CN204341387U - Aerostatics - Google Patents
Aerostatics Download PDFInfo
- Publication number
- CN204341387U CN204341387U CN201420625711.3U CN201420625711U CN204341387U CN 204341387 U CN204341387 U CN 204341387U CN 201420625711 U CN201420625711 U CN 201420625711U CN 204341387 U CN204341387 U CN 204341387U
- Authority
- CN
- China
- Prior art keywords
- utricule
- aerostatics
- horizontal truss
- mobile jib
- truss portion
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/08—Framework construction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/22—Arrangement of cabins or gondolas
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerials With Secondary Devices (AREA)
- Revetment (AREA)
Abstract
The utility model provides a kind of aerostatics, comprising: multiple utricule, and for bus is the axisymmetric body of arc, this utricule is buoyancy utricule; Multiple the draw in the net structures corresponding with the plurality of utricule, each top of structure from corresponding utricule of drawing in the net is to downward-extension; And truss structure, be connected to this and draw in the net one end away from this utricule of structure, this truss structure comprises: horizontal truss portion, what each utricule was corresponding draw in the net, and structure is all connected to this horizontal truss portion, and the anatomical connectivity that draws in the net corresponding to the plurality of utricule angularly distributes in the position in this horizontal truss portion with the center shaft being parallel to vertical direction of this truss structure; And being connected to the below gondola fixed part in this horizontal truss portion, this gondola fixed part is used for collecting or fixing gondola, and this gondola fixed part is connected to the central area in this horizontal truss portion.
Description
Technical field
The utility model relates to air equipment field, particularly relates to aerostatics.
Background technology
Due in technology and understanding, the strategic value of near space just causes the attention of countries in the world also to become the focus of various countries' research because of its distinguishing feature and potential dual-use value for several years up to date.A lot of country is just numerous and confused at present drops into a large amount of funds, actively develops the technology and application research of near space vehicle.Current near space vehicle is mainly aerostatics as near space dirigible, and near space dirigible adopts blimp mostly, has hang time long, the feature such as load capacity is large, flying height is high, viability is strong.
But, the utricule complex structure of near space dirigible, cause its design and cost of manufacture higher.
Therefore, this area needs a kind of design and the lower aerostatics of cost of manufacture badly.
Utility model content
In order to overcome above-mentioned defect, the utility model aims to provide a kind of lower-cost aerostatics.
According to one side of the present utility model, provide a kind of aerostatics, comprising: multiple utricule, for bus is the axisymmetric body of arc, this utricule is buoyancy utricule; Multiple the draw in the net structures corresponding with the plurality of utricule, each top of structure from corresponding utricule of drawing in the net is to downward-extension; And truss structure, be connected to this and draw in the net one end away from this utricule of structure, this truss structure comprises: horizontal truss portion, what each utricule was corresponding draw in the net, and structure is all connected to this horizontal truss portion, and the anatomical connectivity that draws in the net corresponding to the plurality of utricule angularly distributes in the position in this horizontal truss portion with the center shaft being parallel to vertical direction of this truss structure; And being connected to the below gondola fixed part in this horizontal truss portion, this gondola fixed part is used for collecting or fixing gondola, and this gondola fixed part is connected to the central area in this horizontal truss portion.
In one example, this draws in the net structure and comprises force-supporting belt, poly-band structure and hoist cable, this force-supporting belt comprises many from the top of this utricule to longitudinal force-supporting belt that bottom direction extends, one end of described many longitudinal force-supporting belts is interconnected in the top center of this utricule, this poly-band structure is fixed in one end away from this utricule gathering of these many longitudinal force-supporting belts, this hoist cable comprises many lifting ropes, and one end of every bar lifting rope is connected to the side away from this longitudinal force-supporting belt of this poly-band structure.
In one example, this horizontal truss portion comprises multiple mobile jib, multiple bulkhead bar and multiple brace, and the plurality of mobile jib is parallel to each other, and multiple mobile jib joins end to end by the plurality of bulkhead bar successively, and the plurality of brace to be connected between adjacent mobile jib and to tilt with this mobile jib.
In one example, the plurality of bulkhead bar perpendicular to this mobile jib, and often includes multiple bulkhead bar between adjacent two mobile jibs.
In one example, the plurality of brace is arranged between adjacent bulkhead bar, and the two ends of each brace connect the diagonal position of corresponding two mobile jibs and two bulkhead bar limited areas respectively.
In one example, the adjacent end portion of adjacent brace is connected to same mobile jib.
In one example, the quantity of this mobile jib is four, and head and the tail connect in four bulkhead bars of these four mobile jibs in turn, and wherein three bulkhead pole lengths are equal, and the length of another one bulkhead bar is greater than this three bulkhead bars.
In one example, the bulkhead bar that this length is larger is horizontally disposed with and adjacent with this utricule, and the end of these many lifting ropes is connected to the mobile jib in this horizontal truss portion and the point of crossing place of bulkhead bar.
In one example, the frame of this gondola fixed part shape axisymmetricly, many, this frame is connected to the pipe link of mobile jib, and the position of the point of crossing of these many pipe links and mobile jib distributes axisymmetricly with the center shaft perpendicular to mobile jib and the larger bulkhead bar of length in this horizontal truss portion; Multiple 3rd pipe link head and the tail connect the plurality of other end being connected to the pipe link of mobile jib in turn.
In one example, this aerostatics comprises the drive configuration that two are arranged at this horizontal truss portion opposite end further.
In one example, the quantity in this horizontal truss portion is multiple, and the plurality of horizontal truss portion joins end to end, and the plurality of utricule is connected to this horizontal truss.
In one example, the quantity of this utricule is identical with the quantity in this horizontal truss portion, and the center of drawing in the net position that anatomical connectivity intersects in adjacent level truss portion or the plurality of horizontal truss portion of this utricule.
In one example, the quantity in this horizontal truss portion is multiple, and one end, the plurality of horizontal truss portion is connected and is emanant arrangement, the quantity of this utricule is identical with the quantity in this horizontal truss portion, and the position that the plurality of utricule is connected to this horizontal truss is equal with the distance being parallel to the center shaft of vertical direction of this truss structure.
In one example, the plurality of horizontal truss portion angularly distributes with the center shaft being parallel to vertical direction of this truss structure.
The aerostatics of the present embodiment is that the utricule of the axisymmetric body of arc is as buoyancy utricule owing to have employed bus, adopt and draw in the net structure and truss structure to arrange the load of aerostatics, relative to the dirigible structure of prior art, structure is more simple, and cost of manufacture greatly reduces; And the truss structure of the present embodiment makes the structure of aerostatics entirety more firmly solid, effectively can increase the service life of aerostatics; Further, the present embodiment adopts multiple utricule to provide the buoyancy of aerostatics, and the load of aerostatics can be made greatly to increase, thus aerostatics can be made more to have elasticity when applying.
Accompanying drawing explanation
After the detailed description of reading embodiment disclosed in the utility model in conjunction with the following drawings, more can understand above-mentioned feature and advantage of the present utility model better.
Fig. 1 is the schematic diagram of the aerostatics according to one side of the present utility model.
Fig. 2 is the side schematic view of the truss structure of the aerostatics of Fig. 1.
Fig. 3 is the schematic diagram of the aerostatics according to another aspect of the present utility model.
Fig. 4 is the schematic diagram of the truss structure according to another aspect of the present utility model.
Fig. 5 is the schematic diagram of the truss structure according to another aspect of the present utility model.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.Note, the aspects described below in conjunction with the drawings and specific embodiments is only exemplary, and should not be understood to carry out any restriction to protection domain of the present utility model.
As shown in Figure 1, be the schematic diagram of the utility model aerostatics 100 on the one hand, this aerostatics 100 can be used as tropospheric aerostatics, and also can be used as advection layer aerostatics, it is more obvious for advantage during advection layer aerostatics.This aerostatics 100 comprises utricule 10, draw in the net structure 12 and truss structure 14.
The quantity of this utricule 10 is multiple, and in the present embodiment, this utricule quantity is two.This utricule 10 is superpressure buoyancy utricule, and it is generally the axisymmetric body that bus is arc, as spherical, water-drop-shaped etc.In the present embodiment, the shape that this utricule 10 is is spherosome, comprises multiple capsule lobe (not shown) of docking successively, and the capsule lobe docked successively entirety forms spherosome shape.The material of this utricule 10 can adopt the skin material of dirigible, and in present embodiment, this utricule 10 is multiple-structure, comprises anti-aging layer, glue-line, tissue layer, basalis, high-obstruction and weld layer successively.Be understandable that, can also further form light reflecting material layer (not shown) in the outermost of the multiple-structure of utricule 10, as aluminium foil layer etc., can usable reflection sunray, reduce solar light irradiation to the damage of skin material.
This draws in the net structure 12 is the load-carrying construction connecting utricule 10 and truss structure 14, and it comprises force-supporting belt 120, poly-band structure 122 and hoist cable 124, and all corresponding one of each utricule 10 draws in the net structure 12.This force-supporting belt 120 comprises many from the top of utricule 10 to longitudinal force-supporting belt 126 that bottom direction extends, one end of described many longitudinal force-supporting belts 126 is interconnected in the top center of this utricule 10, this longitudinal force-supporting belt 126 angularly distributes with the top center of this utricule 10, to make the load of utricule 10 even; This force-supporting belt 120 can also comprise many hoop force-supporting belt (not shown) of carrying out arranging for the center of circle with the top center of utricule 10, and hoop force-supporting belt is all connected with many longitudinal force-supporting belts 126, to make the load of utricule 10 more even.The material of this force-supporting belt 120 can adopt but be not limited to individual layer aramid belt.
One end away from this utricule 10 of these many longitudinal force-supporting belts 122 is assembled and is fixed on this poly-band structure 122, this poly-band structure 122 be positioned at this utricule 10 side, bottom and with bottom interval preset distance.In the present embodiment, this poly-band structure 122 is a circular plate-like shape, and its material can be corrosion-resistant steel etc.
This hoist cable 124 comprises many lifting ropes 128, and one end of every bar lifting rope 128 is connected to the side away from this longitudinal force-supporting belt 122 of this poly-band structure 122, and this lifting rope 128 can be but be not limited to steel rope.
See also Fig. 2, this truss structure 14 comprises horizontal truss portion 140 and gondola fixed part 142, this horizontal truss portion 140 for being connected and fixed of hoist cable 124, and keep the balance of whole aerostatics 100 and stable.
This horizontal truss portion 140 comprises mobile jib 141, bulkhead bar 143 and brace 144.This mobile jib 141 quantity is multiple, and in the present embodiment, the quantity of this mobile jib 141 is four, is respectively mobile jib 141-1,141-2,141-3 and 141-4, and these four mobile jibs 141 are parallel to each other.
This bulkhead bar 143 is many, for being connected in turn by multiple mobile jib 141 head and the tail.In the present embodiment, the plurality of bulkhead bar 143 is perpendicular to these four mobile jibs 141, this bulkhead bar 143 comprises the bulkhead bar 143-1 connecting mobile jib 141-1 and 141-2, the bulkhead bar 143-2 connecting mobile jib 141-2 and 141-3, connects the bulkhead bar 143-3 of mobile jib 141-3 and 141-4 and connect the bulkhead bar 143-4 of mobile jib 141-4 and 141-1, often includes the bulkhead bar 143 of many equidistant arrangements between adjacent two mobile jibs 141.In the present embodiment, the length of this bulkhead bar 143-2,143-3 and 143-4 is equal, and the length of bulkhead bar 143-1 is greater than the length of bulkhead bar 143-2,143-3 and 143-4, thus on the face perpendicular to this mobile jib 141, four bulkhead bars 143 form the shape of isosceles trapezoid, and bulkhead bar 143-1 and 143-3 is two bases of this isosceles trapezoid.In the present embodiment, the length of this bulkhead bar 143-1 is the twice of the length of this bulkhead bar 143-2,143-3 and 143-4.
This brace 144 is also multiple, and the two ends of this brace 144 are connected to adjacent mobile jib 141 and favour this mobile jib 141, connect multiple brace 144 between adjacent mobile jib 141, to make the connection structure in horizontal truss portion 140 more firm.In the present embodiment, brace 144 is connected between adjacent formers bar 143, and two ends are connected to the infall that bulkhead bar 143 and mobile jib 141 are positioned at diagonal position, and the adjacent end portion of adjacent brace 144 is connected to same mobile jib 141.
For making the structure in horizontal truss portion 140 more firm, it comprises further and connects the mid point of bulkhead bar 143-1 with first reinforcing rod 146 of mobile jib 141-3 and be connected the mid point of bulkhead bar 143-1 and second reinforcing rod 147 of mobile jib 141-4, preferably, all corresponding first reinforcing rod 146 of each bulkhead bar 143-1 and second reinforcing rod 147.
The mobile jib 141 in this horizontal truss portion 140 and bulkhead bar 143 make horizontal truss portion 140 entirety in strip and the profile of lateral plan presents trapezoidal shape.In use, this mobile jib 141 and bulkhead bar 143-1 and 143-3 are in horizontality, and this bulkhead bar 143-1 is positioned at top.This horizontal truss portion 140 is arranged at the below of two utricules 10, and draw in the net structure 12 be connected to this horizontal truss portion 140, particularly, the hoist cable 124 of these two utricules 10 is connected to the position at the contiguous two ends in this horizontal truss portion 140, and the end of many lifting ropes 128 of each utricule 10 is all connected to the mobile jib 141 in horizontal truss portion 140 and the point of crossing place of bulkhead bar 143, and the band of position of the hoist cable 124 being connected to two utricules 10 in this horizontal truss portion 140 is arranged axisymmetricly with the center shaft perpendicular to mobile jib 141-1 and 141-2 in this horizontal truss portion 140, thus when two utricules 10 are in same level position, maintenance level when horizontal truss portion 140 is lifted and stress equalization.
This gondola fixed part 142 is connected to the below in horizontal truss portion 140, comprise the frame 148 in rectangular shape, 148 two, this frame is connected to the head rod 148-1 of mobile jib 141-3 and is connected to the second pipe link 148-2 of mobile jib 141-4, head rod 148-1 and the second pipe link 148-2 forms four inclines of frame 148, and the position of the point of crossing of head rod 148-1 and the second pipe link 148-2 and mobile jib 141-3 and 141-4 distributes axisymmetricly with the center shaft perpendicular to mobile jib 141-1 and 141-2 in this horizontal truss portion 140, maintenance level when being lifted from making horizontal truss portion 140 and stress equalization, four the 3rd pipe link 148-3 head and the tail connect the other end of head rod 148-1 and the second pipe link 148-2 in turn, form four bases of cuboid frame 148, four sides of cuboid frame 148 and bottom surface all have the oblique pipe link 148-4 connecting diagonal angle.The space that this gondola fixed part 142 limits is for loading gondola (not shown), and this gondola is for loading Aerial Electronic Equipment, flight control unit, communicator etc.In other implementations, the profile of this gondola fixed part 142 also can other shape, is generally axisymmetric body, is not limited with the present embodiment.
Aerostatics 100 can comprise buffer structure 149 further, and this buffer structure 149 for being arranged at the cushion of four corners bottom this gondola fixed part 142, for closing on buffering when aerostatics 100 lands, can damage to prevent aerostatics 100.
The aerostatics 100 of the present embodiment is that the utricule 10 of the axisymmetric body of arc is as buoyancy utricule owing to have employed bus, adopt and draw in the net structure 12 and truss structure 14 to arrange the load of aerostatics 100, relative to the dirigible structure of prior art, structure is more simple, and cost of manufacture greatly reduces; And the truss structure 14 of the present embodiment makes the structure of aerostatics 100 entirety more firmly solid, effectively can increase the service life of aerostatics 100; Further, the present embodiment adopts multiple utricule 10 to provide the buoyancy of aerostatics 100, and the load of aerostatics 100 can be made greatly to increase, thus aerostatics 100 can be made more to have elasticity when applying.
Refer to Fig. 3, for the schematic diagram of the utility model aerostatics 200 on the other hand, this aerostatics 200 is with the difference of aerostatics 100, aerostatics 200 comprises two drive configurations 20 further, be arranged at the opposite end in horizontal truss portion 140 respectively, in the present embodiment, this drive configuration 20 is screw propeller.Drive configuration 20 moves in the horizontal direction for driving aerostatics 200.The set-up mode of drive configuration 20 can be decided according to the actual requirements.
Refer to Fig. 4, be the schematic diagram of the truss structure 14a of the another kind of embodiment of the utility model aerostatics, this truss structure 14a comprises six horizontal truss portions 140 and joins end to end, and forming profile is hexagonal truss structure 14a, is preferably regular hexagon.When this truss structure 14a is applied to aerostatics, general employing six utricules 10 are connected with this truss structure 14a, and connection location is positioned at the intersection location in adjacent level truss portion 140, as the region at circular dashed line place in Fig. 4; Gondola (not shown) is arranged at the center being positioned at truss structure 14a, the region that " * " shape dotted line at center is as shown in Figure 4 contained, and can accommodate gondola, also can connect gondola by hoist cable by arranging gondola fixed part 142.Be understandable that, six utricules 10 also can be connected in other position with this truss structure 14a, as the center in each horizontal truss portion 140.Certainly, the quantity of utricule 10 is also not limited to six, can carry out suitable increase and decrease according to actual needs, as long as utricule 10 angularly distributes with the center shaft being parallel to vertical direction of this truss structure 10 with the connection location of truss structure 14a.In the present embodiment, more utricule 10 can provide more buoyancy, can promote more load.Be understandable that, the quantity in horizontal truss portion 140 end to end in truss structure 14a can increase and decrease according to actual needs, is not limited with the present embodiment.
Refer to Fig. 5, for the schematic diagram of the truss structure 14b of the another kind of embodiment of the utility model aerostatics, this truss structure 14b comprises one end and is connected and is six horizontal truss portions 140 of emanant arrangement, form emanant truss structure 14b, and the length in these six horizontal truss portions 140 is equal, in the present embodiment, these six horizontal truss portions 140 angularly distribute with the center shaft being parallel to vertical direction of this truss structure 14b.When this truss structure 14b is applied to aerostatics, general employing six utricules 10 are connected with this truss structure 14b, connection location is positioned in horizontal truss portion 140 and the connection location of six utricules 10 is equal with the distance at the center of this truss structure 14b, as the region at circular dashed line place in Fig. 5; Gondola (not shown) is arranged at the center being positioned at truss structure 14b, the region that " * " shape dotted line at center is as shown in Figure 4 contained, and can accommodate gondola, also can connect gondola by hoist cable by arranging gondola fixed part 142.In the present embodiment, more utricule 10 can provide more buoyancy, can promote more load.In the present embodiment, more utricule 10 can provide more buoyancy, can promote more load.Be understandable that, the quantity in the horizontal truss portion 140 in emanant arrangement in truss structure 14b can increase and decrease according to actual needs, is not limited with the present embodiment.
Description before providing is to make any technical personnel in this area all can put into practice various aspects described herein.But should be appreciated that, protection domain of the present utility model should be as the criterion with claims, and should not be defined to concrete structure and the assembly of above explained orally embodiment.Those skilled in the art, in spirit and scope of the present utility model, can carry out various variation and amendment to each embodiment, and these variations and amendment also drop within protection domain of the present utility model.
Claims (14)
1. an aerostatics, comprising:
Multiple utricule, for bus is the axisymmetric body of arc, this utricule is buoyancy utricule;
Multiple the draw in the net structures corresponding with the plurality of utricule, each top of structure from corresponding utricule of drawing in the net is to downward-extension; And
Truss structure, be connected to this and draw in the net one end away from this utricule of structure, this truss structure comprises:
Horizontal truss portion, what each utricule was corresponding draw in the net, and structure is all connected to this horizontal truss portion, and the anatomical connectivity that draws in the net corresponding to the plurality of utricule angularly distributes in the position in this horizontal truss portion with the center shaft being parallel to vertical direction of this truss structure; And
Be connected to the below gondola fixed part in this horizontal truss portion, this gondola fixed part is used for collecting or fixing gondola, and this gondola fixed part is connected to the central area in this horizontal truss portion.
2. aerostatics as claimed in claim 1, it is characterized in that, this draws in the net structure and comprises force-supporting belt, poly-band structure and hoist cable, this force-supporting belt comprises many from the top of this utricule to longitudinal force-supporting belt that bottom direction extends, one end of described many longitudinal force-supporting belts is interconnected in the top center of this utricule, this poly-band structure is fixed in one end away from this utricule gathering of these many longitudinal force-supporting belts, this hoist cable comprises many lifting ropes, and one end of every bar lifting rope is connected to the side away from this longitudinal force-supporting belt of this poly-band structure.
3. aerostatics as claimed in claim 2, it is characterized in that, this horizontal truss portion comprises multiple mobile jib, multiple bulkhead bar and multiple brace, the plurality of mobile jib is parallel to each other, multiple mobile jib joins end to end by the plurality of bulkhead bar successively, and the plurality of brace to be connected between adjacent mobile jib and to tilt with this mobile jib.
4. aerostatics as claimed in claim 3, it is characterized in that, the plurality of bulkhead bar perpendicular to this mobile jib, and often includes multiple bulkhead bar between adjacent two mobile jibs.
5. aerostatics as claimed in claim 4, it is characterized in that, the plurality of brace is arranged between adjacent bulkhead bar, and the two ends of each brace connect the diagonal position of corresponding two mobile jibs and two bulkhead bar limited areas respectively.
6. aerostatics as claimed in claim 5, it is characterized in that, the adjacent end portion of adjacent brace is connected to same mobile jib.
7. aerostatics as claimed in claim 6, it is characterized in that, the quantity of this mobile jib is four, and head and the tail connect in four bulkhead bars of these four mobile jibs in turn, and wherein three bulkhead pole lengths are equal, and the length of another one bulkhead bar is greater than this three bulkhead bars.
8. aerostatics as claimed in claim 7, is characterized in that, the bulkhead bar that this length is larger is horizontally disposed with and adjacent with this utricule, and the end of these many lifting ropes is connected to the mobile jib in this horizontal truss portion and the point of crossing place of bulkhead bar.
9. aerostatics as claimed in claim 7, it is characterized in that, the frame of this gondola fixed part shape axisymmetricly, the pipe link that many, this frame is connected to mobile jib forms the incline of this frame, and the position of the point of crossing of these many pipe links and mobile jib distributes axisymmetricly with the center shaft perpendicular to mobile jib and the larger bulkhead bar of length in this horizontal truss portion; Multiple 3rd pipe link head and the tail connect the plurality of other end being connected to the pipe link of mobile jib in turn.
10. aerostatics as claimed in claim 1, it is characterized in that, this aerostatics comprises the drive configuration that two are arranged at this horizontal truss portion opposite end further.
11. aerostatics as claimed in claim 1, is characterized in that, the quantity in this horizontal truss portion is multiple, and the plurality of horizontal truss portion joins end to end, and the plurality of utricule is connected to this horizontal truss.
12. aerostatics as claimed in claim 11, it is characterized in that, the quantity of this utricule is identical with the quantity in this horizontal truss portion, and the center of drawing in the net position that anatomical connectivity intersects in adjacent level truss portion or the plurality of horizontal truss portion of this utricule.
13. aerostatics as claimed in claim 1, it is characterized in that, the quantity in this horizontal truss portion is multiple, and one end, the plurality of horizontal truss portion is connected and is emanant arrangement, the quantity of this utricule is identical with the quantity in this horizontal truss portion, and the position that the plurality of utricule is connected to this horizontal truss is equal with the distance being parallel to the center shaft of vertical direction of this truss structure.
14. aerostatics as claimed in claim 13, it is characterized in that, the plurality of horizontal truss portion angularly distributes with the center shaft being parallel to vertical direction of this truss structure.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420625711.3U CN204341387U (en) | 2014-10-27 | 2014-10-27 | Aerostatics |
| PCT/CN2015/086764 WO2016065973A1 (en) | 2014-10-27 | 2015-08-12 | Aerostat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420625711.3U CN204341387U (en) | 2014-10-27 | 2014-10-27 | Aerostatics |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204341387U true CN204341387U (en) | 2015-05-20 |
Family
ID=53224677
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420625711.3U Expired - Fee Related CN204341387U (en) | 2014-10-27 | 2014-10-27 | Aerostatics |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN204341387U (en) |
| WO (1) | WO2016065973A1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016065973A1 (en) * | 2014-10-27 | 2016-05-06 | 深圳光启空间技术有限公司 | Aerostat |
| CN106516070A (en) * | 2015-09-14 | 2017-03-22 | 东莞前沿技术研究院 | High-altitude balloon |
| CN108657412A (en) * | 2017-03-31 | 2018-10-16 | 成都天府新区光启未来技术研究院 | Damping unit and aerostatics for aerostatics |
| CN110228579A (en) * | 2018-03-05 | 2019-09-13 | 东莞前沿技术研究院 | Floating transport device |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2063110U (en) * | 1990-02-10 | 1990-10-03 | 北京市西城新开通用试验厂 | Floating aircraft |
| US6843448B2 (en) * | 2002-09-30 | 2005-01-18 | Daniel W. Parmley | Lighter-than-air twin hull hybrid airship |
| US8061647B1 (en) * | 2007-04-13 | 2011-11-22 | John Powell | High altitude two balloon airship |
| CN204341387U (en) * | 2014-10-27 | 2015-05-20 | 深圳光启空间技术有限公司 | Aerostatics |
-
2014
- 2014-10-27 CN CN201420625711.3U patent/CN204341387U/en not_active Expired - Fee Related
-
2015
- 2015-08-12 WO PCT/CN2015/086764 patent/WO2016065973A1/en active Application Filing
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016065973A1 (en) * | 2014-10-27 | 2016-05-06 | 深圳光启空间技术有限公司 | Aerostat |
| CN106516070A (en) * | 2015-09-14 | 2017-03-22 | 东莞前沿技术研究院 | High-altitude balloon |
| CN108657412A (en) * | 2017-03-31 | 2018-10-16 | 成都天府新区光启未来技术研究院 | Damping unit and aerostatics for aerostatics |
| CN110228579A (en) * | 2018-03-05 | 2019-09-13 | 东莞前沿技术研究院 | Floating transport device |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2016065973A1 (en) | 2016-05-06 |
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