CN202414152U - Balloon bag for hot-air mooring balloon - Google Patents
Balloon bag for hot-air mooring balloon Download PDFInfo
- Publication number
- CN202414152U CN202414152U CN2011205189793U CN201120518979U CN202414152U CN 202414152 U CN202414152 U CN 202414152U CN 2011205189793 U CN2011205189793 U CN 2011205189793U CN 201120518979 U CN201120518979 U CN 201120518979U CN 202414152 U CN202414152 U CN 202414152U
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- Prior art keywords
- air bag
- empennage
- air
- hot gas
- balloon
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Abstract
The utility model discloses a balloon bag for a hot-air mooring balloon. The balloon bag comprises an air bag, an air bag diaphragm, a pressurizing hole, empennages, empennage tension ropes, bowknots and mooring ropes, wherein inner inhaul cables are arranged in the air bag; the air bag is divided into a front air chamber and a rear air chamber which are sealed independently by the air bag diaphragm; the pressurizing hole is formed in the air bag diaphragm; reinforcing meshes formed by high-strength braids are arranged on the air bag and the empennages; and air vents are formed at the bottoms of the empennages and are communicated with the air chamber at the rear end of the air bag. The balloon bag has the outstanding characteristics of high structural strength, large loading capacity, high safety and the like, and completely meets the using requirement of the hot-air mooring balloon and particularly the hyperpressure hot-air mooring balloon.
Description
Technical field
The utility model relates to a kind of hot gas captive balloon sacculus, belongs to the aircraft field that is lighter than air.
Background technology
Captive balloon is a kind of self buoyancy and long-time empty aerostatics that stagnates of mooring hawser realization of relying on; Through carrying electronic machines such as various communications, interference, scouting and detection; Realize multiple different application purpose with its unique use advantage, obtained concern more and more widely.Traditional captive balloon generally adopts hydrogen or helium as lift gas, and in the actual use, people consider hydrogen potential danger in its use, thereby make helium become the lift gas of the unique use of present captive balloon.Yet along with the shortage day by day of this non-renewable resources of helium, when the river rises the boat goes up for helium captive balloon cost and use cost in recent years.Therefore, development is a kind of becomes the important development direction in current aerostatics field with cheap hot air as the hot gas captive balloon of lift gas.Conventional at present fire balloon and hot gas ship adopt open airbag structure; The inner draught head with external environment approaching zero of air bag; Adopt this fire balloon or hot gas ship to stay platform,, promptly occur distortion easily at less wind speed lower gasbag in the course of the work because of its air bag lacks the windward side wind loading rating as the empty set that stagnates; Thereby cause poor stability, the load capacity of this fire balloon or hot gas ship little, be difficult to realize the application advantage of captive balloon.
The utility model content
The purpose of the utility model is to overcome existing hot gas tethered platform and lacks the little deficiency of wind loading rating, easy deformation, poor stability and load capacity, provides a kind of wind loading rating strong, the hot gas captive balloon sacculus that load capacity is high.
In order to achieve the above object, the technical scheme that provides of the utility model is:
A kind of hot gas captive balloon sacculus comprises that mainly air bag, air bag barrier film, pressurized hole, empennage, empennage open rope, bow tie and mooring hawser, and the air bag barrier film is arranged on rearward end in the air bag; Air bag is divided into former and later two independent sealed air chambers; 3～4 empennages are connected with the air bag back end outer surface, and empennage is opened rope and is arranged between empennage and the empennage, and empennage is fused; Bow tie is arranged on the outside face of air bag both sides, is connected with the mooring hawser.
It behind the described airbag aeration swept-out olive spheroid; Bag material can adopt conventional fire balloon or employed gas barrier property fabric of hot air dirigible airship or polymeric coating layer flexible composite; It is characterized in that air bag vertically, be arranged at intervals with the high strength ribbon respectively on the hoop direction, constitute a structure reinforcing mat at gasbag outer surface, the air bag set inside has many group inhauls; Inhaul top point of connection is distributed in the air bag top; The inhaul lower end converges to the air bag bottom, load mounts on the position, and simultaneously, air bag head and afterbody also are respectively arranged with a hot gas captive balloon operation rope.
Described empennage is an inflatable membrane structure empennage, adopts the machine-shaping of fire balloon bag material, empennage vertically and transversely also be provided with the high strength ribbon, empennage and air bag fuse, and are provided with air extractor vent bottom the empennage and are communicated with the air chamber of air bag rear end.
Described empennage Zhang Shengwei organizes the high-strength light fibrecord more, opens anti-rope winding structure is set on the rope.
Described pressurized hole is used to install hot gas captive balloon empennage booster fan, and pressurized hole is arranged on the air bag barrier film, also can be arranged on the joint face of the anterior air chamber of empennage and air bag.
Described mooring hawser adopts the high-strength light fibrecord, and the mooring hawser is distributed in the gasbag outer surface both sides, and its upper end connects bow tie, and the lower end is converged and can be connected with the mooring guy of hot gas captive balloon ground anchoring system.
Adopt a kind of hot gas captive balloon sacculus of the utility model, through air bag in-to-in inhaul, ball load is distributed on the stiffening band of balloon surface uniformly; Through air bag barrier film and pressurized hole, utilize hot gas captive balloon ball to carry booster fan and make the inflatable empennage can obtain the gaseous tension higher, to improve the rigidity of empennage than air bag; Open rope through empennage and improved the integral rigidity and the intensity of empennage, and then improved the wind resistance of sacculus.Therefore, a kind of hot gas captive balloon balloon structure of the utility model has outstanding features such as structural strength height, load capacity is big, safety is good, satisfies the especially operating needs on the superpressure formula hot gas captive balloon of hot gas captive balloon fully.
Description of drawings
Fig. 1 is a kind of hot gas captive balloon sacculus block diagram of the utility model.
Among the figure: 1, air bag; 2, inhaul; 3, empennage; 4, empennage is opened rope; 5, air bag tail rope; 6, air bag barrier film; 7, pressurized hole; 8, bow tie; 9, mooring hawser; 10, air bag string for binding a plait.
The specific embodiment
Below in conjunction with Figure of description and embodiment; The utility model is further described; Embodiment only supplies to explain the usefulness of the utility model; But not to the restriction of the utility model, the technical personnel in relevant technologies field, the modification of under the situation of spirit that does not break away from the utility model and scope, having done or change the category that also should belong to the utility model.
Embodiment
As shown in Figure 1, a kind of hot gas captive balloon sacculus comprises that mainly air bag 1, air bag barrier film 6, pressurized hole 7, empennage 3, empennage open rope 4, bow tie 8 and mooring hawser 9.Wherein air bag 1 outside face vertically, be arranged at intervals with the high strength ribbon respectively on the hoop direction; Constitute a structure reinforcing mat at air bag 1 outside face; Air bag 1 set inside has two groups of inhauls 2, and inhaul 2 top point of connection are distributed in air bag 1 top, and inhaul 2 lower ends converge to air bag 1 bottom, load mounts on the position; Simultaneously, air bag 1 head and afterbody also are respectively arranged with an air bag string for binding a plait 10, air bag tail rope 5; Air bag barrier film 6 is arranged in the air bag 1, rearward end, and air bag 1 is divided into former and later two independent sealed air chambers; Pressurized hole 7 is arranged on the air bag barrier film 6, and mounting hole is used in the circle hot gas captive balloon booster fan installation that is provided with on every side in hole; Three inflatable empennages 3 are connected with air bag 1 rear end, outside face, and vertically reaching of empennage 3 outside faces transversely is provided with the high strength ribbon, and empennage 3 bottoms are provided with air extractor vent and are communicated with the rear end air chamber of air bag 1; Three groups of empennages are opened rope 4 and are arranged between three empennages, empennage 3 is fused, and empennage are opened between the rope 4 antiwind structure is set; Five groups of bow ties 8 are symmetricly set on the outside face of air bag 1 both sides, are connected with mooring hawser 9; Mooring hawser 9 is distributed in air bag 1 outside face both sides, and its upper end connects bow tie 8, and the lower end is converged with the mooring guy of hot gas captive balloon ground anchoring system and is connected.
Repeatedly a kind of hot gas captive balloon sacculus of flight test proof the utility model satisfies the user demand of multiple different loads on the hot gas captive balloon fully.
Claims (7)
1. hot gas captive balloon sacculus; Comprise that air bag, air bag barrier film, pressurized hole, empennage, empennage open rope, bow tie and mooring hawser; It is characterized in that, gasbag outer surface vertically, be arranged at intervals with the high strength ribbon respectively on the hoop direction, constitute a structure reinforcing mat; The air bag set inside has many group inhauls, and inhaul top point of connection is distributed in the air bag top, and the load that the inhaul lower end converges to the air bag bottom mounts on the position; The air bag barrier film is arranged on rearward end in the air bag, and air bag is divided into former and later two independent sealed air chambers; On the joint face of air bag barrier film or empennage and the anterior air chamber of air bag, be provided with the pressurized hole that is used to install hot gas captive balloon empennage booster fan; 3～4 empennages are connected with the air bag back end outer surface, are provided with empennage between empennage and the empennage and open rope, and empennage is fused.
2. hot gas captive balloon sacculus as claimed in claim 1 is characterized in that, said air bag head and afterbody also are respectively arranged with a hot gas captive balloon operation rope.
3. hot gas captive balloon sacculus as claimed in claim 1; It is characterized in that; Said empennage is an inflatable membrane structure empennage, adopts the machine-shaping of fire balloon bag material, and empennage vertically reaches and transversely also is provided with the high strength ribbon; Empennage and air bag fuse, and empennage bottom is provided with air extractor vent and is communicated with the air chamber of air bag rear end.
4. hot gas captive balloon sacculus as claimed in claim 1 is characterized in that said empennage Zhang Shengwei organizes the high-strength light fibrecord more, opens anti-rope winding structure is set on the rope.
5. hot gas captive balloon sacculus as claimed in claim 1 is characterized in that said bow tie is arranged on the outside face of air bag both sides, is connected with the mooring hawser.
6. hot gas captive balloon sacculus as claimed in claim 1; It is characterized in that said mooring hawser adopts the high-strength light fibrecord, the mooring hawser is distributed in the gasbag outer surface both sides; Its upper end connects bow tie, and the lower end is converged and can be connected with the mooring guy of hot gas captive balloon ground anchoring system.
7. like each described hot gas captive balloon sacculus in the claim 1 to 6; It is characterized in that; Be swept-out olive spheroid behind the said airbag aeration, bag material adopts conventional fire balloon or employed gas barrier property fabric of hot air dirigible airship or polymeric coating layer flexible composite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205189793U CN202414152U (en) | 2011-12-13 | 2011-12-13 | Balloon bag for hot-air mooring balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205189793U CN202414152U (en) | 2011-12-13 | 2011-12-13 | Balloon bag for hot-air mooring balloon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202414152U true CN202414152U (en) | 2012-09-05 |
Family
ID=46738939
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205189793U Withdrawn - After Issue CN202414152U (en) | 2011-12-13 | 2011-12-13 | Balloon bag for hot-air mooring balloon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202414152U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102442419A (en) * | 2011-12-13 | 2012-05-09 | 湖南航天机电设备与特种材料研究所 | Balloon body of hot-air captive balloon |
| CN102874402A (en) * | 2012-09-25 | 2013-01-16 | 襄阳宏伟航空器有限责任公司 | Airtight pressure-charged hot-gas floating platform |
-
2011
- 2011-12-13 CN CN2011205189793U patent/CN202414152U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102442419A (en) * | 2011-12-13 | 2012-05-09 | 湖南航天机电设备与特种材料研究所 | Balloon body of hot-air captive balloon |
| CN102442419B (en) * | 2011-12-13 | 2014-10-01 | 湖南航天机电设备与特种材料研究所 | Balloon body of hot-air captive balloon |
| CN102874402A (en) * | 2012-09-25 | 2013-01-16 | 襄阳宏伟航空器有限责任公司 | Airtight pressure-charged hot-gas floating platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20120905 Effective date of abandoning: 20141001 |
|
| RGAV | Abandon patent right to avoid regrant |