CN206218193U - Dirigible utricule and dirigible - Google Patents
Dirigible utricule and dirigible Download PDFInfo
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- CN206218193U CN206218193U CN201621100187.3U CN201621100187U CN206218193U CN 206218193 U CN206218193 U CN 206218193U CN 201621100187 U CN201621100187 U CN 201621100187U CN 206218193 U CN206218193 U CN 206218193U
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- main gasbag
- air chamber
- dirigible
- tail unit
- tail
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Abstract
Disclose a kind of dirigible utricule and dirigible.The captive balloon, including：Main gasbag；Empennage, is arranged at the afterbody of the main gasbag, including at least two tail units；At the structure that the tail unit and the main gasbag are combined, the air chamber of each tail unit is directly connected with the air chamber of the main gasbag.The dirigible utricule that the utility model is provided is at tail unit and the main gasbag faying face, the air chamber of tail unit is directly connected with the air chamber of main gasbag, communicating pipe that need not be outside is the connection being capable of achieving between tail unit, only needing a set of valve and Fan Equipment can maintain the sweeping appearance of all tail units, simple structure, low cost simultaneously can effectively reduce gas leakage risk point.
Description
Technical field
The utility model is related to aircraft field, more particularly, to a kind of dirigible utricule and dirigible.
Background technology
Dirigible is a kind of itself not drive, is gone up to the air by buoyancy, and precalculated position in the air is detained by tether cable
Aerostatics.Dirigible is used as aerial platform, it is necessary to have sufficiently stable property to ensure its safety and meet entrained load (such as detection thunder
Up to, imaging device etc.) stability requirement of normal work.
Empennage is the important component of dirigible utricule, and decisive work is played the aerial self-stabilization state of dirigible utricule is maintained
With empennage controls the aerial statues such as the angle of pitch, yaw angle, the roll angle of dirigible utricule, makes dirigible utricule head towards all the time
Keep the direction of contrary wind.Empennage inside is typically filled with air, air valve, blower fan is provided with above empennage, by certain control
Rule makes empennage inside and outside differential pressure keep within the specific limits, maintaining empennage sweeping appearance.
In general, existing dirigible utricule empennage has two kinds of forms：One kind is that three empennages are separate, each run-out
Each independent a set of blower fan and valve is set on the wing；Another kind is respectively to draw a cross over pipe, empennage in three run-out wing root portions
Mutual UNICOM, sets a set of shared blower fan and valve wherein between any two on a piece of empennage.There is blower fan valve number in the former
Amount problem on the high side；The latter there is a problem of increasing cross over pipe, and annex is more on empennage, and the risk point of gas leakage is more.
Utility model content
In view of the above problems, problem to be solved in the utility model is to provide a kind of simple structure, low cost and can be effective
Reduce the dirigible utricule and dirigible of gas leakage risk point.
To solve the above problems, on the one hand, the utility model uses following technical scheme：
A kind of dirigible utricule, including：
Main gasbag；
Empennage, is arranged at the afterbody of the main gasbag, including at least two tail units；
At the structure that the tail unit and the main gasbag are combined, the air chamber of each tail unit is and institute
The air chamber for stating main gasbag is directly connected.
Preferably, at least one through hole is opened up in the structure that each described tail unit and the main gasbag are combined,
The air chamber of the tail unit is connected through the through hole with the air chamber of the main gasbag.
Preferably, the air chamber of the main gasbag is the first air chamber and the second air chamber, the tail unit through channels separated
Air chamber be connected with second air chamber through the through hole.
Preferably, the separator is arranged at the rear portion of the main gasbag.
Preferably, the separator includes flexible separating film.
Preferably, second air chamber or one of institute also are arranged at including valve and blower fan, the valve and blower fan
State in tail unit.
Preferably, the combination of the junction and the tail unit and the main gasbag of the separator and the main gasbag
Place is intersecting.
Preferably, the empennage includes three tail units being arranged on the main gasbag afterbody periphery, described in three
Tail unit is reverse Y-shaped and is arranged on the periphery of the main gasbag afterbody.
Preferably, a through hole is opened up in the structure that three tail units and the main gasbag are combined.
On the other hand, the utility model uses following technical scheme：
A kind of dirigible, including dirigible utricule as described above.
The utility model provide dirigible utricule at tail unit and the main gasbag faying face, the air chamber of tail unit
Directly connected with the air chamber of main gasbag, it is not necessary to which outside communicating pipe is the connection being capable of achieving between tail unit, only needed a set of
Valve and Fan Equipment can maintain the sweeping appearance of all tail units, and simple structure, low cost simultaneously can effectively reduce gas leakage
Risk point.
Due to using above-mentioned dirigible utricule, simple structure, low cost simultaneously can effectively subtract the dirigible that the utility model is provided
Few gas leakage risk.
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, in the accompanying drawings：
Fig. 1 shows the structural representation of the captive balloon according to the utility model embodiment；
Fig. 2 shows the sectional view of the captive balloon according to the utility model embodiment；
Tail unit is connected with the second air chamber of main gasbag in the captive balloon that Fig. 3 shows according to the utility model embodiment
Structural representation.
In figure, 1, main gasbag；11st, the first air chamber；12nd, the second air chamber；2nd, upper tail unit；3rd, lower-left tail unit；4、
Bottom right tail unit；5th, through hole；6th, separator.
Specific embodiment
Below based on embodiment, present invention is described, but the present invention is not restricted to these embodiments.Under
It is detailed to describe some specific detail sections during text is to detailed description of the invention.Do not have for a person skilled in the art
The description of these detail sections can also completely understand the present invention.In order to avoid obscuring essence of the invention, known method, mistake
Journey, flow, element do not have narration in detail.
It should be appreciated that when certain structure is described, being referred to as being located at another layer, another region when by one layer, a region
" above " or when " top ", can refer to above another layer, another region, or its with another layer, another
Other layers or region are also included between region.Also, if by structure upset, this layer, a region will be positioned at another
Layer, another region " below " or " lower section ".If in order to describe located immediately at another layer, another region above scenario,
Herein will be using " A is directly on B " or the form of presentation of " A is on B and abuts therewith ".
The utility model provides a kind of dirigible utricule, and it includes：
Main gasbag；
Empennage, is arranged at the afterbody of main gasbag, including at least two tail units；
At the structure that tail unit and main gasbag are combined, the air chamber of the air chamber of each tail unit with main gasbag is straight
Lead in succession.
The utility model provide dirigible utricule at tail unit and the main gasbag faying face, the air chamber of tail unit
Directly connected with the air chamber of main gasbag, it is not necessary to which outside communicating pipe is the connection being capable of achieving between tail unit, only needed a set of
Valve and Fan Equipment can maintain the sweeping appearance of all tail units, and simple structure, low cost simultaneously can effectively reduce gas leakage
Risk point.
The embodiment of dirigible utricule of the present utility model is illustrated with reference to Fig. 1 to Fig. 3.
As shown in figure 1, the dirigible utricule includes main gasbag 1 and is arranged at the empennage of the afterbody of main gasbag 1.Main gasbag 1
Shape is not limited, for example, can be the spindle bodily form as shown in Figure 1, and the head sizes of main gasbag 1 are big, and tail dimension is small, spindle
The main gasbag 1 of the bodily form can effectively reduce windage, improve the stationarity of dirigible utricule.
Empennage includes three tail units, and at tail unit and the faying face of main gasbag 1, the air chamber of each tail unit is equal
Air chamber with main gasbag 1 is directly connected.Specifically, as shown in Figures 2 and 3, the knot that each tail unit is combined with main gasbag 1
At least one through hole is opened up on structure, the air chamber via through holes of tail unit are connected with the air chamber of main gasbag 1, therefore it may only be necessary to
A set of valve and Fan Equipment can maintain the sweeping appearance of all tail units.Specifically, valve and Fan Equipment are settable
In main gasbag 1, it is also possible in a tail unit being disposed therein, to reach more preferable effect, valve and blower fan are set
In main gasbag 1 in the middle of three tail units.
Three tail units are arranged on the afterbody periphery of main gasbag 1, it is preferred that as shown in figure 3, three tail unit difference
It is upper tail unit 2, lower-left tail unit 3 and bottom right tail unit 4, three tail units are reverse Y-shaped and are arranged at the tail of main gasbag 1
On the periphery in portion.
It is, of course, understood that the quantity and arrangement of tail unit are not limited to be above-mentioned form, can be according to tool
Body demand is set.
Further, the air chamber of main gasbag 1 is divided into the first air chamber 11 and the second air chamber 12 through separator 6, separator 6
Front portion is the first air chamber 11, and rear portion is the second air chamber 12, and the air chamber via through holes 5 of tail unit are connected with the second air chamber 12, valve
Door and blower fan are arranged in the second air chamber 12.In a preferred embodiment, separator 6 is arranged on the rear portion of main gasbag 1, enters one
Step is preferred, and the distance of separator 6 and the tail end of main gasbag 1 is a quarter of the total length of main gasbag 1 to 1/6th, more preferably
It is 1/5th.In embodiment, the junction of the separator 6 and the main gasbag 1 and the tail unit and the master
Intersect the junction of air bag 1.
The concrete structure of separator 6 is not limited, it is preferred that separator 6 can have in flexible separation membrane, separation membrane in flexibility
Gas shock in effect buffering main gasbag 1, improves the stationarity of dirigible utricule.
Tail unit is with opening up at least one through hole 5, the air chamber via through holes of tail unit in the structure that main gasbag 1 is combined
5 are connected with the air chamber of main gasbag 1.Specifically, as shown in figure 3, each tail unit is with equal in the structure that main gasbag 1 is combined
Offer a through hole 5, be the efficiency for ensureing gas flowing between tail unit and main gasbag 1, the aperture of through hole 5 set compared with
Greatly.
The quantity of through hole 5 is not limited to one, or multiple, is that can also reduce accordingly when the quantity of through hole 5 is more
The aperture of through hole 5, can so increase the structural strength of main gasbag 1.
Further, tail unit can be by the face of tail unit and the face of main gasbag 1 with the structure that main gasbag 1 is combined
It is combined to be formed, or in tail unit and the junction of main gasbag 1, tail unit is set in opening, the edge of opening
Outer surface with main gasbag 1 is connected, and through hole 5 is opened on main gasbag 1.
Additionally, it should be understood by one skilled in the art that accompanying drawing is provided to descriptive purpose provided herein, and
What accompanying drawing was not necessarily drawn to scale.
The utility model also provides a kind of embodiment of dirigible, and the dirigible includes dirigible utricule as described above, described
Dirigible can be kite balloon airship or non-kite balloon airship.The dirigible can also include being connected to the gondola of dirigible.
It will also be appreciated that example embodiment is provided, so that the disclosure is comprehensive, and its scope is fully passed on
To those skilled in the art.Many specific details (such as examples of particular elements, apparatus and method) are presented to provide to this
Disclosed comprehensive understanding.It will be apparent to one skilled in the art that specific detail need not be used, example embodiment can be with much not
Same form is carried out, and example embodiment is understood not to limit the scope of the present disclosure.In some example embodiments,
Well-known device structure and widely-known technique are not described in.
When an element or layer be mentioned as another element or layer " on ", " being engaged to ", " being connected to " or " coupled
To " another element or during layer, it directly can be engaged on another element or layer, directly, be connected or coupled to another element or
Layer, or there may be intermediary element or layer.By contrast, when an element be mentioned as " direct " another element or layer " on ",
When " being bonded directly to ", " being directly coupled to " or " being directly coupled to " another element or layer, can not exist intermediary element
Or layer.Other words for describing relation between element should be explained in a similar manner (for example, " between " with " directly exist
Between ", " neighbouring " and " being directly adjacent to " etc.).As used herein, term "and/or" includes the listed of one or more associations
Any or all combinations in project.
Although term first, second, third, etc. can be used for describing each element, part, region, floor and/or area herein
Section, but these elements, part, region, layer and/or section should not be limited by these terms.These terms can be only used for by
One element, part, region, layer or section are distinguished with another element, region, layer or section.Such as " first ", " second "
Term and other numerical value terms do not mean that order or order when used herein, unless clearly indicated by the context.Thus, below
The first element, part, region, layer or the section for discussing are referred to alternatively as the second element, part, region, layer or section, without departing from
The teaching of example embodiment.Additionally, in the description of the invention, unless otherwise indicated, " multiple " is meant that two or two
More than.
The preferred embodiments of the present invention are the foregoing is only, is not intended to limit the invention, for those skilled in the art
For, the present invention can have various changes and change.It is all any modifications made within spirit and principles of the present invention, equivalent
Replace, improve etc., should be included within the scope of the present invention.
Claims (10)
1. a kind of dirigible utricule, it is characterised in that including：
Main gasbag；
Empennage, is arranged at the afterbody of the main gasbag, including at least two tail units；
At the structure that the tail unit and the main gasbag are combined, the air chamber of each tail unit with the master
The air chamber of air bag is directly connected.
2. dirigible utricule according to claim 1, it is characterised in that each described tail unit is mutually tied with the main gasbag
Open up at least one through hole in the structure of conjunction, the air chamber of the tail unit through the through hole and the main gasbag air chamber phase
Connection.
3. dirigible utricule according to claim 2, it is characterised in that the air chamber of the main gasbag is the through channels separated
One air chamber and the second air chamber, the air chamber of the tail unit are connected through the through hole with second air chamber.
4. dirigible utricule according to claim 3, it is characterised in that after the separator is arranged at the main gasbag
Portion.
5. dirigible utricule according to claim 3, it is characterised in that the separator includes flexible separating film.
6. dirigible utricule according to claim 3, it is characterised in that also including valve and blower fan, the valve and blower fan
It is arranged in second air chamber or one of them described tail unit.
7. dirigible utricule according to claim 4, it is characterised in that the junction of the separator and the main gasbag with
Intersect the junction of the tail unit and the main gasbag.
8. the dirigible utricule according to any one of claim 1 to 7, it is characterised in that the empennage includes being arranged at described
Three tail units on main gasbag afterbody periphery, three tail units are reverse Y-shaped and are arranged at the main gasbag afterbody
On periphery.
9. dirigible utricule according to claim 8, it is characterised in that three tail units are mutually tied with the main gasbag
A through hole is opened up in the structure of conjunction.
10. a kind of dirigible, including the dirigible utricule as described in any one of claim 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621100187.3U CN206218193U (en) | 2016-09-29 | 2016-09-29 | Dirigible utricule and dirigible |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621100187.3U CN206218193U (en) | 2016-09-29 | 2016-09-29 | Dirigible utricule and dirigible |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206218193U true CN206218193U (en) | 2017-06-06 |
Family
ID=58782541
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621100187.3U Active CN206218193U (en) | 2016-09-29 | 2016-09-29 | Dirigible utricule and dirigible |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206218193U (en) |
-
2016
- 2016-09-29 CN CN201621100187.3U patent/CN206218193U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230803 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 |
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| TR01 | Transfer of patent right |