CN109436282A - The pulling component of aerostatics - Google Patents
The pulling component of aerostatics Download PDFInfo
- Publication number
- CN109436282A CN109436282A CN201811091555.6A CN201811091555A CN109436282A CN 109436282 A CN109436282 A CN 109436282A CN 201811091555 A CN201811091555 A CN 201811091555A CN 109436282 A CN109436282 A CN 109436282A
- Authority
- CN
- China
- Prior art keywords
- pulling
- lining cloth
- cloth
- aerostatics
- component
- 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.)
- Withdrawn
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Details Of Garments (AREA)
Abstract
The invention discloses a kind of pulling components of aerostatics.Wherein, which includes: load component, lining cloth, bottom liner cloth and reinforces lining cloth.Wherein: load component includes plane domain and pulling region；Plane domain is arranged between lining cloth and bottom liner cloth；Bottom liner cloth is fixed on aerostatics；Reinforce lining cloth to be fixed on lining cloth；Pulling region, which is extend out to, to be reinforced except lining cloth.The embodiment of the present invention is not only simple in structure, and intensity is very high, is also limited without use direction.
Description
Technical field
The present invention relates to the technical fields of aerostatics, more particularly, to a kind of pulling component of aerostatics.
Background technique
With the fast development of aeronautical technology, aerostatics is widely applied.Pulling, which is that aerostatics product is main, holds
Power component is indispensable a part.
However, being subject to certain restrictions in present conventional use process.Fan-shaped pulling is by prominent wind load or along load
When opposite direction stress, fan-shaped pulling is easier to pulling occur and utricule removes situation.
In order to solve the problems, such as that pulling and utricule are removed, now attempt to increase the lining cloth reversely torn in fan-shaped pulling.
Although lining cloth increases the reversed tearing strength of pulling to a certain extent, pulling is still limited by use direction on the whole.
Though round pulling is influenced smaller by direction, because intensity is lower, can only use as complementary pulling.
Summary of the invention
In consideration of it, the present invention provides a kind of aerostatics in order to solve at least one technical problem in the prior art
Pulling component.Wherein, which includes:
Load component, lining cloth, bottom liner cloth and reinforcement lining cloth, in which:
Load component includes plane domain and pulling region；
Plane domain is arranged between lining cloth and bottom liner cloth；
Bottom liner cloth is fixed on aerostatics；
Reinforce lining cloth to be fixed on lining cloth；
Pulling region, which is extend out to, to be reinforced except lining cloth.
The embodiment of the present invention is not only simple in structure, and intensity is very high, is also limited without use direction.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, will make below to required in the embodiment of the present invention
Attached drawing is briefly described, it is therefore apparent that drawings described below is only some embodiments of the present invention, for this
For the technical staff in field, without creative efforts, it can also be obtained according to these attached drawings other attached
Figure.
Fig. 1 is the structural schematic diagram of the pulling component of the aerostatics of one embodiment of the invention；
Fig. 2 is the structural schematic diagram of the load component of one embodiment of the invention.
Wherein: load component -1, bottom liner cloth -3, reinforces lining cloth -4 at lining cloth -2.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described.Obviously, described embodiment is
A part of the embodiment of the present invention, rather than whole embodiments.Based on the embodiments of the present invention, those skilled in the art
Without making creative work, every other embodiment obtained, shall fall within the protection scope of the present invention.
The feature and illustrative examples of various aspects of the invention is described more fully below.In following detailed description
In, many details are proposed, in order to provide complete understanding of the present invention.But come for those skilled in the art
It says it will be apparent that the present invention can be implemented in the case where not needing some details in these details.Below to reality
The description of example is applied just for the sake of providing and better understanding to of the invention by showing example of the invention.The present invention is never
It is limited to any specific setting and method set forth below, but covering finishes under the premise of without departing from the spirit of the present invention
Structure, method, any improvement of device, substitutions and modifications.In the the accompanying drawings and the following description, well known structure and skill is not shown
Art is unnecessary fuzzy to avoid causing to the present invention.
It should be noted that in the absence of conflict, the feature in the embodiment of the present invention and embodiment can be tied mutually
It closes, each embodiment mutually can be referred to and be quoted.The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
Fig. 1 is the structural schematic diagram of the pulling component of the aerostatics of one embodiment of the invention.
As shown in Figure 1, the pulling component of aerostatics may include: load component 1, lining cloth 2, bottom liner cloth 3 and reinforce lining cloth
4.Wherein, load component 1 may include plane domain and pulling region；Plane domain is arranged between lining cloth 2 and bottom liner cloth 3；
Bottom liner cloth 3 is fixed on aerostatics；Reinforce lining cloth 4 to be fixed on lining cloth 2；Pulling region, which is extend out to, to be reinforced except lining cloth 4.
Fig. 2 is the structural schematic diagram of the load component of one embodiment of the invention.
As shown in Fig. 2, load component 1 may include plane domain and pulling region.
In some embodiments, by the effect of pulling, pulling may be selected traction pulling, be tethered at pulling, auxiliary pulling etc..Its
It can be used for being tethered at, hanging the fields such as load for aerostatics product.According to the shape of pulling, fan-shaped pulling and round drawing can be divided into
Loop etc..
In some embodiments, the fixed form between load component 1, lining cloth 2 and bottom liner cloth 3 can fix to be glued.
In some embodiments, reinforce being hot synthetic type between lining cloth 4 and lining cloth 2.
In some embodiments, the processing method of load component 1 is the processing method based on stereo weaving technology.
In some embodiments, 1 plane domain of load component is clipped between lining cloth 2 and bottom liner cloth 3, blend compounds connect agent will
It, which is glued, fixes, and will reinforce lining cloth 4 and 2 hot synthetic type of lining cloth with heat seal equipment.
By many experiments, the results show that the pulling component of aerostatics is not only simple in structure, and intensity is very high, also
No use direction limitation.Currently, the pulling has been applied on various types of aerial bicycles and captive balloon.
Finally it should be noted that: the above embodiments are merely illustrative of the technical solutions of the present invention, but protection of the invention
Range is not limited thereto, and anyone skilled in the art in the technical scope disclosed by the present invention, can be thought easily
It is modified or replaceed to various equivalent, these, which are modified or replaceed, should all be included within the scope of the present invention.
Claims (4)
1. a kind of pulling component of aerostatics characterized by comprising
Load component (1), lining cloth (2), bottom liner cloth (3) and reinforcement lining cloth (4), in which:
The load component (1) includes plane domain and pulling region；
The plane domain is arranged between the lining cloth (2) and the bottom liner cloth (3)；
The bottom liner cloth (3) is fixed on aerostatics；
The reinforcement lining cloth (4) is fixed on the lining cloth (2)；
The pulling region is extend out to except the reinforcement lining cloth (4).
2. the pulling component of aerostatics according to claim 1, which is characterized in that wherein:
Fixed form between the load component (1), the lining cloth (2) and the bottom liner cloth (3) is to be glued to fix.
3. the pulling component of aerostatics according to claim 1, which is characterized in that wherein:
It is hot synthetic type between the reinforcement lining cloth (4) and the lining cloth (2).
4. the pulling component of aerostatics according to any one of claim 1-3, which is characterized in that wherein:
The processing method of the load component (1) is the processing method based on stereo weaving technology.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811091555.6A CN109436282A (en) | 2018-09-18 | 2018-09-18 | The pulling component of aerostatics |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811091555.6A CN109436282A (en) | 2018-09-18 | 2018-09-18 | The pulling component of aerostatics |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109436282A true CN109436282A (en) | 2019-03-08 |
Family
ID=65533077
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811091555.6A Withdrawn CN109436282A (en) | 2018-09-18 | 2018-09-18 | The pulling component of aerostatics |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109436282A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201350971Y (en) * | 2008-12-27 | 2009-11-25 | 中国特种飞行器研究所 | Tethered balloon nose cone stay device |
| US20140021288A1 (en) * | 2012-07-20 | 2014-01-23 | Andrew Charles Elson | Unmanned aerial vehicle and method of launching |
| CN205952275U (en) * | 2016-08-05 | 2017-02-15 | 东莞前沿技术研究院 | Multidirectional load draws tong " pan " structure and aerostatics |
| CN206984293U (en) * | 2017-07-12 | 2018-02-09 | 东莞前沿技术研究院 | Tab and there is its aerostatics |
| CN109866911A (en) * | 2017-12-04 | 2019-06-11 | 中国特种飞行器研究所 | A kind of aerostatics butterfly junction structure |
-
2018
- 2018-09-18 CN CN201811091555.6A patent/CN109436282A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201350971Y (en) * | 2008-12-27 | 2009-11-25 | 中国特种飞行器研究所 | Tethered balloon nose cone stay device |
| US20140021288A1 (en) * | 2012-07-20 | 2014-01-23 | Andrew Charles Elson | Unmanned aerial vehicle and method of launching |
| CN205952275U (en) * | 2016-08-05 | 2017-02-15 | 东莞前沿技术研究院 | Multidirectional load draws tong " pan " structure and aerostatics |
| CN206984293U (en) * | 2017-07-12 | 2018-02-09 | 东莞前沿技术研究院 | Tab and there is its aerostatics |
| CN109866911A (en) * | 2017-12-04 | 2019-06-11 | 中国特种飞行器研究所 | A kind of aerostatics butterfly junction structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190308 |