CN206087830U - Can remain horizontally aircraft carrier throughout - Google Patents
Can remain horizontally aircraft carrier throughout Download PDFInfo
- Publication number
- CN206087830U CN206087830U CN201620725723.2U CN201620725723U CN206087830U CN 206087830 U CN206087830 U CN 206087830U CN 201620725723 U CN201620725723 U CN 201620725723U CN 206087830 U CN206087830 U CN 206087830U
- Authority
- CN
- China
- Prior art keywords
- link
- luggage carrier
- chute
- spherical
- spring
- 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
Abstract
The utility model discloses a can remain horizontally aircraft carrier throughout, including mounting panel, link, carrier and supporting legs, the mounting panel is provided with installation screw and spliced pole, the spliced pole sets up in the mounting panel below, is provided with spherical slider, the shape of link is the cross, is provided with spherical spout, spring, spacing hole and transfers knothole, spherical spout setting is at the link top, spacing hole sets up to two, transfer knothole to set up to two, the carrier sets up in the link below, is provided with the spacer pin and adjusts the pole, it has two to adjust the pole, sets up at carrier left end and right -hand member respectively, inserts in transferring knothole, is provided with screw thread and adjusting nut, the supporting legs has four, sets up respectively in carrier bottom four corners, is provided with spout, spring and support column, the utility model relates to a rationally, convenient to use is fit for transporting the goods that some needs keep the level to can press from both sides tight goods, need not bind again.
Description
Technical field
The utility model is related to a kind of aircraft devices, specifically a kind of to remain horizontal aircraft luggage carrier.
Background technology
With the continuous progress of science and technology, also more extensively, technology is also more ripe for the utilization of aircraft；Both at home and abroad
There is manufacturer to begin to use unmanned plane to transport express delivery；But existing some aircraft article carrying platform placing articles are not very convenient, subtract
Shake effect is also preferable to the greatest extent, is especially transporting more inconvenient when some need the goods of holding level.
Utility model content
The purpose of this utility model is that offer is a kind of can remain horizontal aircraft luggage carrier, to solve the above-mentioned back of the body
The problem proposed in scape technology.
For achieving the above object, the utility model provides following technical scheme：
It is a kind of to remain horizontal aircraft luggage carrier, including installing plate, link, luggage carrier and support feet；Institute
State installing plate and be provided with installation screw and connecting pole；The installation screw is set to four, is distributed in installing plate corner；The company
Connect post and be arranged on installing plate lower section, be provided with spherical sliding block；The spherical sliding block is arranged on connecting pole lower section；The link
Cross is shaped as, spherical chute, spring, spacing hole and adjustment hole is provided with；The spherical chute is arranged on link top；
The spring is set to four, is separately positioned on around spherical chute four positions all around；The spacing hole is set to two
It is individual, it is separately positioned on the top and bottom of link；The adjustment hole is set to two, is separately positioned on link left end with the right side
End；The luggage carrier is arranged on link lower section, is provided with spacer pin and adjusting rod；The spacer pin has two, is respectively provided with
In luggage carrier top and bottom, it is inserted in the spacing hole of link；The adjusting rod has two, is separately positioned on luggage carrier left end
With right-hand member, it is inserted in adjustment hole, is provided with screw thread and adjusting nut；The screw thread is arranged on adjusting rod upper end；The regulation spiral shell
Mother set is in adjusting rod upper end；The support feet has four, is separately positioned on luggage carrier bottom corner, be provided with chute, spring and
Support column；The chute is arranged on support foot bottom；The support column is arranged in chute, is connected with chute top by spring
Connect.
As further program of the utility model：The luggage carrier middle setting has annulus.
As the utility model further scheme：The support column bottom is provided with slipmat.
Compared with prior art, the beneficial effects of the utility model are：
Spherical chute shape of the present utility model carves conjunction with spherical sliding block shape, can be enclosed within each orientation on spherical sliding block and slide
It is dynamic, make link be in horizontality all the time, it is to avoid to cause to transport goods with rocking together because of rocking for aircraft, transport
Send safer；The spring can play support and cushioning effect, prevent aircraft excessive in landing rear-inclined；The regulation spiral shell
Female load space that can pass through rotation adjustment luggage carrier, adapts to different size of goods, and directly presss from both sides goods after tightening
Tightly, without being bundled again；The annulus can increase the contact area with goods bottom surface, make the more stable of goods placement.
Description of the drawings
Fig. 1 is the structural representation of the aircraft luggage carrier that can remain horizontal.
Fig. 2 is the structural representation that can remain luggage carrier in horizontal aircraft luggage carrier.
Fig. 3 is the structural representation that can remain support feet in horizontal aircraft luggage carrier.
In figure：1- support feets, 2- luggage carriers, 3- adjusting rods, 4- screw threads, 5- adjustment holes, 6- adjusting nuts, 7- installs spiral shell
Hole, 8- installing plates, 9- connecting poles, 10- springs, 11- links, 12- spherical sliding blocks, the spherical chutes of 13-, 14- spacing holes, 15-
Spacer pin, 16- annulus, 17- slipmat, 18- support columns, 19- chutes.
Specific embodiment
The technical scheme of this patent is described in more detail with reference to specific embodiment.
Fig. 1-3 are referred to, it is a kind of to remain horizontal aircraft luggage carrier, including installing plate 8, link 11, load
Rack 2 and support feet 1；The installing plate 8 is provided with installation screw 7 and connecting pole 9；The installation screw 7 is set to four, point
Cloth can be firmly installed in installing plate 8 on aircraft in 8 four jiaos of installing plate, it is ensured that transport the stability of process；The connection
Post 9 is arranged on the lower section of installing plate 8, is provided with spherical sliding block 12；The spherical sliding block 12 is arranged on the lower section of connecting pole 9；The company
Connect frame 11 is shaped as cross, is provided with spherical chute 13, spring 10, spacing hole 14 and adjustment hole 5；The spherical chute 13
The top of link 11 is arranged on, shape carves conjunction with the shape of spherical sliding block 12, each orientation on spherical sliding block 12 can be enclosed within and slided, made
Link 11 is in all the time horizontality, it is to avoid causes to transport goods with rocking together because of rocking for aircraft, transports
It is safer；The spring 10 is set to four, is separately positioned on around spherical chute 13 four positions all around, can play
Support and cushioning effect, prevent aircraft excessive in landing rear-inclined；The spacing hole 14 is set to two, the company of being separately positioned on
Connect the top and bottom of frame 11；The adjustment hole 5 is set to two, is separately positioned on the left end of link 11 and right-hand member；The load
Rack 2 is arranged on the lower section of link 11, is provided with spacer pin 15, adjusting rod 3 and annulus 16；The spacer pin 15 has two, point
The top and bottom of luggage carrier 2 are not arranged on, are inserted in the spacing hole 14 of link 11, play position-limiting action, it is ensured that luggage carrier 2 and company
Connect frame 11 and be in parastate all the time；The adjusting rod 3 has two, is separately positioned on the left end of luggage carrier 2 and right-hand member, is inserted in regulation
In hole 5, screw thread 4 and adjusting nut 6 are provided with；The screw thread 4 is arranged on the upper end of adjusting rod 3；The adjusting nut 6 is enclosed within regulation
The upper end of bar 3, can pass through the load space of rotation adjustment luggage carrier 2, adapt to different size of goods, and directly will after tightening
Goods clamping, without being bundled again；The annulus 16 is arranged in the middle of luggage carrier 2, can increase the contact surface with goods bottom surface
Product, makes the more stable of goods placement；The support feet 1 has four, is separately positioned on the bottom corner of luggage carrier 2, is provided with cunning
Groove 19, spring 10 and support column 18；The chute 19 is arranged on the bottom of support feet 1；The support column 18 is arranged in chute 19,
It is connected with the top of chute 19 by spring 10, and is provided with slipmat 17；The spring 10 makes support feet 1 have good damping
Property, reduce impact during landing；The slipmat 17 is arranged on the bottom of support column 18, with good anti-skidding effect.
The better embodiment of this patent is explained in detail above, but this patent is not limited to above-mentioned embodiment party
Formula, in the ken that one skilled in the relevant art possesses, can be with the premise of without departing from this patent objective
Make a variety of changes.
Claims (3)
1. it is a kind of to remain horizontal aircraft luggage carrier, including installing plate, link, luggage carrier and support feet；It is special
Levy and be, the installing plate is provided with installation screw and connecting pole；The installation screw is set to four, is distributed in installing plate four
Angle；The connecting pole is arranged on installing plate lower section, is provided with spherical sliding block；The spherical sliding block is arranged on connecting pole lower section；Institute
That states link is shaped as cross, is provided with spherical chute, spring, spacing hole and adjustment hole；The spherical chute is arranged on
Link top；The spring is set to four, is separately positioned on around spherical chute four positions all around；It is described spacing
Hole is set to two, is separately positioned on the top and bottom of link；The adjustment hole is set to two, is separately positioned on connection
Frame left end and right-hand member；The luggage carrier is arranged on link lower section, is provided with spacer pin and adjusting rod；The spacer pin has two
Root, is separately positioned on luggage carrier top and bottom, is inserted in the spacing hole of link；The adjusting rod has two, is respectively provided with
In luggage carrier left end and right-hand member, it is inserted in adjustment hole, is provided with screw thread and adjusting nut；The screw thread is arranged on adjusting rod
End；The adjusting nut is enclosed within adjusting rod upper end；The support feet has four, is separately positioned on luggage carrier bottom corner, arranges
There are chute, spring and support column；The chute is arranged on support foot bottom；The support column is arranged in chute, by spring
It is connected with chute top.
2. it is according to claim 1 to remain horizontal aircraft luggage carrier, it is characterised in that in the luggage carrier
Between be provided with annulus.
3. it is according to claim 1 to remain horizontal aircraft luggage carrier, it is characterised in that the support column bottom
Portion is provided with slipmat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725723.2U CN206087830U (en) | 2016-07-11 | 2016-07-11 | Can remain horizontally aircraft carrier throughout |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725723.2U CN206087830U (en) | 2016-07-11 | 2016-07-11 | Can remain horizontally aircraft carrier throughout |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206087830U true CN206087830U (en) | 2017-04-12 |
Family
ID=58465969
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620725723.2U Expired - Fee Related CN206087830U (en) | 2016-07-11 | 2016-07-11 | Can remain horizontally aircraft carrier throughout |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206087830U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108032747A (en) * | 2017-11-29 | 2018-05-15 | 江苏迅电畅达电源科技有限公司 | A kind of portable charging pile for possessing self-leveling function |
-
2016
- 2016-07-11 CN CN201620725723.2U patent/CN206087830U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108032747A (en) * | 2017-11-29 | 2018-05-15 | 江苏迅电畅达电源科技有限公司 | A kind of portable charging pile for possessing self-leveling function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 Termination date: 20180711 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |