CN208515822U - A kind of aircraft rubber catch with locking device - Google Patents
A kind of aircraft rubber catch with locking device Download PDFInfo
- Publication number
- CN208515822U CN208515822U CN201820735562.4U CN201820735562U CN208515822U CN 208515822 U CN208515822 U CN 208515822U CN 201820735562 U CN201820735562 U CN 201820735562U CN 208515822 U CN208515822 U CN 208515822U
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- China
- Prior art keywords
- rubber catch
- rod assembly
- tightener
- drag link
- hole
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Abstract
The utility model discloses a kind of aircraft rubber catch with locking device, including being placed in two rubber catch before and after wheel rolling surface, being laterally interspersed in two drag links of rubber catch central through hole respectively and cover on drag link for tensing the elastic rod assembly of drag link；Elastic rod assembly is two sets, is symmetrical set, and every elastic rod assembly of set includes tightener and two front and back pull rods；Tightener rear and front end is equipped with coaxial and opposite hand of spiral threaded hole；One end of front and back pull rod is equipped with the circular hole passed through for drag link, and the other end is equipped with the threaded post with tightener screw hole.The utility model adjusts the distance between wheel front and back rubber catch by locking device, can quickly and easily lock airplane wheel, and can quickly remove, the locking of rubber catch is stronger, and easy to operate, time saving and energy saving.
Description
Technical field
The utility model relates to airplane ground support equipment fields, and in particular to a kind of aircraft rubber with locking device
Catch.
Background technique
Under strong wind weather, aircraft needs to take Ground Mooring measure, prevents from being blown by strong wind and causes accidental injury.In aircraft
Setting catch is one of aircraft picketing measure before and after wheel.Civil aircraft generallys use rubber catch at present, usually manually makes
The rubber catch before and after wheel is bundled with rope.Artificial binding catch, low efficiency, the time is long, and binding mode is different, it is elastic not
Deng.
Utility model content
To solve the above problems, the utility model provides a kind of aircraft rubber catch with locking device, can be convenient
Quickly rubber catch before and after airplane wheel is locked, securely and reliably, locking is secured.
In order to achieve the above object, the technical scheme adopted by the utility model is that:
A kind of aircraft rubber catch with locking device, including two rubber wheels being placed in front of and after wheel rolling surface
Gear is laterally interspersed in two drag links of rubber catch central through hole respectively and covers between two drag links for tensing
The elastic rod assembly of drag link；Elastic rod assembly is two sets, is symmetrical set, every elastic rod assembly of set includes pine
Tight device and two front and back pull rods；Tightener rear and front end is equipped with coaxial and opposite hand of spiral threaded hole；The one of front and back pull rod
End is equipped with the circular hole passed through for drag link, and the other end is equipped with the threaded post with tightener screw hole.
Further, to prevent front and back pull rod from falling off from drag link end, the both ends of the drag link are equipped with pin hole, described
Elastic rod assembly further includes two lock pins being plugged in pin hole.
Compared with prior art, the utility model has the beneficial effects that:
The rubber catch of the utility model adjusts the distance between wheel front and back rubber catch by locking device, can
Airplane wheel quickly and easily to be lockked, and can quickly be removed, the locking of rubber catch is stronger, and easy to operate,
It is time saving and energy saving.
Detailed description of the invention
Fig. 1 is the structural schematic diagram one of the utility model；
Fig. 2 is the structural schematic diagram two of the utility model；
Description of symbols: 1- drag link；2- tightener；Pull rod before and after 3-；4- lock pin；5- pin hole；6- rubber catch；7-
Wheel.
Specific embodiment
The content of the utility model is described in further details with reference to the accompanying drawings and detailed description.
Embodiment:
As depicted in figs. 1 and 2, a kind of aircraft rubber catch with locking device, including it is respectively placed in the rolling of wheel 7
It two rubber catch 6 after in front, the drag link 1 being interspersed on rubber catch 6 and covers on drag link 1 for tensing cross
The locking rod assembly of pull rod 1.
Rubber catch 6 is triangular in shape, which is provided with the central through hole parallel with 7 axial direction of wheel, and drag link 1 is front and back two
Root is respectively interposed in the central through hole of rubber catch 6, and the length of drag link 1 is greater than the width of rubber catch 6, and both ends are exposed
Outside 6 end face of rubber catch, for being connect with locking rod assembly.
Elastic rod assembly is two sets, is symmetrical set, and every set is locked by 1 tightener, 2,2 front and back pull rods 3 and 2
Pin 4 forms.Tightener 2 is rectangular configuration, and the threaded hole of coaxial line, and front and back screw thread is arranged in rear and front end face middle position
The hand of spiral in hole is opposite.Circular hole is arranged in one end of front and back pull rod 3, is exposed at rubber catch 6 at 1 both ends of drag link so as to cover
On bar other than both ends of the surface, pin hole 5 is arranged in 1 end of drag link, prevents front and back pull rod 3 from falling off for installing lock pin 4.Front and back pull rod
3 other end is equipped with threaded post, and the direction that is in line is mounted in the threaded hole of 2 rear and front end of tightener, rotates adjusting elasticity device
2, front and back pull rod 3 can be made to protract in the opposite direction and retraction, to pull drag link 1 that rubber catch 6 is driven closely to recline
On 7 tyre surface of wheel, play the role of lockking wheel 7.
In use, rubber catch 6 is respectively placed in 7 front and back of wheel, drag link 1 is through to the center of rubber catch 6 respectively
In through-hole, by the length of 2 adjusting elasticity rod assembly of tightener to suitable position, front and back pull rod 3 is respectively fitted over drag link 1
Both ends, insertion lock pin 4 is completed pre-assembled, then rotate the tighteners 2 of 7 two sides of wheel simultaneously, tense drag link 1 to centre,
To which rubber catch 6 is locked at the front and back of wheel 7, and when needing to unclamp, as long as opposite direction rotates tightener 2.
Above-listed detailed description is illustrating for the utility model possible embodiments, and the embodiment is not to limit
The scope of the patents of the utility model, all equivalence enforcements or change without departing from carried out by the utility model, is intended to be limited solely by this case
In the scope of the patents.
Claims (2)
1. a kind of aircraft rubber catch with locking device, it is characterised in that: including be placed in front of and after wheel rolling surface two
A rubber catch is laterally interspersed in two drag links of rubber catch central through hole and covers between two drag links respectively
For tensing the elastic rod assembly of drag link；Elastic rod assembly is two sets, is symmetrical set, every elastic rod assembly of set
It include tightener and two front and back pull rods；Tightener rear and front end is equipped with coaxial and opposite hand of spiral threaded hole；Front and back
One end of pull rod is equipped with the circular hole passed through for drag link, and the other end is equipped with the threaded post with tightener screw hole.
2. according to the aircraft rubber catch described in claim 1 with locking device, it is characterised in that: the both ends of the drag link
Equipped with pin hole, the elastic rod assembly further includes two lock pins being plugged in pin hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820735562.4U CN208515822U (en) | 2018-05-17 | 2018-05-17 | A kind of aircraft rubber catch with locking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820735562.4U CN208515822U (en) | 2018-05-17 | 2018-05-17 | A kind of aircraft rubber catch with locking device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208515822U true CN208515822U (en) | 2019-02-19 |
Family
ID=65339158
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820735562.4U Active CN208515822U (en) | 2018-05-17 | 2018-05-17 | A kind of aircraft rubber catch with locking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208515822U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113415437A (en) * | 2021-08-25 | 2021-09-21 | 民航成都物流技术有限公司 | Anti-sliding device for automatic wheel chock of vehicle |
-
2018
- 2018-05-17 CN CN201820735562.4U patent/CN208515822U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113415437A (en) * | 2021-08-25 | 2021-09-21 | 民航成都物流技术有限公司 | Anti-sliding device for automatic wheel chock of vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: Room 103, East Haikou Free Trade Zone, 168 Nanhai Avenue, Xiuying District, Haikou City, Hainan Province, 570311 Patentee after: HNA TECHNIK Co.,Ltd. Address before: 571126 Strategic Development Department, 5F, HNA Maintenance Skills Training Center, HNA Base, Meilan Airport, Haikou, Hainan Patentee before: HNA TECHNIC CO.,LTD. |