CN103057724B - A kind of Aerobridge stabilizer - Google Patents
A kind of Aerobridge stabilizer Download PDFInfo
- Publication number
- CN103057724B CN103057724B CN201310005556.5A CN201310005556A CN103057724B CN 103057724 B CN103057724 B CN 103057724B CN 201310005556 A CN201310005556 A CN 201310005556A CN 103057724 B CN103057724 B CN 103057724B
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- CN
- China
- Prior art keywords
- cam
- stabilizing leg
- aerobridge
- stabilizer
- driver train
- 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
- 239000003381 stabilizer Substances 0.000 title claims abstract description 12
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 19
- 230000000694 effects Effects 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Abstract
The invention discloses a kind of Aerobridge stabilizer, be arranged at the supporting traverse two ends of the running gear of connecting bridge, the driver train comprising stabilizing leg, cam and rotate for power cam, described stabilizing leg upper end is fixedly connected with walking crossbeam, described cam and driver train are arranged on the lower end of stabilizing leg, described cam can form stable support point, increases the wind resisting stability of connecting bridge.Adopt the present invention of said structure after connecting bridge completes and dock with aircraft, start driver train, the rotation of band moving cam, until cam edge and earth surface, plays the effect of stable support Boarding bridge access.Structure of the present invention is simple, easy to operate.
Description
Technical field
The present invention relates to a kind of Aerobridge stabilizer.
Background technology
Existing flexible connecting bridge system is generally by the hinged weight supporting Boarding bridge access on its walking wheel carrier; This type of flexible connecting bridge structure easily causes connecting bridge to rock, and particularly rocking when connecting bridge is higher can be more obvious.In order to take into account stability, running gear also has and adopts two-wheel shelf structure, and the stability of this type of running gear is better, but realizing this class formation need arrange synchronous rotary mechanism, make the structure of product more complicated, cost is higher, reliability is low.Based on above reason, the invention provides a kind of Aerobridge stabilizer, in order to stable support Boarding bridge access, improve the stability of connecting bridge, make running gear can simple designs as much as possible.
Summary of the invention
In order to solve the problem, the invention provides a kind of Aerobridge stabilizer.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of Aerobridge stabilizer, be arranged at the supporting traverse two ends of the running gear of connecting bridge, the driver train comprising stabilizing leg, cam and rotate for power cam, described stabilizing leg upper end is fixedly connected with supporting traverse, described cam and driver train are arranged on the lower end of stabilizing leg, described cam can form stable support point, increases the wind resisting stability of connecting bridge.
The drop-gear box that described driver train comprises motor and is connected with motor output shaft, described cam is fixedly mounted on reduction gearbox output shaft.
Described cam edge is coated with rubber cushion.
Described cam is arranged on stabilizing leg side.
Described cam is arranged on immediately below stabilizing leg.
The invention has the beneficial effects as follows: adopt the present invention of said structure after connecting bridge completes expansion, start driver train, band moving cam rotates, until cam edge and earth surface, play the effect of stable support Boarding bridge access, and responded to by current detecting and control motor.Structure of the present invention is simple, easy to operate.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described:
Fig. 1 is the front view of the first embodiment of the present invention;
Fig. 2 is the right elevation of Fig. 1;
Fig. 3 is the front view of the second embodiment of the present invention;
Fig. 4 is the right elevation of Fig. 3.
Detailed description of the invention
With reference to Fig. 1 ~ Fig. 2, as shown in the figure be the first embodiment of the present invention, the present invention is a kind of Aerobridge stabilizer, comprise stabilizing leg 4, cam 1 and the driver train rotated for power cam 1, cam 1 edge is used for and earth surface, stabilizing leg 4 upper end is connected with the supporting traverse end winding support of the running gear of connecting bridge, driver train is arranged in stabilizing leg 4, driver train comprises the motor 2 be arranged on stabilizing leg 4 and the drop-gear box 3 be connected with motor 2 output shaft, cam 1 is fixedly mounted on drop-gear box 3 output shaft, cam 1 edge is coated with one deck rubber cushion 5, increase the contact surface on cam 1 and ground, improve the stability of stable support, cam 1 is arranged on stabilizing leg 4 side.Adopt said structure the present invention connecting bridge walking process cam 1 not with earth surface, after connecting bridge completes and docks with aircraft, starter motor 2, band moving cam 1 rotates, until cam 1 edge and earth surface, play the effect of stable support Boarding bridge access, and responded to by current detecting and control motor 2.Structure of the present invention is simple, easy to operate.
With reference to Fig. 3 ~ Fig. 4, as shown in the figure be the second embodiment of the present invention, it is substantially identical with the first embodiment, and difference is that cam 1 is arranged on immediately below stabilizing leg 4.
Above-described embodiment is preferred version of the present invention, and the present invention also can have other embodiments.Those skilled in the art also can make equivalent variations or replacement under the prerequisite without prejudice to spirit of the present invention, and these equivalent modification or replacement are all included in the application's claim limited range.
Claims (4)
1. an Aerobridge stabilizer, it is characterized in that, be arranged at the supporting traverse two ends of the running gear of connecting bridge, the driver train comprising stabilizing leg (4), cam (1) and rotate for power cam (1), described stabilizing leg (4) upper end is fixedly connected with walking crossbeam, described cam (1) and driver train are arranged on the lower end of stabilizing leg (4), and described cam (1) can form stable support point; The drop-gear box (3) that described driver train comprises motor (2) and is connected with motor (2) output shaft, described cam (1) is fixedly mounted on drop-gear box (3) output shaft.
2. a kind of Aerobridge stabilizer as claimed in claim 1, is characterized in that described cam (1) edge is coated with rubber cushion (5).
3. a kind of Aerobridge stabilizer as claimed in claim 2, is characterized in that described cam (1) is arranged on stabilizing leg (4) side.
4. a kind of Aerobridge stabilizer as claimed in claim 2, is characterized in that described cam (1) is arranged on immediately below stabilizing leg (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310005556.5A CN103057724B (en) | 2013-01-08 | 2013-01-08 | A kind of Aerobridge stabilizer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310005556.5A CN103057724B (en) | 2013-01-08 | 2013-01-08 | A kind of Aerobridge stabilizer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103057724A CN103057724A (en) | 2013-04-24 |
| CN103057724B true CN103057724B (en) | 2016-03-30 |
Family
ID=48100683
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310005556.5A Expired - Fee Related CN103057724B (en) | 2013-01-08 | 2013-01-08 | A kind of Aerobridge stabilizer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103057724B (en) |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1332854C (en) * | 2004-02-26 | 2007-08-22 | 中国国际海运集装箱(集团)股份有限公司 | Ancillary shoring set of aerobridge and aerobridge with the set controlling method |
| CN201484665U (en) * | 2009-09-04 | 2010-05-26 | 蒂森克虏伯机场系统(中山)有限公司 | Auxiliary supporting device of passenger boarding bridge |
| CN202541845U (en) * | 2012-03-16 | 2012-11-21 | 蒂森克虏伯机场系统(中山)有限公司 | Auxiliary stabilizing device for boarding bridge |
| CN203172890U (en) * | 2013-01-08 | 2013-09-04 | 蒂森克虏伯机场系统(中山)有限公司 | Boarding bridge stabilizing device |
-
2013
- 2013-01-08 CN CN201310005556.5A patent/CN103057724B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN103057724A (en) | 2013-04-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160330 |