CN109693806B - Mooring balloon anchoring platform and using method - Google Patents
Mooring balloon anchoring platform and using method Download PDFInfo
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- CN109693806B CN109693806B CN201910037914.8A CN201910037914A CN109693806B CN 109693806 B CN109693806 B CN 109693806B CN 201910037914 A CN201910037914 A CN 201910037914A CN 109693806 B CN109693806 B CN 109693806B
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- mooring
- chamber
- ball seat
- cross arm
- platform
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
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- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
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Abstract
The invention belongs to the technical field of captive balloon operation and guarantee design, and relates to a captive balloon anchoring platform and a using method thereof; a captive balloon mooring platform comprising: the device comprises a ball seat, a spare part chamber, an empennage storage chamber, a lift-off recovery chamber, a maintenance chamber and a plurality of lift-off recovery devices, wherein the spare part chamber, the empennage storage chamber, the lift-off recovery chamber, the maintenance chamber and the lift-off recovery devices are positioned in the ball seat; the ball seat is in a trapezoidal table shape, the middle part of the upper surface of the ball seat is provided with a conformal curved surface matched with the lower surface of the balloon, and two sides of the upper surface of the ball seat are provided with a cross arm slide rail, a cross arm arranged on the cross arm slide rail and a plurality of upper mooring riggings; the ball seat is provided with a door for entering the maintenance room; a plurality of bottom mooring riggings are arranged at the bottom of the interior of the lift-off recovery chamber; during anchoring, helium in the sphere can be released, so that the sphere is shrunken and placed in a conformal curved surface, and the cover plate is tightly fixed through the cross arm slide rail so as to resist extreme climate such as strong storm; by utilizing the captive balloon anchoring platform, the application area can be continuously expanded to areas with complex geographical and topographic conditions, such as ocean reefs, steep mountains, wetland beaches and the like.
Description
Technical Field
The invention belongs to the technical field of tethered balloon operation and guarantee design, and particularly relates to a tethered balloon anchoring platform and a using method thereof.
Background
Due to the advantages of long standing time, good economical efficiency, high safety and the like, the captive balloon has wider and wider application field and higher environmental adaptability requirement, and needs to resist severe weather such as strong wind and the like in the use process. The captive balloon needs to complete safe and reliable work in long voyage, and guarantee conditions including gas guarantee, weather guarantee, electric power guarantee, spare part guarantee, aerial work platform and the like need to be provided.
The current operation and guarantee scheme of the captive balloon mainly comprises two modes of a vehicle-mounted mobile mode and a position fixed mode. The mobile type arrangement is flexible, but guarantees such as roads, detection maintenance and boat depot fields need to be provided, the work is difficult to be carried out in regions with limited terrain conditions, such as ocean reefs, steep mountains, wetland beaches and other geographical and terrain condition limited regions, the wind resistance of the mobile type captive balloon is limited by design such as anchor parking, the existing captive balloon operation and guarantee mode is difficult to transport, lift and mount, and the environmental adaptability is insufficient. The construction scale of the captive balloons and the construction guarantee conditions such as the hardened ground, the hardened ball house, the high-altitude operation platform and the like in the position mode is large, the construction cost is high, the operation guarantee resource requirement is large, and the use of the captive balloons is limited as the application fields of the captive balloons are continuously increased.
At present, large-scale guarantee equipment such as ball storehouses, position, anchor parking and the like is generally constructed on the ground, and early withdrawing and evasion are carried out through meteorological prediction. However, in the areas such as ocean reefs, steep mountains, wetland beaches and the like, the areas are far away from cities, lack of engineering matching capacity, limited engineering construction sites, difficult use of large-scale mechanical equipment, heavy system equipment and auxiliary tools, limited equipment guarantee conditions and long replenishment period. The captive balloons applied in these places cannot avoid strong wind by withdrawing and converting, and cannot or cannot build large-scale guarantee conditions to resist severe weather. Therefore, it is necessary to reduce the operation of the captive balloon and guarantee the resource demand, improve the automation degree of the equipment, and improve the guarantee performance and reliability of the system.
Disclosure of Invention
The purpose of the invention is: a mooring balloon anchoring platform and a using method are designed to solve the technical problems that the existing mooring balloon scheme cannot avoid strong wind through retraction and conversion in regions such as ocean reefs, steep mountains, wetland beaches and the like, and large-scale guarantee conditions are not available or cannot be built to resist severe weather, and the environmental adaptability of the mooring balloon is improved.
In order to solve the technical problem, the technical scheme of the invention is as follows: a captive balloon anchoring platform, comprising:
the device comprises a ball seat 1, and a spare part chamber 2, an empennage storage chamber 8, a lift-off recovery chamber 9, a maintenance chamber 10 and a plurality of lift-off recovery devices 14 which are positioned in the ball seat; the ball seat 1 is in a trapezoidal table shape, the middle of the upper surface of the ball seat is provided with a conformal curved surface 5 matched with the lower surface of the balloon, and two sides of the upper surface of the ball seat are provided with a cross arm slide rail 3, a cross arm 6 arranged on the cross arm slide rail 3 and a plurality of upper mooring riggings 4; the tee 1 is provided with a door 11 for accessing the service room 10; a plurality of bottom mooring riggings 15 are arranged at the bottom inside the lift-off recovery chamber 9; the upper part of the cross arm slide rail 3 is provided with an upper rail for the sliding of the cross arm 6.
Preferably, the anchoring platform further comprises a cover plate for covering the upper part of the conformal curved surface 5, and the upper part of the cross arm sliding rail 3 is provided with an inner side rail for fixing the cover plate.
The service room 10 is located at an opposite side of the spare part room 2 or a front area of the ball seat 1.
The tail storage chamber 8 is at the rear of the tee 1 or in the spare part chamber 2.
The use method of the captive balloon anchoring platform comprises the following steps in the erection process:
spreading the captive balloon on the conformal curved surface 5; the ball body 7 is inflated through a helium tank in the spare part chamber 2 inside the ball seat 1; the cross arm 6 is folded and moves back and forth on the cross arm slide rail 3, the ball body 7 is fixed, and the tail wing is installed for the captive balloon.
The bottom mooring rigging 15 can be a mooring lock, mooring chain, mooring cable.
The upper mooring rigging 4 can be a mooring lock, mooring chain, mooring cable.
The use method of the captive balloon anchoring platform comprises the following steps in the anchoring process:
attaching the captive balloon to the conformal curved surface 5 of the ball seat 1; the captive balloon is secured to the mooring platform by cross-point mooring of the upper mooring rigging 4 and the lower mooring rigging 15. The upper part of the sphere 7 and the upper mooring rigging 4 as well as the lower part of the sphere 7 and the bottom mooring rigging 15 form multi-point mooring fixation; the bottom mooring rigging 15 positioned in the lift-off recovery chamber 9 is fixed in a cross mooring mode when being moored with the lower part of the ball body 7.
The balloon empennage is detached and stored in the empennage storage chamber 8. The operations such as captive balloon detection and maintenance are performed through the cross arm 6 and the cross arm slide rail 3, and field-level maintenance is performed in the maintenance room 10. When a strong storm comes, helium in the sphere 7 is partially released, so that the sphere 7 is shrunken and placed in the conformal curved surface 5, and the cover plate is tightly fixed and compressed through the cross arm slide rail 3 to resist extreme weather.
The invention has the beneficial effects that: the captive balloon anchoring platform can be used for continuously expanding an application area to regions with complex geographical and topographic conditions, such as ocean islands, steep mountains, wetland beaches and the like, executing various tasks, such as reconnaissance monitoring, broadband communication, environmental monitoring, resource detection and the like, promoting the development and utilization of the construction of the Xinjiang soil, and providing important support for realizing the science and technology strong national strategy and the like in China. The mooring balloon anchoring platform provides powerful operation guarantee support for the application and popularization of the mooring balloon.
Drawings
In order to more clearly illustrate the technical solution of the present invention, the drawings used in the embodiment of the present invention will be briefly explained. It is obvious that the drawings described below are only some embodiments of the invention, and that for a person skilled in the art, other drawings can be obtained from these drawings without inventive effort.
FIG. 1 is a schematic illustration of an embodiment of a captive balloon mooring platform according to the invention;
FIG. 2 is a top view of an example tethered balloon anchoring platform of the present invention;
FIG. 3 is a schematic illustration of the manner in which an example of a captive balloon anchoring platform of the present invention is tethered;
the device comprises a ball seat 1, a spare part chamber 2, a cross arm slide rail 3, an upper mooring rigging 4, a conformal curved surface 5, a cross arm 6, a ball 7, a tail storage chamber 8, a lift-off recovery chamber 9, a maintenance chamber 10, a door 11, lift-off recovery equipment 14 and a bottom mooring rigging 15.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention. It is to be understood that the embodiments described are only a few embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Features of various aspects of embodiments of the invention will be described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be practiced without these specific details. The following description of the embodiments is merely intended to better understand the present invention by illustrating examples thereof. The present invention is not limited to any particular arrangement or method provided below, but rather covers all product structures, any modifications, alterations, etc. of the method covered without departing from the spirit of the invention.
In the drawings and the following description, well-known structures and techniques are not shown to avoid unnecessarily obscuring the present invention.
One embodiment of a captive balloon mooring platform of the invention, shown in figures 1 and 2, comprises a tee 1, spare part room 2, cross arm skid 3, upper mooring rigging 4, conformal curved surface 5, cross arm 6, tail storage 8, lift-off recovery 9, service room 10, door 11, lift-off recovery equipment 14, and bottom mooring rigging 15. The ball seat 1 is in a trapezoidal table shape, so that rainwater can be combed through conveniently, the building can resist wind, the middle part of the upper surface is provided with a conformal curved surface 5 matched with the lower surface of the balloon, and two sides of the upper surface are provided with cross arm slide rails 3; the spare part chamber 2 is mainly used for storing helium and spare parts and arranging a captive balloon operation monitoring room according to requirements. The service chamber 10 is mainly used for the maintenance of the capsule and the ball-mounted equipment, and may be located at the opposite side of the spare part chamber 2 or in the front area of the ball seat 1. The tail storage chamber 8 is arranged in the rear area of the tee 1 or directly in the spare part chamber 2. Independent tracks are arranged on the upper portion and the inner side of the cross arm sliding rail 3, the upper track is used for sliding of the cross arm 6, and the inner track is used for fixing the conformal curved surface 5 covering plate.
When using the captive balloon mooring platform of the present invention, the various processes are as follows:
during erection, the captive balloon is laid on the conformal curved surface 5 and the ball 7 is inflated by a helium tank in the spare part chamber 2 on one side of the ball seat 1. The cross arm 6 is folded, moves back and forth on the cross arm slide rail 3, stretches out and draws back according to the installation height distance, fixes the ball body 7, and installs accessories such as empennages and the like for the captive balloon.
During anchoring, the captive balloon can be completely attached to the conformal curved surface 5, so that the captive balloon and the ball seat 1 are integrated. The captive balloon is secured to the mooring platform by a plurality of upper mooring lines 4 and lower mooring lines 15 in a cross-over multi-point mooring manner, schematically illustrated in figure 3, using mooring lines for the lower mooring lines 15; the balloon empennage is detached and stored in the empennage storage chamber 8. The operations such as captive balloon detection and maintenance are performed through the cross arm 6 and the cross arm slide rail 3, and field-level maintenance is performed in the maintenance room 10. When a strong storm comes, helium in the sphere 7 is partially released, so that the sphere 7 is shrunken and placed in the conformal curved surface 5, and the cover plate is tightly fixed and compressed through the cross arm slide rail 3 to resist extreme weather.
When the hoisting and the recovery are carried out, the cross arm 6 is opened, and the mooring rope passes through the equipment room 9 in the middle of the conformal curved surface 5 to carry out the parking height adjustment. The mooring cable provides guarantee such as electric power for the ball body, and data information is processed and transmitted.
In practical application, the anchoring platform can be combined with the landform and the geomorphic appearance, can be built into various forms such as a mountain accompanying type, a buried type, a horizontal type and an overhead type, and is mainly used for the erection, anchoring, lifting off and recovering of the captive balloon. The mountain-accompanying type buried type can be selected in mountainous regions, the horizontal type can be selected in ocean island reefs and reefs, and the overhead type can be adopted in submerged reefs, mudflats, wetlands and the like.
The captive balloon anchoring platform can effectively solve the difficulties of use, maintenance and guarantee in regions such as ocean reefs. The application range of the captive balloon is expanded, and the environmental adaptability of the captive balloon is improved. The wind resistance of the ground anchoring of the captive balloon, particularly the resistance to extreme weather, is improved, the construction of the operation and guarantee conditions of the captive balloon when the geographic and topographic conditions are limited is solved, the construction scale of the operation and guarantee conditions of the captive balloon is reduced, and the construction cost is reduced.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solutions of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily think of equivalent modifications or replacements within the technical scope of the present invention, such as the location of the functional components inside the tee 1, such as the spare part chamber 2, the tail storage chamber 8, the lift-off recovery chamber 9, the maintenance chamber 10, etc., is not limited to this embodiment, and can be arranged reasonably, and these modifications or replacements should be covered within the scope of the present invention.
Claims (8)
1. A captive balloon mooring platform, said mooring platform comprising:
the device comprises a ball seat (1), and a spare part chamber (2), an empennage storage chamber (8), a lift-off recovery chamber (9), a maintenance chamber (10) and a plurality of lift-off recovery devices (14) which are arranged in the ball seat; the ball seat (1) is in a trapezoidal shape, a conformal curved surface (5) matched with the lower surface of the balloon is arranged in the middle of the upper surface, and cross arm sliding rails (3), cross arms (6) installed on the cross arm sliding rails (3) and a plurality of upper mooring riggings (4) are arranged on two sides of the upper surface;
the ball seat (1) is provided with a door (11) for entering a maintenance room (10);
a plurality of bottom mooring riggings (15) are arranged at the bottom inside the lift-off recovery chamber (9);
the upper part of the cross arm sliding rail (3) is provided with an upper rail for the sliding of a cross arm (6);
the anchoring platform further comprises a covering plate used for covering the upper part of the conformal curved surface (5), and the upper part of the cross arm sliding rail (3) is provided with an inner side rail used for fixing the covering plate;
the process of erecting the anchoring platform comprises the following steps:
spreading the captive balloon on the conformal curved surface (5); the ball body (7) is inflated through a helium tank in a spare part chamber (2) in the ball seat (1); the cross arm (6) is folded and moves back and forth on the cross arm slide rail (3), and the ball body (7) is fixed to install the tail wing for the captive balloon.
2. A mooring platform according to claim 1, wherein the service chamber (10) is located opposite the spare part chamber (2) or in a forward region of the ball seat (1).
3. A mooring platform as claimed in claim 1, wherein the tail stowage compartment (8) is rearward of the tee (1) or within the spare part compartment (2).
4. A mooring platform as claimed in claim 1, wherein the bottom mooring rigging (15) is a mooring lock, mooring chain or mooring cable.
5. A mooring platform as claimed in claim 1, wherein the upper mooring rigging (4) is a mooring lock, mooring chain or mooring cable.
6. A method of using a captive balloon mooring platform, said mooring platform being as defined in claim 1, said method comprising the steps of, during mooring:
attaching the captive balloon to a conformal curved surface (5) of the ball seat (1); the captive balloon is secured to the mooring platform by cross-over multipoint mooring of upper mooring rigging (4) and lower mooring rigging (15).
7. The method of use of claim 6, wherein said mooring procedure further comprises the steps of: the balloon empennage is detached and stored in an empennage storage chamber (8).
8. The method of use of claim 7, wherein said mooring procedure further comprises the steps of: releasing the air in the sphere (7) enables the sphere (7) to be shriveled and placed in the conformal curved surface (5), and the cover plate is tightly fixed through the cross arm sliding rail (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910037914.8A CN109693806B (en) | 2019-01-15 | 2019-01-15 | Mooring balloon anchoring platform and using method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910037914.8A CN109693806B (en) | 2019-01-15 | 2019-01-15 | Mooring balloon anchoring platform and using method |
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| Publication Number | Publication Date |
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| CN109693806A CN109693806A (en) | 2019-04-30 |
| CN109693806B true CN109693806B (en) | 2022-04-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201910037914.8A Active CN109693806B (en) | 2019-01-15 | 2019-01-15 | Mooring balloon anchoring platform and using method |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN211417567U (en) * | 2020-01-02 | 2020-09-04 | 南京祖航航空科技有限公司 | Airship transferring and mooring device |
| US11685500B2 (en) | 2020-09-16 | 2023-06-27 | Galaxy Unmanned Systems LLC | Unmanned airships, aerostats, and hybrid airship-aerostat systems and methods thereof |
| CN112550657B (en) * | 2020-11-06 | 2022-09-20 | 中国特种飞行器研究所 | Tethered balloon integrated comprehensive operation guarantee platform and use method thereof |
| CN112591070B (en) * | 2020-11-23 | 2022-12-16 | 中国科学院空天信息创新研究院 | Tethered Balloon Mooring Facility Ball Stand and Ball Holder Components |
| USD1002870S1 (en) | 2021-09-16 | 2023-10-24 | Galaxy Unmanned Systems LLC | Hybrid airship-aerostat |
| CN115837960A (en) * | 2022-11-25 | 2023-03-24 | 中国特种飞行器研究所 | High seaworthiness shipborne captive balloon system |
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| US7093790B1 (en) * | 1999-04-16 | 2006-08-22 | John Scott Davidson | Mooring facility for tethered gas balloon |
| CN101898633A (en) * | 2010-04-28 | 2010-12-01 | 湖南航天管理局 | All-in-one anchoring trailer |
| 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 |
| CN106516069A (en) * | 2016-10-25 | 2017-03-22 | 中国电子科技集团公司第三十八研究所 | Mobile anchoring vehicle for withdrawing, releasing and parking of tethered balloon |
| JP2017226254A (en) * | 2016-06-20 | 2017-12-28 | ソフトバンク株式会社 | Captive balloon |
| CN108557051A (en) * | 2018-06-15 | 2018-09-21 | 湖南航天远望科技有限公司 | A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system |
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2019
- 2019-01-15 CN CN201910037914.8A patent/CN109693806B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7093790B1 (en) * | 1999-04-16 | 2006-08-22 | John Scott Davidson | Mooring facility for tethered gas balloon |
| CN101898633A (en) * | 2010-04-28 | 2010-12-01 | 湖南航天管理局 | All-in-one anchoring trailer |
| 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 |
| JP2017226254A (en) * | 2016-06-20 | 2017-12-28 | ソフトバンク株式会社 | Captive balloon |
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| CN109693806A (en) | 2019-04-30 |
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