CN204998743U - It draws aerostatics of stumbling to be suitable for drawing of aerostatics to stumble and to have this - Google Patents
It draws aerostatics of stumbling to be suitable for drawing of aerostatics to stumble and to have this Download PDFInfo
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- CN204998743U CN204998743U CN201520772793.9U CN201520772793U CN204998743U CN 204998743 U CN204998743 U CN 204998743U CN 201520772793 U CN201520772793 U CN 201520772793U CN 204998743 U CN204998743 U CN 204998743U
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- aerostatics
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- folded section
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Abstract
The utility model provides a be suitable for drawing of aerostatics to stumble, including backer and load strip, the surface of the utricule of aerostatics is located to the backer, a pair of folding section is folded into to the load strip to be defined as first folding section and the folding section of second respectively, first folding section and the folding section of second all connect be fixed in the backer on, and the folding joint of first folding section and the folding section of second locates to be formed with the load strip link that can supply the rope connection to fix. Because the utility model discloses a load strip is for folding into on a pair of folding section back locates the backer, if make the rope connect in load strip link can, in view of the above, when rope tractive load strip, the load strip can be scattered in first folding section, the folding section of second with its effort that receives, the even atress of assurance load strip avoids the utricule tractive impaired to make that it stumbles to draw reaches anticipated bearing capacity, simultaneously, also borrow the setting by load strip link, be favorable to being connected between rope and the load strip. The utility model discloses still provide the aerostatics.
Description
Technical field
The utility model relates to the technical field of aerostatics, particularly relates to a kind ofly be suitable for the pulling of aerostatics and have the aerostatics of this pulling.
Background technology
Aerostatics generally refers to aircraft that proportion is lighter than air, that rely on atmospheric buoyancy force lift-off.Aerostatics generally can be divided into captive balloon and dirigible.Captive balloon does not generally have power system, relies on tether cable to be connected with wayside equipment or website; Dirigible is dynamic, can in remote control or autonomous flight under automatically controlling.To aerostatics is fixed on ground or carry gondola, fixed equipment with it it, often need arranging one can transmit the framing member with distractive load, and this framing member is referred to as pulling.
Existing pulling, it is primarily of base fabric, load bar and coupling link composition, wherein, the load bar be fixed on base fabric is provided separately, thus, need to use the larger coupling link of overall dimension just can connect load bar, and each load bar just can be made simultaneously stressed.But the weight of the coupling link that overall dimension is larger is also comparatively large, like this, easily causes the overall weight of pulling comparatively large, correspondingly, also increase the load of aerostatics utricule, easily make it occur the problem of damaging.If can the coupling link that overall dimension is less be used, the problem that part load bar cannot be stressed can be there is, so that the weight capacity of pulling declines, correspondingly, reduce the reliability of aerostatics utricule.
Therefore, be necessary to provide a kind of technological means to address the aforementioned drawbacks.
Utility model content
The purpose of this utility model is the defect overcoming prior art, there is provided a kind of pulling being suitable for aerostatics, with the pulling solving prior art because of the load that adopts the coupling link of large-size so that increase aerostatics utricule or the problem declined because of the coupling link so that its weight capacity that adopt reduced size.
The utility model is achieved in that the pulling being suitable for aerostatics, and described aerostatics comprises a utricule, and described pulling comprises:
Base fabric, the surface of described utricule is located at by described base fabric; And
Load bar, described load bar is folded into a pair folded section, and be defined as the first folded section and the second folded section respectively, described first folded section and described second folded section are all connected and fixed on described base fabric, and the folding junction of described first folded section and described second folded section is formed with the load bar coupling end that movable setting is connected and fixed for rope.
Particularly, described first folded section and described second folded section are for being symmetrically set on described base fabric.
Particularly, described pulling also comprises one in order to connect the attaching parts of described load bar coupling end and described rope, and described attaching parts comprises the first connecting portion in order to contact with described load bar coupling end and the second connecting portion in order to be connected with described rope.
Further, described first connecting portion is the cross bar portion contacted with described load bar coupling end, and described second connecting portion is a v-shaped structure.
Further, the shape of described attaching parts is axially symmetric structure, and the mid point of the axis of symmetry of described attaching parts through described cross bar portion and the tip of described v-shaped structure.
Further, described attaching parts is a coupling link.
Further, the cross section of described coupling link is equilateral polygon, and the limit number of described equilateral polygon is 2n-1, and n >=2.
Particularly, described load bar is provided with multiple, and the load bar coupling end of described multiple load bar overlaps, the first folded section of described multiple load bar and the second folded section fan-shaped array respectively.
Further, the first folded section of described multiple load bar is identical with the second folded section angulation.
Preferably, the width of the load bar coupling end that described multiple load bar is corresponding is equal setting.
The technique effect being suitable for the pulling of aerostatics of the present utility model is: because load bar of the present utility model is for being located on base fabric after being folded into a pair folded section, as long as make rope be connected to load bar coupling end, accordingly, when pulled by cable load bar, the application force that load bar can be subject to is scattered in the first folded section, the second folded section, ensure load bar uniform stressed, avoid utricule tractive impaired, and make pulling reach the weight capacity of expection; Meanwhile, also by the setting of load bar coupling end, be conducive to the connection between rope and load bar.
The utility model also provides aerostatics, comprises utricule, and also comprise the above-mentioned described pulling being suitable for aerostatics, described pulling is fixed on described utricule.Because this aerostatics has above-mentioned pulling, be both conducive to the load transmitted and disperse on aerostatics, the safe reliability of aerostatics can have been improved again.
Accompanying drawing explanation
Fig. 1 is the schematic diagram that the pulling being suitable for aerostatics of the present utility model is located at utricule;
Fig. 2 is the schematic diagram being located at base fabric after the load bar being suitable for the pulling of aerostatics of the present utility model passes coupling link;
Fig. 3 is the structural representation being suitable for the load bar of the pulling of aerostatics of the present utility model;
Fig. 4 is the structural representation being suitable for the attaching parts of the pulling of aerostatics of the present utility model.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
be suitable for the embodiment of the pulling of aerostatics:
Refer to Fig. 1 to Fig. 4, the utility model provides a kind of pulling being suitable for aerostatics, sets forth below to the embodiment that this is suitable for the pulling of aerostatics.
In the present embodiment, aerostatics can be captive balloon, also can be dirigible, and it comprises a utricule 10, anchoring facility, observing and controlling facility, power supply facilities and pulling 20, and the facility that anchors, observing and controlling facility, power supply facilities and pulling 20 are all installed on utricule 10.Wherein, this pulling 20 comprises base fabric 21 and load bar 22 forms, and is further described below to each parts of this pulling 20:
The surface of utricule 10 is located at by base fabric 21;
Load bar 22 is folded into a pair folded section, and be defined as the first folded section 221 and the second folded section 222 respectively, first folded section 221 and the second folded section 222 are all connected and fixed on base fabric 10, and the folding junction of the first folded section 221 and the second folded section 222 is formed with the load bar coupling end 223 that movable setting is connected and fixed for rope 30, the position that this load bar coupling end 223 indicates for A in Fig. 3; In addition, because this load bar coupling end 223 is flexible material, it can strut one and supply rope 30 to penetrate the collar extension of tie-down, and visible, this load bar coupling end 223 is equivalent to be a cyclic structure.
Because the load bar 22 of the present embodiment is for being located on base fabric 10 after being folded into a pair folded section, as long as make rope 30 be connected to load bar coupling end 223, accordingly, when rope 30 tractive load bar 22, the application force that load bar 22 can be subject to is scattered in the first folded section 221, second folded section 222, ensure load bar 22 uniform stressed, avoid utricule 10 tractive impaired, and make pulling 20 reach the weight capacity of expection; Meanwhile, also by the setting of load bar coupling end 223, the connection between rope 30 and load bar 22 is conducive to.
Refer to Fig. 2 and Fig. 3, for the ease of being folded with load bar 22, and after making load bar 22 stressed by power stepless action on utricule 10, the first folded section 221 and the second folded section 222 are for being symmetrically set on base fabric 10.
Refer to Fig. 1 and Fig. 2, the preferred implementation of the load bar 22 in the present embodiment is that load bar 22 is provided with multiple, be preferably three, certainly, the load bar 22 of greater number also can be set according to actual conditions, and these embodiments also belong to the protection category of the present embodiment; And the load bar coupling end 223 of three load bars 22 overlaps, the first folded section 221 of three load bars 22 and the second folded section 222 fan-shaped array respectively, bears application force to make these three load bars 22 at diverse location.Preferably, the first folded section 221 of three load bars 22 is identical with the second folded section 222 angulation.
Side by side, the width of three load bar coupling ends 223 of three load bar 22 correspondences is equal setting, during to ensure the folding load bar coupling end 223 formed of these three load bars 22 by pulled by cable, this rope can by its application force stepless action on three load bars 22.
Refer to Fig. 4, and composition graphs 1 and Fig. 2, as the preferred implementation of the present embodiment, pulling 20 also comprises one in order to connect the attaching parts 23 of load bar coupling end 223 and both ropes 30, attaching parts 23 comprises the first connecting portion 231 in order to contact with load bar coupling end 223 and the second connecting portion 232 in order to be connected with rope 30, wherein, the setting of attaching parts 23, be conducive to the tractive of rope 30 pairs of load bars 22, and effectively can reduce the problem easily load bar 22 being caused to damage when rope 30 directly contacts load bar 22; In addition, the setting of the first connecting portion 231, second connecting portion 232, is conducive to fixing the location of load bar coupling end 223, rope 30.
Particularly, first connecting portion 231 is the cross bar portion contacted with load bar coupling end 223, so that folding for three the load bars 22 load bar coupling end 223 formed is located fixing, and avoid impacting the folding load bar coupling end 223 formed of these three load bars 22; And the second connecting portion 232 is a v-shaped structure, be beneficial to the tie-down of rope 30.
During in order to make rope 30 by attaching parts 23 tractive load bar coupling end 223, can by its application force stepless action in load bar coupling end 223, attaching parts 23 is a zhou duicheng tuxing structure, and the mid point of its axis of symmetry through cross bar portion and the tip of v-shaped structure.Side by side, the processing and manufacturing to attaching parts 23 is also convenient to.
Refer to Fig. 4, the preferred implementation of the attaching parts 23 in the present embodiment is, attaching parts 23 is a coupling link, to simplify the concrete structure of attaching parts 23, is conducive to production and processing, and reduces productive costs.
Further, coupling link is polygon, and polygonal limit number is 2n-1, and n >=2, preferably, n=2, namely polygonized structure is triangular structure, simplifies the structure of coupling link with this further; Certainly, also according to actual conditions, the coupling link of pentagonal configuration, heptagon structure etc. can be adopted.Preferably, the shape of coupling link is equilateral polygon.
Refer to Fig. 2, the preferred implementation of the base fabric 21 in the present embodiment is, base fabric 21 is the geometric form structure of rule, so that production and processing, certainly, also base fabric 21 can be processed as irregular geometric form structure.Preferably, base fabric 21 is sector structure, so that the setting of load bar 22.
the embodiment of aerostatics:
Refer to Fig. 1 to Fig. 3, the utility model provides a kind of aerostatics, sets forth below to the embodiment of this aerostatics.
The aerostatics of the present embodiment can be captive balloon, also can be dirigible, and it comprises a utricule 10, anchoring facility, observing and controlling facility, power supply facilities and above-mentioned pulling 20, and the facility that anchors, observing and controlling facility, power supply facilities and pulling 20 are all installed on utricule 10.Because this aerostatics has above-mentioned pulling 20, be both conducive to the load transmitted and disperse on aerostatics, the safe reliability of aerostatics can have been improved again.
The foregoing is only the utility model preferred embodiment; its structure is not limited to the above-mentioned shape enumerated; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (11)
1. be suitable for the pulling of aerostatics, described aerostatics comprises a utricule, it is characterized in that, described pulling comprises:
Base fabric, the surface of described utricule is located at by described base fabric; And
Load bar, described load bar is folded into a pair folded section, and be defined as the first folded section and the second folded section respectively, described first folded section and described second folded section are all connected and fixed on described base fabric, and the folding junction of described first folded section and described second folded section is formed with the load bar coupling end that movable setting is connected and fixed for rope.
2. be suitable for the pulling of aerostatics as claimed in claim 1, it is characterized in that: described first folded section and described second folded section are for being symmetrically set on described base fabric.
3. be suitable for the pulling of aerostatics as claimed in claim 1, it is characterized in that: also comprise one in order to connect the attaching parts of described load bar coupling end and described rope, described attaching parts comprises the first connecting portion in order to contact with described load bar coupling end and the second connecting portion in order to be connected with described rope.
4. be suitable for the pulling of aerostatics as claimed in claim 3, it is characterized in that: described first connecting portion is the cross bar portion contacted with described load bar coupling end, and described second connecting portion is a v-shaped structure.
5. be suitable for the pulling of aerostatics as claimed in claim 4, it is characterized in that: the shape of described attaching parts is axially symmetric structure, and the mid point of the axis of symmetry of described attaching parts through described cross bar portion and the tip of described v-shaped structure.
6. be suitable for the pulling of aerostatics as claimed in claim 5, it is characterized in that: described attaching parts is a coupling link.
7. be suitable for the pulling of aerostatics as claimed in claim 6, it is characterized in that: described coupling link is polygon, described polygonal limit number is 2n-1, and n >=2.
8. the pulling being suitable for aerostatics as described in any one of claim 1-7, it is characterized in that: described load bar is provided with multiple, and the load bar coupling end of described multiple load bar overlaps, the first folded section of described multiple load bar and the second folded section fan-shaped array respectively.
9. be suitable for the pulling of aerostatics as claimed in claim 8, it is characterized in that: the first folded section of described multiple load bar is identical with the second folded section angulation.
10. be suitable for the pulling of aerostatics as claimed in claim 8, it is characterized in that: the width of the load bar coupling end that described multiple load bar is corresponding is equal setting.
11. aerostatics, comprise utricule, it is characterized in that: also comprise the pulling being suitable for aerostatics as described in any one of claim 1-10, described pulling is fixed on described utricule.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520772793.9U CN204998743U (en) | 2015-09-29 | 2015-09-29 | It draws aerostatics of stumbling to be suitable for drawing of aerostatics to stumble and to have this |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520772793.9U CN204998743U (en) | 2015-09-29 | 2015-09-29 | It draws aerostatics of stumbling to be suitable for drawing of aerostatics to stumble and to have this |
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| Publication Number | Publication Date |
|---|---|
| CN204998743U true CN204998743U (en) | 2016-01-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520772793.9U Active CN204998743U (en) | 2015-09-29 | 2015-09-29 | It draws aerostatics of stumbling to be suitable for drawing of aerostatics to stumble and to have this |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667753A (en) * | 2016-03-03 | 2016-06-15 | 上海交通大学 | Multi-point bearing loop for aerostat |
| CN106055833A (en) * | 2016-06-22 | 2016-10-26 | 中国电子科技集团公司第三十八研究所 | Flexible simulation based design method for tongs connecting assembly of aerostat |
| CN106741806A (en) * | 2016-12-28 | 2017-05-31 | 东莞前沿技术研究院 | Tab and the aerostatics using tab |
| CN107010193A (en) * | 2017-03-24 | 2017-08-04 | 中国电子科技集团公司第三十八研究所 | A kind of nose cone device being tethered at for aerostatics head with anticollision |
| CN109250060A (en) * | 2017-07-12 | 2019-01-22 | 东莞前沿技术研究院 | Pulling and aerostatics with it |
| WO2019019665A1 (en) * | 2017-07-27 | 2019-01-31 | 深圳光启空间技术有限公司 | Force-bearing puller structure and aerostat |
| CN109507020A (en) * | 2017-09-20 | 2019-03-22 | 东莞前沿技术研究院 | Testpieces strength testing device and testpieces strength test method |
-
2015
- 2015-09-29 CN CN201520772793.9U patent/CN204998743U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667753A (en) * | 2016-03-03 | 2016-06-15 | 上海交通大学 | Multi-point bearing loop for aerostat |
| CN106055833A (en) * | 2016-06-22 | 2016-10-26 | 中国电子科技集团公司第三十八研究所 | Flexible simulation based design method for tongs connecting assembly of aerostat |
| CN106741806A (en) * | 2016-12-28 | 2017-05-31 | 东莞前沿技术研究院 | Tab and the aerostatics using tab |
| CN107010193A (en) * | 2017-03-24 | 2017-08-04 | 中国电子科技集团公司第三十八研究所 | A kind of nose cone device being tethered at for aerostatics head with anticollision |
| CN107010193B (en) * | 2017-03-24 | 2019-09-10 | 中国电子科技集团公司第三十八研究所 | A kind of nose cone device being tethered at for aerostatics head with anticollision |
| CN109250060A (en) * | 2017-07-12 | 2019-01-22 | 东莞前沿技术研究院 | Pulling and aerostatics with it |
| WO2019019665A1 (en) * | 2017-07-27 | 2019-01-31 | 深圳光启空间技术有限公司 | Force-bearing puller structure and aerostat |
| CN109507020A (en) * | 2017-09-20 | 2019-03-22 | 东莞前沿技术研究院 | Testpieces strength testing device and testpieces strength test method |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230625 Address after: Room 501, Building D2, Songshan Lake International Innovation and Entrepreneurship Community, Songshan Lake High tech Industrial Development Zone, Dongguan City, Guangdong Province, 523000 Patentee after: Dongguan Dongguan Institute of Science and Technology Innovation Address before: 523000 Room 502, 5th floor, building 1, innovation and Technology Park, Songshanhu high tech Industrial Development Zone, Dongguan City, Guangdong Province Patentee before: DONGGUAN FRONTIER TECHNOLOGY INSTITUTE Patentee before: SHENZHEN KUANG-CHI SPACE TECH. Co.,Ltd. |