true CN202840361U (en) | 2013-03-27 |
Family
ID=47951979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220519636 Expired - Fee Related CN202840361U (en) | 2012-10-11 | 2012-10-11 | Primary guide rope remote control unhooking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202840361U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103368103A (en) * | 2013-05-09 | 2013-10-23 | 衡水众翔电子科技有限公司 | Flying device and method for hanging sag wire on electric transmission line |
| CN103904587A (en) * | 2014-04-25 | 2014-07-02 | 国家电网公司 | Hot-line work line throwing device |
| CN104037647A (en) * | 2014-05-07 | 2014-09-10 | 国家电网公司 | Bolt cutter hook |
| CN105539737A (en) * | 2015-12-31 | 2016-05-04 | 国家海洋局第一海洋研究所 | Water-borne electronic remote control releaser |
| CN104242144B (en) * | 2013-06-20 | 2016-10-19 | 国家电网公司 | A kind of saving casting device |
-
2012
- 2012-10-11 CN CN 201220519636 patent/CN202840361U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103368103A (en) * | 2013-05-09 | 2013-10-23 | 衡水众翔电子科技有限公司 | Flying device and method for hanging sag wire on electric transmission line |
| CN103368103B (en) * | 2013-05-09 | 2016-01-20 | 衡水众翔电子科技有限公司 | For hanging flight instruments and the method for sag rope to transmission line |
| CN104242144B (en) * | 2013-06-20 | 2016-10-19 | 国家电网公司 | A kind of saving casting device |
| CN103904587A (en) * | 2014-04-25 | 2014-07-02 | 国家电网公司 | Hot-line work line throwing device |
| CN104037647A (en) * | 2014-05-07 | 2014-09-10 | 国家电网公司 | Bolt cutter hook |
| CN105539737A (en) * | 2015-12-31 | 2016-05-04 | 国家海洋局第一海洋研究所 | Water-borne electronic remote control releaser |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130327 Termination date: 20141011 |
|
| EXPY | Termination of patent right or utility model |