CN206446786U - Support meanss - Google Patents
Support meanss Download PDFInfo
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- CN206446786U CN206446786U CN201720125997.2U CN201720125997U CN206446786U CN 206446786 U CN206446786 U CN 206446786U CN 201720125997 U CN201720125997 U CN 201720125997U CN 206446786 U CN206446786 U CN 206446786U
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- Prior art keywords
- air cushion
- holding unit
- inflation
- cushion layer
- tethered
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Abstract
Disclose a kind of support meanss, the afterbody of aerostatics is tethered at for supporting, including inflation holding unit and multiple air cushion layers, the multiple air cushion layer is cascading, the inflation holding unit is located at the top of the multiple air cushion layer, the inflation holding unit be used to hold up and support it is described be tethered at aerostatics, the multiple air cushion layer is used for the height that the inflation holding unit is adjusted by respective inflation/deflation.The support meanss that the utility model is provided, because inflation holding unit is provided with holding unit, the stable support to being tethered at aerostatics main gasbag can be realized, so that to the easy to adjust quick of afterbody bracing cable length in follow-up assembling process, relative to existing mode, potential safety hazard is greatly reduced, and reduces construction cost.Also, the Height Adjustable of holding unit is inflated, the dirigible of different model specification is can adapt to.
Description
Technical field
The utility model is related to aerostatics technical field, more particularly, to a kind of support meanss.
Background technology
Dirigible as a kind of floating platform, its basic functional principle be using the filling gas in balloon utricule in atmosphere
Produce buoyancy and carry payload, and realize that skyborne long-time is resident by the towing of tether cable.
The soft structure of dirigible is divided into the big structure of main gasbag, balloonet, radome fairing and empennage etc. four, and wherein empennage was being left a blank
Play a part of adjustment and stabilising direction in journey.Between empennage, between empennage, main gasbag, it is attached using bracing cable, single
The load transmission that individual empennage is subject to is distributed on other empennages and main gasbag, reduces the local stress of empennage, it is to avoid utricule is made
Into damage.So, the length of tail bracing wires has to pass through regulation, makes each bracing cable all stress moderate, can conduct well
Load, is unable to stress and crosses havoc utricule again.At present, during tail bracing wires regulation, using 2 cranes and cord main gasbag
Sling, empennage position there are enough inflated spatials to plentiful, reach the state that lift-off is left a blank when using.But, use crane
Certain potential safety hazard (it is possible that the born damaged consequence of dirigible) can be there is with cord, and financial cost can be increased.
Utility model content
In view of this, the purpose of this utility model is that provide a kind of can realize supports to the stable of dirigible main gasbag,
Potential safety hazard is greatly reduced, and reduces the support meanss of construction cost.
A kind of support meanss are provided according to the utility model, the afterbody of aerostatics is tethered at for supporting, including inflation is held up
Portion and multiple air cushion layers, the multiple air cushion layer are cascading, and the inflation holding unit is located at the multiple air cushion layer
Top, the inflation holding unit be used to hold up and support it is described be tethered at aerostatics, the multiple air cushion layer is used for by respective
Inflation/deflation come adjust it is described inflation holding unit height.
Preferably, the inflation holding unit includes inflation main body, and recessed downwards from the upper table of the inflation main body
Groove profile portion, the inflation holding unit, which is held up, described to be tethered at aerostatics and the aerostatics that is tethered at is located at the upper of the groove profile portion
Side.
Preferably, the groove profile portion includes one close to first semicircular part for being tethered at aerostatics afterbody and away from described
The second semicircular part of aerostatics afterbody is tethered at, and the radius of first semicircular part is less than second semicircular part, just
In the afterbody that aerostatics is tethered at described in support.
Preferably, the groove profile portion includes connecting the first of first semicircular part and second semicircular part respectively
Oblique line portion and the second oblique line portion, the distance between first oblique line portion and the second oblique line portion are being tethered at aerostatics tail close to described
The position in portion is nearest.
Preferably, the inflation holding unit is provided with the first gas tube, and first gas tube is used to hold up the inflation
Inflate in portion；The second gas tube is respectively equipped with multiple air cushion layers, second gas tube is used to enter each air cushion layer
Row inflation/deflation is to adjust the height of the support meanss.
Preferably, the multiple air cushion layer is that partition wall is provided between integral type structure, the adjacent air cushion layer, is used for
Each air cushion layer is separated into single cavity.
Preferably, it is split-type structural between the multiple air cushion layer, it is detachably connected between each described air cushion layer.
Preferably, connected between each described air cushion layer through frenulum bondage or VELCRO adhesion.
Preferably, the inflation holding unit and the air cushion layer are identical with the utricule material for being tethered at aerostatics.
Preferably, the number of plies of the air cushion layer is 4-6 layers, and the thickness of each layer is respectively 0.8-1.2m.
The support meanss that the utility model is provided, because inflation holding unit is provided with holding unit, can be realized to dirigible master
The stable support of air bag so as to the easy to adjust quick of afterbody bracing cable length in follow-up assembling process, relative to existing side
Formula, greatly reduces potential safety hazard, and reduce construction cost.Also, the Height Adjustable of holding unit is inflated, be can adapt to not
The dirigible of same model specification.
Brief description of the drawings
By description referring to the drawings to the utility model embodiment, of the present utility model above-mentioned and other mesh
, feature and advantage will be apparent from.
Fig. 1 shows the structural representation of the support meanss according to the utility model embodiment.
Fig. 2 shows the front view of the support meanss according to the utility model embodiment.
Fig. 3 shows the top view of the support meanss according to the utility model embodiment.
Fig. 4 shows the application state schematic diagram according to the support meanss of the utility model embodiment.
In figure：First gas tube 11, groove profile portion 12, the first semicircular part 121, the second semicircular part 122, the first oblique line portion
123rd, the second oblique line portion 124, inflation main body 13, air cushion layer 2, the second gas tube 21, next door 20, main gasbag 3, afterbody 4, support dress
Put 100.
Embodiment
Various embodiments of the present utility model are more fully described hereinafter with reference to accompanying drawing.In various figures, identical
Element is represented using same or similar reference.For the sake of clarity, the various pieces in accompanying drawing are not drawn to paint
System.
As Figure 1-4, the support meanss that the utility model is provided, for carrying out bracing wire in the empennage to being tethered at aerostatics
Or during bracing cable, the afterbody 4 for being tethered at aerostatics is held up, play a part of holding up support and protect.The support meanss include inflation and held in the palm
Portion and multiple air cushion layers 2 are played, multiple air cushion layers 2 are cascading, inflation holding unit is located at the top of multiple air cushion layers 2, fills
Gas holding unit is used to hold up and support to be tethered at aerostatics, and multiple air cushion layers 2 are used to adjust inflation support by respective inflation/deflation
The height in the portion of rising.
Inflating holding unit includes inflation main body 13, and from the upper table of inflation main body 13 recessed groove profile portion 12 downwards, fills
Gas holding unit is tethered at aerostatics for picking-up, and makes to be tethered at the top that aerostatics is located at groove profile portion 12.Wherein, groove profile portion 12 includes
One close to the first semicircular part 121 for being tethered at aerostatics afterbody 4 and away from the second semicircular part 122 for being tethered at aerostatics afterbody 4,
And first semicircular part 121 radius be less than the second semicircular part 122 radius, be easy to support the afterbody 4 for being tethered at aerostatics.Groove
Type portion 12 includes connecting the first semicircular part 121 and the first oblique line portion 123 of the second semicircular part 122 and the second oblique line respectively
Portion 124, the distance between the first oblique line portion 123 and the second oblique line portion 124 are nearest in the close position for being tethered at aerostatics afterbody 4,
The size for being tethered at aerostatics afterbody is less than the size on head, and the structure of the similar taper in groove profile portion 12 is more suitable for being tethered at aerostatics tail
The excellent support in portion 4.
Multiple air cushion layers 2 are integral type structure, and partition wall 20 is provided between adjacent air cushion layer 2, for by each air cushion
Layer 2 is separated into single cavity.It is alternatively between split-type structural, each air cushion layer 2 and removably connects between multiple air cushion layers 2
Connect.It can be connected between each air cushion layer 2 by frenulum bondage or VELCRO adhesion.No matter multiple air cushion layers 2 are integral type or can
Detachable, can be by carrying out inflation/deflation come the whole height of adjusting supporting device to each air cushion layer 2.
Wherein, it between inflation holding unit and multiple air cushion layers 2 can be overall structure, or dismountable split type knot
Structure.When for dismountable split-type structural, can using adhesion connection or frenulum connection by the way of realize inflation holding unit with
Connection between multiple air cushion layers 2.
In this embodiment, inflation holding unit and air cushion layer 2 are identical with the utricule material for being tethered at aerostatics.Inflate holding unit
For type inflatable soft body structure, the first gas tube 11 is which is provided with, for carrying out inflation/deflation to it.First gas tube 11, which is located at, to be filled
On the side of gas holding unit inflation main body 13, certainly, the first gas tube may also be arranged on upper surface or bottom in other embodiments
Face or other positions for inflating holding unit, can realize and carry out inflation/deflation to inflation holding unit.
Each air cushion layer 2 can be to be detachably connected between split-type structural, each air cushion layer 2.Specifically, each air cushion layer
2 can be separately machined into cystic structures by capsule skin respectively, processes and is tied up by adhesion connection or frenulum between rear each layer air cushion layer 2
The mode such as tie up to connect each air cushion layer 2 successively stratification.In this way, the separate repair to each air cushion layer 2 and protection can be facilitated
Maintenance.The second gas tube 21 is respectively equipped with the side of each air cushion layer 2, the set location of second gas tube 21 can be with
One gas tube 11 is located at the same side, in order to concentrate inflation.It is inflated through 21 pairs of corresponding air cushion layers 2 of each second gas tube
Or deflate, to adjust the height of inflation holding unit, to adapt to the dirigible of different model specification.
It is to separate between monolithic construction, adjacent air cushion layer 2 through next door 20 between multiple air cushion layers 2.Each air cushion layer
Between 2 overall layer structure is formed by the way of capsule skin is sutured or is bonded.The specific set location of second gas tube 21
Tie up identical during split-type structural between multiple air cushion layers 2.
In this embodiment, the number of plies of air cushion layer 2 is 4-6 layers, and the thickness of each layer is respectively 0.8-1.2m.For example, it is preferable to
It it is 5 layers for the quantity of air cushion layer 2, each thickness degree is respectively 1 meter.
Support meanss 100 in the application, when the empennage to being tethered at aerostatics carries out bracing wire or bracing cable, hold up afterbody
Meanwhile, the head for being tethered at aerostatics is contacted to earth, and support meanss 100 are being tethered at the center of gravity rearward position picking-up again of aerostatics, to being
Aerostatics is stayed to play a part of holding up support and protect.
Because support meanss 100 are provided with inflation holding unit, the stable branch of the main gasbag 3 to being tethered at aerostatics can be realized
Support so as to the easy to adjust quick of the bracing cable length of afterbody 4 in follow-up empennage assembling or maintenance process, relative to existing side
Formula, greatly reduces potential safety hazard, and reduce construction cost.Also, the Height Adjustable of holding unit is inflated, be can adapt to not
The dirigible of same model specification.
It should be noted that herein, such as first and second or the like relational terms are used merely to a reality
Body or operation make a distinction with another entity or operation, and not necessarily require or imply these entities or deposited between operating
In any this actual relation or order.Moreover, term " comprising ", "comprising" or its any other variant are intended to
Nonexcludability is included, so that process, method, article or equipment including a series of key elements not only will including those
Element, but also other key elements including being not expressly set out, or also include being this process, method, article or equipment
Intrinsic key element.In the absence of more restrictions, the key element limited by sentence "including a ...", it is not excluded that
Also there is other identical element in process, method, article or equipment including key element.
Finally it should be noted that：Obviously, above-described embodiment is only intended to clearly illustrate the utility model example,
And the not restriction to embodiment.For those of ordinary skill in the field, may be used also on the basis of the above description
To make other changes in different forms.There is no necessity and possibility to exhaust all the enbodiments.And thus
Among the obvious changes or variations amplified out is still in protection domain of the present utility model.
Claims (10)
1. a kind of support meanss, the afterbody of aerostatics is tethered at for supporting, it is characterised in that including inflation holding unit and multiple gas
Bed course, the multiple air cushion layer is cascading, and the inflation holding unit is located at the top of the multiple air cushion layer,
The inflation holding unit be used to hold up and support it is described be tethered at aerostatics, the multiple air cushion layer is used to fill by respective
Deflate to adjust the height of the inflation holding unit.
2. support meanss according to claim 1, it is characterised in that the inflation holding unit includes inflation main body, and certainly
The upper table of the inflation main body recessed groove profile portion downwards, the inflation holding unit, which is held up, described is tethered at aerostatics and described in making
It is tethered at the top that aerostatics is located at the groove profile portion.
3. support meanss according to claim 2, it is characterised in that the groove profile portion includes one and is tethered at floating close to described
First semicircular part of device afterbody and the second semicircular part that aerostatics afterbody is tethered at away from described in, and first semicircular part
Radius be less than the radius of second semicircular part, be easy to be tethered at the afterbody of aerostatics described in support.
4. support meanss according to claim 3, it is characterised in that the groove profile portion includes connecting described the first half respectively
The first oblique line portion and the second oblique line portion of rounded portions and second semicircular part, first oblique line portion and the second oblique line portion it
Between distance nearest close to the position for being tethered at aerostatics afterbody.
5. support meanss according to claim 1, it is characterised in that the inflation holding unit is provided with the first gas tube, institute
Stating the first gas tube is used for the inflation holding unit inflation；The second gas tube, institute are respectively equipped with multiple air cushion layers
Stating the second gas tube is used to each air cushion layer is carried out inflation/deflation to adjust the height of the support meanss.
6. support meanss according to claim 1, it is characterised in that the multiple air cushion layer is integral type structure, adjacent
The air cushion layer between be provided with partition wall, for each air cushion layer to be separated into single cavity.
7. support meanss according to claim 1, it is characterised in that be split-type structural between the multiple air cushion layer,
It is detachably connected between each described air cushion layer.
8. support meanss according to claim 7, it is characterised in that through frenulum bondage or evil spirit between each described air cushion layer
Art patch adhesion connection.
9. support meanss according to claim 1, it is characterised in that the inflation holding unit and the air cushion layer with it is described
The utricule material for being tethered at aerostatics is identical.
10. the support meanss according to claim any one of 1-9, it is characterised in that the number of plies of the air cushion layer is 4-6
Layer, the thickness of each layer is respectively 0.8-1.2m.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720125997.2U CN206446786U (en) | 2017-02-10 | 2017-02-10 | Support meanss |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720125997.2U CN206446786U (en) | 2017-02-10 | 2017-02-10 | Support meanss |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206446786U true CN206446786U (en) | 2017-08-29 |
Family
ID=59664858
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720125997.2U Active CN206446786U (en) | 2017-02-10 | 2017-02-10 | Support meanss |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206446786U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547220A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | Forming and distributing method for stratospheric airship |
-
2017
- 2017-02-10 CN CN201720125997.2U patent/CN206446786U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547220A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | Forming and distributing method for stratospheric airship |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230808 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 |