CN207089683U - A kind of easy unmanned plane mooring device - Google Patents
A kind of easy unmanned plane mooring device Download PDFInfo
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- CN207089683U CN207089683U CN201721001765.2U CN201721001765U CN207089683U CN 207089683 U CN207089683 U CN 207089683U CN 201721001765 U CN201721001765 U CN 201721001765U CN 207089683 U CN207089683 U CN 207089683U
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- China
- Prior art keywords
- tethered
- bushing
- anticreep
- unmanned plane
- hanger
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Abstract
It the utility model is related to a kind of easy unmanned plane mooring device, it is characterised in that by being tethered at base, anticreep bushing, hanger, hook and captive band composition；Being tethered at floor installation unmanned plane needs to be tethered at position；Anticreep bushing, which is arranged on to be tethered on base, to be used to install hanger, while anticreep bushing one end protrudes covering face；Hanger is connected on anticreep bushing, and hanger termination is used for coupling hook；Captive band both ends equipped with hook, for connect be tethered at a little and ground fixed position or transport fixing point.The utility model meets that unmanned plane is parked and transport is tethered at requirement, while mooring device is in light weight, and cost is low, simple and practical；It is tethered at base and uses aerolite alleviator weight, meet aviation requirement, anticreep bushing uses steel alloy, and wearability is good, prevents damage to be tethered at base, anticreep bushing easy installation and removal；Device is simple, and the cumbersome mooring device of weight is light；The present apparatus is simple and practical, in light weight, and cost is low.
Description
Technical field
A kind of unmanned plane mooring device technical field is the utility model is related to, is a kind of improved easy specifically
Unmanned plane mooring device.
Background technology
Unmanned plane mooring device is to transport and parking security consideration for unmanned plane.At present, the condition under normal climate
Under, unmanned plane is typically braked using catch.But when there is atrocious weather or in transportation, in order to prevent aircraft from producing
The breakoff phenomenon such as rollover or sliding, especially in the case of surface strong wind, the load for all directions born due to aircraft is larger,
For ensure aircraft park safety, it is necessary to increase the measure of being tethered at, it is existing aircraft picketing device include adjusting means, top connection,
The components such as lower contact, mooring guy, so carry out institute's mooring device complexity for unmanned plane, cost is higher, and weight is also heavier, and
It is unfavorable for replacing and is tethered at a position, the utility model is easy to use, changes facility, and cost is low.
Based on this, present application is made.
Utility model content
The purpose of this utility model is overcome the deficiencies in the prior art, there is provided a kind of easy unmanned plane mooring device.
The purpose of this utility model is achieved through the following technical solutions：
A kind of easy unmanned plane mooring device, by being tethered at base, anticreep bushing, hanger, hook and captive band composition；
Being tethered at floor installation unmanned plane needs to be tethered at position；Anticreep bushing, which is arranged on to be tethered on base, to be used to install hanger,
Play it is wear-resisting prevent that hanger from pulling de- effect, while anticreep bushing one end protrudes covering face, and protection covering prevents covering due to hanging
Ear rocks destruction covering；Hanger is connected on anticreep bushing, and hanger termination can be used for coupling hook；Captive band both ends are equipped with extension
Hook, for connect be tethered at a little and ground fixed position or transport fixing point.
Further, can be adjusted as the size and structural shape for being tethered at base according to a locational space is tethered at；Make
It can reduce covering opening with anticreep bushing, prevent local openings are excessive from influenceing aircraft skin integral rigidity and performance, be simultaneously
Protection covering, destroys stressed-skin construction when preventing hanger from tightening or rocking, the anticreep bushing other end need to protrude covering face, anticreep lining
Set length dimension can be adjusted according to actual skin thickness, and slightly prominent skin shape face 2mm is advisable；The big I of hanger according to
Real aircraft parks the stressing conditions born when ground is prominent to fly and selects suitable hanger size.
The easy unmanned plane mooring device of the application is mainly by a kind of easy unmanned plane mooring device, by being tethered at base,
Anticreep bushing, hanger, hook and captive band are formed.It is tethered at base and typically uses the aluminium alloy of aviation 7050 or 7075, it is in light weight, strong
Spend.It is tethered at base center and opens circular hole, for installing anticreep bushing, this circular hole should be less than anticreep insert diameter, use K7 tolerances
Coordinate.Anticreep bushing screwed hole of centre is because of hanger to be installed, therefore anticreep bushing uses high rigidity 30CrMnSiA hard alloy
Steel, wearability are good.Anticreep bushing is with lining shoulder, and lining shoulder external diameter is bigger 4mm than Outer Diameter of lining, and lining shoulder can effectively prevent hanger from serving as a contrast
Set pulls de-.Bushing endoporus is screwed hole, and for installing hanger, bushing lower outer diameter is bigger 4mm than internal diameter to be advisable, can be according to reality
Unmanned plane stressing conditions are adjusted.In order to prevent hanger from tightening or cause skin-surface stress when rocking, covering knot is destroyed
Structure, anticreep bushing lower surface should slightly protrude skin shape face 2mm, while skin-surface opening should be bigger than anticreep bushing lower diameter
2mm, for bushing by the way that the length dimension of anticreep bushing can be adjusted according to actual skin thickness.Hanger (GB825) connects
Onto anticreep bushing, the prominent winged situation in ground can be parked according to unmanned plane weight and place and selects suitable hanger.Captive band both ends
Equipped with hook (HB6391) be used for connection be tethered at a little with local fixed position or transport fixing point.
Operation principle of the present utility model is：First the insertion of anticreep bushing is tethered on base, according to unmanned plane grid beam position,
It is determined that being tethered at understructure, base is tethered at using rivet in unmanned grid beam, hanger is directly threaded into anticreep bushing, is tethered at
Band both ends for being connected a little and being tethered at a little, are tethered to aircraft equipped with hook (HB6391), prevent the prominent wind in ground or fortune
Defeated middle aircraft is damaged.When aircraft needs flight, back-out hanger.
Compared with prior art, good effect of the present utility model is：
Meet that unmanned plane is parked and transport is tethered at requirement, while mooring device is in light weight, cost is low, simple and practical.
It is tethered at base and uses aerolite alleviator weight, meets aviation requirement, anticreep bushing uses alloy
Steel, wearability is good, prevents damage to be tethered at base, anticreep bushing easy installation and removal.Because simple in construction effectively reduce is processed into
This, while install and change conveniently, reduce later stage working service cost.Because device is simple, weight it is cumbersome be tethered at dress
Put light.The present apparatus is simple and practical, in light weight, and cost is low.
Brief description of the drawings
Fig. 1 is schematic diagram of the present utility model；
Fig. 2 is the utility model schematic view of the mounting position；
Fig. 3 is the utility model structure diagram；
Fig. 4 is the utility model section figure；
Fig. 5 changes schematic diagram to be tethered at understructure；
Label in figure：1. it is tethered at base；2 anticreep bushings；3 hangers；4 hooks；5 captive bands；6 beams；7 frames；8 bottom coverings.
Embodiment
A kind of embodiment of easy unmanned plane mooring device of the utility model presented below.
Embodiment 1
A kind of easy unmanned plane mooring device of the present embodiment, with reference to figure by being tethered at base 1, anticreep bushing 2, gasket ring 3, extension
Hook 4 (HB6391) and captive band 5 are formed.Base 1 is tethered to be fixed on Airplane frame and beam, anticreep bushing 2, which is embedded in, to be tethered on bottom,
Hanger 3 is arranged on anticreep bushing, and the connection hanger of hook 4 and captive band, captive band 5 are connected a little and be tethered at a little.Wherein it is
Seat 1 of keeping on file can restructure pattern according to a position is tethered at, and refer to Fig. 5.
The easy unmanned plane mooring device of the application is mainly by a kind of easy unmanned plane mooring device, by being tethered at base,
Anticreep bushing, hanger, hook and captive band are formed.It is tethered at base and typically uses the aluminium alloy of aviation 7050 or 7075, it is in light weight, strong
Spend.It is tethered at base center and opens circular hole, for installing anticreep bushing, this circular hole should be less than anticreep insert diameter, use K7 tolerances
Coordinate.Anticreep bushing screwed hole of centre is because of hanger to be installed, therefore anticreep bushing uses high rigidity 30CrMnSiA hard alloy
Steel, wearability are good.Anticreep bushing is with lining shoulder, and lining shoulder external diameter is bigger 4mm than Outer Diameter of lining, and lining shoulder can effectively prevent hanger from serving as a contrast
Set pulls de-.Bushing endoporus is screwed hole, and for installing hanger, bushing lower outer diameter is bigger 4mm than internal diameter to be advisable, can be according to reality
Unmanned plane stressing conditions are adjusted.In order to prevent hanger from tightening or cause skin-surface stress when rocking, covering knot is destroyed
Structure, anticreep bushing lower surface should slightly protrude skin shape face 2mm, while skin-surface opening should be bigger than anticreep bushing lower diameter
2mm, for bushing by the way that the length dimension of anticreep bushing can be adjusted according to actual skin thickness.Hanger (GB825) connects
Onto anticreep bushing, the prominent winged situation in ground can be parked according to unmanned plane weight and place and selects suitable hanger.Captive band both ends
Equipped with hook (HB6391) be used for connection be tethered at a little with local fixed position or transport fixing point.
Operation principle of the present utility model is：First the insertion of anticreep bushing is tethered on base, according to unmanned plane grid beam position,
It is determined that being tethered at understructure, base is tethered at using rivet in unmanned grid beam, hanger is directly threaded into anticreep bushing, is tethered at
Band both ends for being connected a little and being tethered at a little, are tethered to aircraft equipped with hook (HB6391), prevent the prominent wind in ground or fortune
Defeated middle aircraft is damaged.When aircraft needs flight, back-out hanger.
Described above is only preferred embodiment of the present utility model, it is noted that for the common skill of the art
Art personnel, without departing from the concept of the premise utility, some improvements and modifications can also be made, these improvements and modifications
Also should be regarded as in the scope of protection of the utility model.
Claims (6)
1. a kind of easy unmanned plane mooring device, it is characterised in that by being tethered at base, anticreep bushing, hanger, link up with and be tethered at
Band composition；Being tethered at floor installation unmanned plane needs to be tethered at position；Anticreep bushing, which is arranged on to be tethered on base, to be used to install hanger, together
When anticreep bushing one end protrude covering face；Hanger is connected on anticreep bushing, and hanger termination is used for coupling hook；Captive band both ends
Equipped with hook, it is tethered at a little for connecting and ground fixed position or transports fixing point.
2. a kind of easy unmanned plane mooring device as claimed in claim 1, it is characterised in that be tethered at base typically using boat
Empty 7050 or 7075 aluminium alloys.
3. a kind of easy unmanned plane mooring device as claimed in claim 1, it is characterised in that be tethered at base center and open circle
Hole, for installing anticreep bushing, this circular hole should be less than anticreep insert diameter, use K7 tolerance fits.
4. a kind of easy unmanned plane mooring device as claimed in claim 1, it is characterised in that anticreep bushing uses high rigidity
30CrMnSiA hard alloy steels.
A kind of 5. easy unmanned plane mooring device as claimed in claim 1, it is characterised in that anticreep bushing carries lining shoulder,
It is bigger 4mm than Outer Diameter of lining to serve as a contrast shoulder external diameter, it is de- that lining shoulder can effectively prevent hanger from pulling bushing.
6. a kind of easy unmanned plane mooring device as claimed in claim 1, it is characterised in that anticreep bushing endoporus is screw thread
Hole, for installing hanger, bushing lower outer diameter is bigger 4mm than internal diameter to be advisable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721001765.2U CN207089683U (en) | 2017-08-11 | 2017-08-11 | A kind of easy unmanned plane mooring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721001765.2U CN207089683U (en) | 2017-08-11 | 2017-08-11 | A kind of easy unmanned plane mooring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207089683U true CN207089683U (en) | 2018-03-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721001765.2U Active CN207089683U (en) | 2017-08-11 | 2017-08-11 | A kind of easy unmanned plane mooring device |
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| CN (1) | CN207089683U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945384A (en) * | 2018-07-02 | 2018-12-07 | 合肥瀚翔智能科技有限公司 | One kind being tethered at unmanned plane photoelectricity Tethered force-bearing connector |
| CN109305382A (en) * | 2018-10-17 | 2019-02-05 | 江西洪都航空工业集团有限责任公司 | Tie-down point and jacking bracket structure on a kind of aircraft |
-
2017
- 2017-08-11 CN CN201721001765.2U patent/CN207089683U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945384A (en) * | 2018-07-02 | 2018-12-07 | 合肥瀚翔智能科技有限公司 | One kind being tethered at unmanned plane photoelectricity Tethered force-bearing connector |
| CN108945384B (en) * | 2018-07-02 | 2021-05-11 | 合肥瀚翔智能科技有限公司 | Photoelectric mooring bearing connector for mooring unmanned aerial vehicle |
| CN109305382A (en) * | 2018-10-17 | 2019-02-05 | 江西洪都航空工业集团有限责任公司 | Tie-down point and jacking bracket structure on a kind of aircraft |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 312000 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee after: Shaoxing Baojing composite material Co.,Ltd. Patentee after: JINGGONG (SHAOXING) COMPOSITE TECHNOLOGY R & D CO.,LTD. Address before: 312030 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee before: JINGGONG (SHAOXING) COMPOSITE MATERIAL CO.,LTD. Patentee before: JINGGONG (SHAOXING) COMPOSITE TECHNOLOGY R & D CO.,LTD. |
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| CP03 | Change of name, title or address | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 312000 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee after: Shaoxing Baojing composite material Co.,Ltd. Patentee after: Shaoxing Baojing Composite Technology Research and Development Co.,Ltd. Address before: 312000 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee before: Shaoxing Baojing composite material Co.,Ltd. Patentee before: JINGGONG (SHAOXING) COMPOSITE TECHNOLOGY R & D CO.,LTD. |
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| CP01 | Change in the name or title of a patent holder |