CN205819588U - Earth anchor cover plate - Google Patents
Earth anchor cover plate Download PDFInfo
- Publication number
- CN205819588U CN205819588U CN201620512412.8U CN201620512412U CN205819588U CN 205819588 U CN205819588 U CN 205819588U CN 201620512412 U CN201620512412 U CN 201620512412U CN 205819588 U CN205819588 U CN 205819588U
- Authority
- CN
- China
- Prior art keywords
- cover plate
- earth anchor
- supporting plate
- keyhole
- plate
- 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
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- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
Abstract
The utility model discloses a kind of earth anchor cover plate, including supporting plate and cover plate, described supporting plate is provided with locking device, described cover plate is provided with keyhole and keyhole, described keyhole and described locking device connect, described supporting plate and cover plate connect through described locking device, and described cover plate is connected with the positioning lock of aircraft through described keyhole, and described supporting plate is connected with earth anchor.Earth anchor cover plate disclosed in the utility model, solves over the complicated procedures of fixing tire, and installs simple, and operation is simple, it is easy to arranges, is greatly saved labour force, improves efficiency；Locked cover plate when not using, maintains an equal level in order to keep the smooth and attractive in appearance of machine level ground with ground, prevents place hollow phenomenon；And it is easy to cleaning and the management on machine level ground, it is easy to winter clear the snow；Processed by antirust, anti-corrosive, add the service life of described earth anchor cover plate.
Description
Technical field
This utility model relates to airport equipment, especially a kind of earth anchor cover plate.
Background technology
On machine level ground, ground anchor for tying airplane system is to arrange a bowl pockets on concrete road surface at present, buries underground in hole
The earth anchor that reinforcing bar curves.This earth anchor is primarily present problems with: when earth anchor does not uses, and it forms pit, shadow on surface, machine level ground
Ring the operation of various service vehicles on machine level ground, passenger's imprudence step on earth anchor time may fall down, injured；In northern area, winter
In it earth anchor pit, residual snowmelt, easily causes freeze-thaw damage and the corrosion failure of earth anchor periphery concrete；Earth anchor reeves
Place, is arc up and down, and opening is little, operating difficulties when reeving, and the operating time is long.
Summary of the invention
In order to solve the problems referred to above, this utility model provides following proposal:
A kind of earth anchor cover plate, including supporting plate and cover plate, described supporting plate is provided with locking device, and described cover plate is provided with keyhole
With keyhole, described keyhole and described locking device connect, described supporting plate and cover plate connect through described locking device, described lid
Plate is connected with the positioning lock of aircraft through described keyhole, and described supporting plate is connected with earth anchor.
In this utility model, described locking device refers to the device described cover plate and described supporting plate being locked together, its
The locking requirement of strength of intensity anchor system contentedly of locking, described locking device can be lockset, such as the mechanical lock of safety cabinet,
Key is needed to operate；Can also be retaining mechanism, specifically see that the technology according to this area is configured, need similar key
Instrument carry out opening or locked.
In this utility model, described keyhole refers to the hole that coordinate phase-locked with described Plane location, and described keyhole refers to institute
State the hole that the key of locking device can pass through.
Preferably, described supporting plate is provided with supporting leg, and described supporting plate is connected with earth anchor through described supporting leg.The purpose so arranged is
While reaching system strength requirement, save material, improve economy.
Preferably, described cover plate is provided with pull-up hole.The purpose so arranged is opening of the most described cover plate.
Preferably, described supporting plate and/or described cover plate are provided with antirust, anti-corrosive layer.
Preferably, described antirust, anti-corrosive layer is set to zinc coat.
Preferably, described supporting plate and/or described cover plate are provided with wearing layer.
Preferably, described wearing layer is set to carbon fiber layer and/or alloy-layer.
Preferably, described supporting plate and/or described cover plate are provided with antistatic backing.
Preferably, described antistatic backing is set to carbon fiber layer.
In this utility model, described cover plate and described supporting plate are stamped to form by iron plate, do antirust, anti-corrosive the most again and process, with
Increase service life.
In this utility model, described cover plate is for being connected with the positioning lock of aircraft, then through described locking device with described
Supporting plate is fastenedly connected, and reaches the purpose of fastening aircraft tire, simple to operate, time-consuming, substantially increases efficiency.
The beneficial effect that this utility model produces:
Earth anchor cover plate disclosed in the utility model, solves over the complicated procedures of fixing tire, and installs simple, behaviour
Make simple, it is easy to arrange, be greatly saved labour force, improve efficiency；Locked cover plate when not using, maintains an equal level with ground and uses
To keep the smooth and attractive in appearance of machine level ground, prevent place hollow phenomenon；And it is easy to cleaning and the management on machine level ground, it is easy to winter
Clear the snow；Processed by antirust, anti-corrosive, add the service life of described earth anchor cover plate.
Accompanying drawing explanation
Fig. 1 is the structural representation of cover plate of the present utility model；
Fig. 2 is the structural representation of supporting plate of the present utility model；
Fig. 3 is the sectional view of supporting plate of the present utility model.
In figure:
Supporting plate 1, cover plate 2, locking device 3, keyhole 4, keyhole 5, supporting leg 6, pull-up hole 7.
Detailed description of the invention
Below in conjunction with the accompanying drawings, detailed description of the invention of the present utility model is described in further detail.
Earth anchor cover plate as shown in Figure 1, Figure 2 and Figure 3, including supporting plate 1 and cover plate 2, described supporting plate 1 is provided with locking device
3, described cover plate 2 is provided with keyhole 4 and keyhole 5, and described keyhole 5 and described locking device 3 connect, described supporting plate 1 and lid
Plate 2 connects through described locking device 3, and described cover plate 2 is connected with the positioning lock of aircraft through described keyhole 4.
Described supporting plate 1 is provided with supporting leg 6, and described supporting plate 1 is connected with earth anchor through described supporting leg 6.So arrange purpose be
While reaching system strength requirement, save material, improve economy.
Described cover plate 2 is provided with pull-up hole 7.The purpose so arranged is opening of the most described cover plate 2.
Described supporting plate 1 and described cover plate 2 are provided with antirust, anti-corrosive layer, and described antirust, anti-corrosive layer is set to zinc coat；Described supporting plate
Being provided with wearing layer with described cover plate, described wearing layer is set to alloy-layer；Described supporting plate and described cover plate are provided with antistatic backing, described
Antistatic backing is set to carbon fiber layer.The purpose so arranged is to increase the service life of described earth anchor cover plate and static electricity resistance
Energy.
Described cover plate 2 is connected with the positioning lock of aircraft, is then fastenedly connected with described supporting plate 1 through described locking device 3, reaches
To the purpose of fastening aircraft tire, simple to operate, time-consuming, substantially increase efficiency.
The above is only preferred implementation of the present utility model, it is noted that for the common skill of the art
For art personnel, on the premise of without departing from this utility model know-why, it is also possible to make some improvement, these improve also should
It is considered as protection domain of the present utility model.
Claims (9)
1. an earth anchor cover plate, it is characterised in that: including supporting plate (1) and cover plate (2), described supporting plate (1) is provided with locking device
(3), described cover plate (2) is provided with keyhole (4) and keyhole (5), described keyhole (5) and described locking device (3) and connects, institute
Stating supporting plate (1) and cover plate (2) to connect through described locking device (3), described cover plate (2) is through the location of described keyhole (4) Yu aircraft
Lock connects, and described supporting plate (1) is connected with earth anchor.
Earth anchor cover plate the most according to claim 1, it is characterised in that: described supporting plate (1) is provided with supporting leg (6), described supporting plate
(1) it is connected with earth anchor through described supporting leg (6).
Earth anchor cover plate the most according to claim 1 and 2, it is characterised in that: described cover plate (2) is provided with pull-up hole (7).
Earth anchor cover plate the most according to claim 1 and 2, it is characterised in that: described supporting plate (1) and/or described cover plate (2) set
There is antirust, anti-corrosive layer.
Earth anchor cover plate the most according to claim 4, it is characterised in that: described antirust, anti-corrosive layer is set to zinc coat and/or carbon
Fibrous layer.
Earth anchor cover plate the most according to claim 1 and 2, it is characterised in that: described supporting plate (1) and/or described cover plate (2) set
There is wearing layer.
Earth anchor cover plate the most according to claim 6, it is characterised in that: described wearing layer is set to carbon fiber layer and/or alloy
Layer.
Earth anchor cover plate the most according to claim 1 and 2, it is characterised in that: described supporting plate (1) and/or described cover plate (2) set
There is antistatic backing.
Earth anchor cover plate the most according to claim 8, it is characterised in that: described antistatic backing is set to carbon fiber layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620512412.8U CN205819588U (en) | 2016-05-31 | 2016-05-31 | Earth anchor cover plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620512412.8U CN205819588U (en) | 2016-05-31 | 2016-05-31 | Earth anchor cover plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205819588U true CN205819588U (en) | 2016-12-21 |
Family
ID=57559286
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620512412.8U Expired - Fee Related CN205819588U (en) | 2016-05-31 | 2016-05-31 | Earth anchor cover plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205819588U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113848083A (en) * | 2021-12-01 | 2021-12-28 | 中国飞机强度研究所 | Freezing and thawing prevention terrace for airplane test and freezing and thawing prevention parameter optimization method |
-
2016
- 2016-05-31 CN CN201620512412.8U patent/CN205819588U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113848083A (en) * | 2021-12-01 | 2021-12-28 | 中国飞机强度研究所 | Freezing and thawing prevention terrace for airplane test and freezing and thawing prevention parameter optimization method |
| CN113848083B (en) * | 2021-12-01 | 2022-02-18 | 中国飞机强度研究所 | Freezing and thawing prevention terrace for airplane test and freezing and thawing prevention parameter optimization method |
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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: 20161221 Termination date: 20190531 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |