CN102951301A - Ground anchor system used for mooring airplane - Google Patents
Ground anchor system used for mooring airplane Download PDFInfo
- Publication number
- CN102951301A CN102951301A CN2011102519940A CN201110251994A CN102951301A CN 102951301 A CN102951301 A CN 102951301A CN 2011102519940 A CN2011102519940 A CN 2011102519940A CN 201110251994 A CN201110251994 A CN 201110251994A CN 102951301 A CN102951301 A CN 102951301A
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- steel
- anchor
- ground anchor
- mooring
- ground
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Abstract
The invention provides a ground anchor system used for mooring airplanes, which does not influence the operation of service vehicles. The ground anchor system comprises an undergrounded steel barrel body, wherein the steel barrel body is provided with a steel cover plate, a steel anchor bar is fixed on the steel barrel body, the steel anchor bar is in a shape of a cross, and the center of the steel anchor bar is fixed with an anchor mooring ring. The ground anchor system used for mooring airplanes, which is provided by the invention, adopts a structure of a steel barrel with a steel cover, and can effectively solve defects of the existing ground anchor. When the ground anchor is not used, the cover is closed, and is aligned with the surface of a road surface, so that the ground anchor does not influence the driving of the vehicles and the traveling of passengers. The steel barrel is integrally cast, and can prevent the freezing and the melting of snowmelt and the corrosion of a deicing fluid from damaging the structure. The ground anchor is not provided with a free edge of plain concrete, so that the concrete around the ground anchor is difficult to damage. The ring hole of the mooring ring is large, and the mooring ring can be rotated, so that a steel wire rope can conveniently penetrate through the mooring ring.
Description
Technical field
The present invention relates to a kind of airfield equipment, especially a kind of ground anchor for tying airplane system.
Background technology
The ground anchor for tying airplane system reserves a bowl pockets at concrete pavement slab on the machine level ground at present, the annulus that the embedded light round bar curves in the hole.Mainly there is following problem in this earth anchor: when (1) earth anchor did not use, it formed pit on road face surface, affected the running comfort of various service vehicles on the machine level ground, and the passenger may fall down when stepping on because of carelessness earth anchor, injured; (2) bowl pockets of earth anchor is formed by plain concrete, and its limit section is as easy as rolling off a log falls the limit; (3) at northern area, the interior residual snowmelt of earth anchor pit in winter, deicing liquid easily cause the earth anchor concrete freeze-thaw damage of periphery and corrosion failure.And this concrete destruction is difficult to repair.(4) earth anchor reeve place is up and down arc, and opening is little, operating difficulties during reeve.
Summary of the invention
The invention provides a kind of ground anchor for tying airplane system that does not affect the service vehicle operation.
Realize a kind of ground anchor for tying airplane system of the object of the invention, comprise being positioned at underground steel drum body, described steel drum body is provided with steel deck-plate, is fixed with the anchor reinforcing bar on the described steel drum body, described anchor reinforcing bar across, and it is anchor ring that the center of described anchor reinforcing bar is fixed with.
Adjacent two free-ended intermediate distribution of described anchor reinforcing bar have many auxiliary bars, described auxiliary bar quadrangularly.
The beneficial effect of a kind of ground anchor for tying airplane of the present invention system is as follows:
A kind of ground anchor for tying airplane of the present invention system adopts the steel drum structure with the steel lid, can effectively solve the defective that above-mentioned existing earth anchor exists.When not using, builds by earth anchor lid, and concordant with face surface, road, do not affect Vehicle Driving Cycle and passenger current.The steel drum inblock cast can be resisted snowmelt, deicing liquid to freeze thawing and the corrosion failure of structure.Earth anchor does not have the free edge of plain concrete, and earth anchor periphery cement concrete is not easy to damage.Be that the anchor ring annular distance is large, can rotate, be convenient to reeve.
Description of drawings
Fig. 1 is the structural representation of a kind of ground anchor for tying airplane of the present invention system.
Fig. 2 is the upward view of Fig. 1.
The specific embodiment
As shown in Figure 1, 2, a kind of ground anchor for tying airplane of the present invention system comprises being positioned at underground steel drum body 1, described steel drum body 1 is provided with steel deck-plate 5, be fixed with anchor reinforcing bar 3 on the described steel drum body 1, described anchor reinforcing bar 3 across, it is anchor ring 2 that the center of described anchor reinforcing bar 3 is fixed with.
Adjacent two free-ended intermediate distribution of described anchor reinforcing bar 3 have many auxiliary bars 4, described auxiliary bar 4 quadrangularlies.
Embodiment recited above is described preferred implementation of the present invention; be not that scope of the present invention is limited; design under the spiritual prerequisite not breaking away from the present invention; various distortion and improvement that the common engineering staff in this area make technical solution of the present invention all should fall in the definite protection domain of claims of the present invention.
Claims (2)
1. ground anchor for tying airplane system, it is characterized in that: comprise being positioned at underground steel drum body, described steel drum body is provided with steel deck-plate, is fixed with the anchor reinforcing bar on the described steel drum body, described anchor reinforcing bar across, it is anchor ring that the center of described anchor reinforcing bar is fixed with.
2. ground anchor for tying airplane according to claim 1 system, it is characterized in that: adjacent two free-ended intermediate distribution of described anchor reinforcing bar have many auxiliary bars, described auxiliary bar quadrangularly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102519940A CN102951301A (en) | 2011-08-30 | 2011-08-30 | Ground anchor system used for mooring airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102519940A CN102951301A (en) | 2011-08-30 | 2011-08-30 | Ground anchor system used for mooring airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102951301A true CN102951301A (en) | 2013-03-06 |
Family
ID=47760806
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011102519940A Pending CN102951301A (en) | 2011-08-30 | 2011-08-30 | Ground anchor system used for mooring airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102951301A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184799A (en) * | 2016-07-25 | 2016-12-07 | 中国人民解放军总参谋部第六十研究所 | A kind of carrier-borne depopulated helicopter harpoon system |
| 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 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3904154A (en) * | 1974-05-13 | 1975-09-09 | Us Navy | Securing system for jet engine testing of aircraft |
| US20040258498A1 (en) * | 2003-05-30 | 2004-12-23 | Johannes Bruns | Apparatus for mounting lashing devices in a freight loading system of a transport conveyance, particularly an aircraft |
| CN101035695A (en) * | 2004-09-02 | 2007-09-12 | 艾利丹尼森公司 | Cover for a tie-down anchor |
| US7651305B1 (en) * | 2009-06-10 | 2010-01-26 | The United States Of America As Represented By The Secretary Of The Navy | Retractable fitting |
| CN202213722U (en) * | 2011-08-30 | 2012-05-09 | 中国民航机场建设集团公司 | Ground anchor for tying airplane |
-
2011
- 2011-08-30 CN CN2011102519940A patent/CN102951301A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3904154A (en) * | 1974-05-13 | 1975-09-09 | Us Navy | Securing system for jet engine testing of aircraft |
| US20040258498A1 (en) * | 2003-05-30 | 2004-12-23 | Johannes Bruns | Apparatus for mounting lashing devices in a freight loading system of a transport conveyance, particularly an aircraft |
| CN101035695A (en) * | 2004-09-02 | 2007-09-12 | 艾利丹尼森公司 | Cover for a tie-down anchor |
| US7651305B1 (en) * | 2009-06-10 | 2010-01-26 | The United States Of America As Represented By The Secretary Of The Navy | Retractable fitting |
| CN202213722U (en) * | 2011-08-30 | 2012-05-09 | 中国民航机场建设集团公司 | Ground anchor for tying airplane |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184799A (en) * | 2016-07-25 | 2016-12-07 | 中国人民解放军总参谋部第六十研究所 | A kind of carrier-borne depopulated helicopter harpoon system |
| 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 |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130306 |