CN202508283U - Aircraft grounding device - Google Patents
Aircraft grounding device Download PDFInfo
- Publication number
- CN202508283U CN202508283U CN2011205449803U CN201120544980U CN202508283U CN 202508283 U CN202508283 U CN 202508283U CN 2011205449803 U CN2011205449803 U CN 2011205449803U CN 201120544980 U CN201120544980 U CN 201120544980U CN 202508283 U CN202508283 U CN 202508283U
- Authority
- CN
- China
- Prior art keywords
- rotating shaft
- wiinding cartridge
- aircraft
- ground contact
- steel rope
- 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 - Lifetime
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- Elimination Of Static Electricity (AREA)
Abstract
The utility model discloses an aircraft grounding device used for grounding and conducting static electricity when an aircraft is parked, maintained and refueled. The aircraft grounding device comprises a winding box, an aircraft plug, a handle and a rotating shaft, wherein one end of the handle is hinged with the winding box; the rotating shaft is arranged in the winding box; the two ends of the rotating shaft extend out of the winding box; a steel wire rope is positioned in the winding box and is coiled on the rotating shaft; the first end of the steel wire rope is fixed to the rotating shaft; and the second end of the steel wire rope can extend out of the winding box to connect the aircraft plug. The aircraft grounding device is small in size, simple in structure, convenient to use, and small in storage space.
Description
Technical field:
The utility model relates to ground contact and leads electrostatic technique, particularly be a kind of when being used for aircraft and parking, keep in repair and refuel ground connection lead the ground contact device of static.
Background technology:
At present, the ground contact device that uses on the airport is a kind of ground contact line of simple type.This ground contact line is made up of a cable, aircraft joint and earth terminal.Cable is about 12 m.A whole set of ground contact line is not only heavy, and bad harvesting, and is at random when use, storage, carries also inconvenience of transfer.
The utility model content:
The utility model be in order to overcome with epipodium not, to provide a kind of small and exquisite, light, ground contact device that can the folding and unfolding conductor wire.
The utility model ground contact device; Comprise Wiinding cartridge, aircraft plug, an end and Wiinding cartridge pivotally attached handle, be contained in the Wiinding cartridge and rotating shaft that Wiinding cartridge is stretched out at two ends; Be positioned at that first end that Wiinding cartridge is coiled in the steel rope in the rotating shaft is fixed in the rotating shaft and second end can stretch out that Wiinding cartridge is outer to be connected with the aircraft plug, during use, rotating shaft one end be right after ground stud steel rope is communicated with the earth; The ground hole that the aircraft plug injects on the aircraft gets final product safety.
Earth clamp is arranged in the above-mentioned device, be sleeved on steel rope and stretch out the connector on the Wiinding cartridge exterior portions, the two ends that connect steel rope are connected with connector with earth clamp respectively, and are safer.
Above-mentioned rotating shaft is stretched out on the end of Wiinding cartridge handwheel is housed.
All-in-one-piece with it is housed in the above-mentioned rotating shaft has the installation sleeve of mounting groove on it, and an end of steel rope stretches in the installation sleeve mounting groove and is fixed in the mounting groove.
Block plate, following block plate are housed in the above-mentioned Wiinding cartridge, and several two ends that are evenly distributed on the wrapping post of rotating shaft periphery are separately fixed on the upper and lower block plate.
The utility model ground contact device is used for aircraft when parking, keeping in repair and refueling, and ground connection is led static.Wiinding cartridge is enclosed within on the ground stud during use; And earth clamp clamps ground stud makes steel rope communicate with the earth; The aircraft plug injects the ground hole on the aircraft, and after two ends connected, aircraft and the earth formed a path through earth system; Reach the static of leading away on the aircraft, play the effect of safety precaution.
The utility model steel rope can move in the Wiinding cartridge fully, and handle is also collapsible, and whole device is light, small and exquisite, the use that is easy to carry, and device also can adopt corrosion protection design simultaneously, with the use of reply under inclement weather, accomplishes durable in use.Wiinding cartridge can be adopted when using aluminum alloy system, and that the aircraft plug terminal also uses is wear-resisting, the tin bronze manufacturing of corrosion resistant, and steel rope employing flexibility is good, good conductivity, corrosion-resistant steel steel rope that anti-corrosive properties is good, and it is the viton cover that handle casing can adopt.The utility model package unit compact conformation, rationally, anti-corrosive properties is good; Storage takes up room little, use, easy to carry, and the aircraft plug can change simultaneously; Can satisfy the user demand of different types of machines, the utility model ground contact device become " universalization, miniaturization ".
Description of drawings:
Fig. 1 is the utility model structural representation.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 is the A-A cutaway view among Fig. 1.
Fig. 4 is an I portion enlarged drawing among Fig. 3.
The specific embodiment:
Referring to Fig. 1～Fig. 4, present embodiment ground contact device comprises Wiinding cartridge 2, aircraft plug 3, an end and Wiinding cartridge pivotally attached handle 1, is contained in the Wiinding cartridge and rotating shaft 6 that Wiinding cartridge is stretched out at two ends, earth clamp 4.Rotating shaft is stretched out on the end of Wiinding cartridge handwheel 12 is housed.All-in-one-piece with it is housed in the Wiinding cartridge rotating shaft has the installation sleeve 8 of mounting groove 7 on it.Block plate 9, following block plate 10 are housed in the Wiinding cartridge.Several two ends that are evenly distributed on the wrapping post 11 of rotating shaft periphery are separately fixed on the upper and lower block plate.Being arranged in first end that Wiinding cartridge is coiled in the steel rope 5 on the several wrapping posts on the rotating shaft periphery stretches into the installation sleeve mounting groove and is fixed on mounting groove and second end stretches out that Wiinding cartridge is outer to be connected with the aircraft plug.Steel rope stretches out has connector 13 on the Wiinding cartridge exterior portions.The two ends that connect steel rope 14 are connected with connector with earth clamp respectively.
Claims (5)
1. ground contact device; It is characterized in that comprising Wiinding cartridge, aircraft plug, an end and Wiinding cartridge pivotally attached handle, be contained in the Wiinding cartridge and rotating shaft that Wiinding cartridge is stretched out at two ends, be positioned at that first end that Wiinding cartridge is coiled in the steel rope in the rotating shaft is fixed in the rotating shaft and second end can stretch out that Wiinding cartridge is outer to be connected with the aircraft plug.
2. ground contact device as claimed in claim 1 is characterized in that earth clamp is arranged in the device, is sleeved on steel rope and stretches out the connector on the Wiinding cartridge exterior portions, and the two ends that connect steel rope are connected with connector with earth clamp respectively.
3. according to claim 1 or claim 2 ground contact device is characterized in that rotating shaft is stretched out on the end of Wiinding cartridge handwheel is housed.
4. according to claim 1 or claim 2 ground contact device is characterized in that being equipped with in the rotating shaft installation sleeve that all-in-one-piece with it has mounting groove on it, and steel rope first end stretches in the installation sleeve mounting groove and is fixed in the mounting groove.
5. according to claim 1 or claim 2 ground contact device is characterized in that being equipped with in the Wiinding cartridge block plate, block plate down, and several two ends that are evenly distributed on the wrapping post of rotating shaft periphery are separately fixed on the upper and lower block plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205449803U CN202508283U (en) | 2011-12-23 | 2011-12-23 | Aircraft grounding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205449803U CN202508283U (en) | 2011-12-23 | 2011-12-23 | Aircraft grounding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202508283U true CN202508283U (en) | 2012-10-31 |
Family
ID=47060782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205449803U Expired - Lifetime CN202508283U (en) | 2011-12-23 | 2011-12-23 | Aircraft grounding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202508283U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103818562A (en) * | 2013-12-03 | 2014-05-28 | 海丰通航科技有限公司 | Airplane ground service integrated support system |
| CN104981085A (en) * | 2015-06-19 | 2015-10-14 | 成都飞机工业集团电子科技有限公司 | Grounding device |
| CN105905308A (en) * | 2016-06-14 | 2016-08-31 | 沈阳飞机工业（集团）有限公司 | Device for replacing fragile part conveniently |
| CN107702687A (en) * | 2017-09-27 | 2018-02-16 | 国网浙江省电力公司紧水滩水力发电厂 | Monitoring device applied to transformer station's subsidence monitoring of foundation |
-
2011
- 2011-12-23 CN CN2011205449803U patent/CN202508283U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103818562A (en) * | 2013-12-03 | 2014-05-28 | 海丰通航科技有限公司 | Airplane ground service integrated support system |
| CN104981085A (en) * | 2015-06-19 | 2015-10-14 | 成都飞机工业集团电子科技有限公司 | Grounding device |
| CN105905308A (en) * | 2016-06-14 | 2016-08-31 | 沈阳飞机工业（集团）有限公司 | Device for replacing fragile part conveniently |
| CN107702687A (en) * | 2017-09-27 | 2018-02-16 | 国网浙江省电力公司紧水滩水力发电厂 | Monitoring device applied to transformer station's subsidence monitoring of foundation |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201125 Address after: Floor 1, building 3, No. 10, Gaopeng Avenue, high tech Zone, Chengdu, Sichuan 610000 Patentee after: Chengdu Hangli Equipment Technology Co., Ltd Address before: 10 No. 610041 Sichuan province Chengdu Gaopeng Road Patentee before: CHENGDU HOLY AVIATION SCIENCE & TECHNOLOGY Co.,Ltd. |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20121031 |