CN116353812A - Offshore issuing system and method for stratospheric airship - Google Patents
Offshore issuing system and method for stratospheric airship Download PDFInfo
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- CN116353812A CN116353812A CN202310571857.8A CN202310571857A CN116353812A CN 116353812 A CN116353812 A CN 116353812A CN 202310571857 A CN202310571857 A CN 202310571857A CN 116353812 A CN116353812 A CN 116353812A
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- 238000000034 method Methods 0.000 title claims abstract description 27
- 239000001307 helium Substances 0.000 claims abstract description 19
- 229910052734 helium Inorganic materials 0.000 claims abstract description 19
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims abstract description 19
- 239000004744 fabric Substances 0.000 claims description 10
- 238000012360 testing method Methods 0.000 claims description 9
- 239000002775 capsule Substances 0.000 claims description 5
- 239000002360 explosive Substances 0.000 claims description 3
- 230000000977 initiatory effect Effects 0.000 claims description 3
- 230000008054 signal transmission Effects 0.000 claims description 2
- 230000001681 protective effect Effects 0.000 abstract description 4
- 238000004891 communication Methods 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/005—Arrangements for landing or taking-off, e.g. alighting gear
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
- B63B35/50—Vessels or floating structures for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
Abstract
The invention discloses a stratospheric airship offshore issuing system and an offshore issuing method, wherein the stratospheric airship offshore issuing system comprises an airship and a ship for transporting the airship, a helium storage tank is arranged on the ship, a barometer is arranged at an outlet of the helium storage tank, a winch is arranged on one side of the helium storage tank, the winch is connected with one end of a lifting traction rope, the other end of the lifting traction rope is connected with the bottom of the airship, the bottom of the airship is also connected with an issuing traction rope, the other end of the issuing traction rope is connected with a bottom plate of the ship, and protective air bags are arranged on two sides of the winch. The stratospheric airship offshore issuing system and the stratospheric airship offshore issuing method are adopted, large-scale airship libraries are not needed, the issuing work is more convenient, the issuing places are not fixed, the problem that the fixed airship libraries are easy to monitor is solved, and the problems of motorized issuing and rapid deployment of the airship are also solved.
Description
Technical Field
The invention relates to the technical field of offshore release airship, in particular to a stratospheric airship offshore release system and a release method.
Background
When the airship is released, ground facilities such as a ship warehouse are generally needed, and the following problems are mainly caused: firstly, the release of the airship is dependent on a large-scale boat warehouse, and the place of the boat warehouse is fixed and is easy to monitor; secondly, after the airship is issued on the ground, the airship needs to fly to a target area, and can not be deployed quickly due to the low flying speed of the airship; thirdly, the airship is easy to be influenced by rainfall and strong wind at the place of a ship warehouse when being released, and the release window is easy to be limited by weather conditions at a fixed place.
In order to solve the above problems, there is a need to design an airship issuing method that is independent of the airship warehouse, is flexible, concealed, and reaches the target area as soon as possible.
Disclosure of Invention
The invention aims to provide a stratospheric airship offshore issuing system and a stratospheric airship offshore issuing method, which do not need to rely on a large-scale airship warehouse, have more convenient issuing work and unfixed issuing places, solve the problem that a fixed airship warehouse is easy to monitor, and also solve the problems of motorized issuing and rapid deployment of the airship.
The invention provides a stratospheric airship offshore release system and a release method, and the stratospheric airship offshore release system comprises an airship and a ship for transporting the airship, wherein a helium storage tank is arranged on the ship, a barometer is arranged at an outlet of the helium storage tank, a winch is arranged on one side of the helium storage tank, the winch is connected with one end of a lifting traction rope, the other end of the lifting traction rope is connected with the bottom of the airship, the bottom of the airship is also connected with a release traction rope, the other end of the release traction rope is connected with a bottom plate of the ship, and protective airbags are arranged on two sides of the winch.
Preferably, two lifting haulage ropes are arranged, a first tying point is arranged on the lifting haulage ropes, one lifting haulage rope is arranged on the releasing haulage rope, and a second tying point is arranged on the releasing haulage rope.
The invention also provides a stratospheric airship offshore issuing method, which comprises the following steps:
s1, performing assembly and test work on a ship by the airship, and protecting the whole airship to avoid the influence of offshore environment, wherein the ship is in a standby state;
s2, after receiving a departure command, carrying the airship by the ship to a target area, and meanwhile, researching, judging and selecting an optimal airship issuing point; after reaching the release point, the ship monitors the offshore wind speed in real time, and adjusts the direction of the ship in real time according to the wind direction, so that the wind direction is blown to the head of the airship from the tail of the airship, and simultaneously adjusts the navigational speed in real time, so that the wind speed is consistent with the advancing speed of the ship;
s3, after meeting the release conditions, the winch releases the lifting traction rope to be connected with the bottom of the airship, the bottom of the airship is connected with the release traction rope, then a helium storage tank is opened to rapidly charge helium into the airship until the designed inflation amount is reached, and the head of the airship is in a vertical state and is controlled by traction of the winch;
s4, after the issuing command is obtained, the winch releases the lifting traction rope, the airship is gradually lifted under the action of buoyancy until the airship is tethered by the tail issuing traction rope, and the buoyancy is completely transferred to the issuing traction rope; in the process, the winch can also release the lifting traction rope and move towards the tail of the ship, so that the airship is controlled to lift;
s5, after confirming that the state of the airship is normal, the remote control cutting device sequentially releases the constraint ropes of the first mooring point and the second mooring point, and the airship releases and lifts off in a non-forming mode.
Preferably, in step S1, developing the final assembly specifically includes: the bag body is unfolded and a boat-mounted part is installed;
after the assembly is completed, testing work is carried out, wherein the testing work comprises the step of electrifying and detecting the on-board components and the step of detecting signal transmission.
Preferably, in step S1, the protection is specifically: the waterproof cloth is paved at the bottom of the airship in advance, and after the assembly is completed, the whole airship is covered by the waterproof cloth from the upper part of the airship and is sealed with the waterproof cloth at the bottom through a zipper.
Preferably, in step S2, the wind speed of the optimal airship issuing point is less than 3m/S, and no rainfall exists.
Preferably, in the step S3, the release condition is that the wind speed is less than 3m/S and no rainfall exists.
Preferably, in step S5, the airship is in a normal state, which means that the upper parts and the electric appliances of the airship can work normally, and the capsule body is not damaged.
Preferably, in step S5, the remote control cutting device is installed on the lifting traction rope at one end of the airship and the upper part of the releasing traction rope, and the remote control cutting device is one of an initiating explosive device separator and a mechanical separator.
Therefore, the invention adopts the above-mentioned stratospheric airship offshore issuing system and the issuing method, and has the following technical effects:
(1) The airship is transported by the ship, and works such as assembly, detection, protection and the like are carried out on the ship, so that a large-scale ship warehouse is not needed, and the issuing work is more convenient.
(2) The airship is distributed on the sea, the distribution area can be selected according to the actual weather condition, the distribution place is not fixed, and the problem that the fixed airship warehouse is easy to monitor is solved.
(3) The airship can be brought to a designated area for release, and the problems of maneuvering release and quick deployment of the airship are solved.
(4) The problem that a plurality of airships can be issued at the same time is solved.
The technical scheme of the invention is further described in detail through the drawings and the embodiments.
Drawings
FIG. 1 is a system layout diagram of a stratospheric airship marine dispensing system according to the invention;
fig. 2 is an offshore airship release diagram of a stratospheric airship release system and a release method according to the invention.
Reference numerals
1. An airship; 2. a watercraft; 3. a helium storage tank; 4. a hoist; 5. lifting the traction rope; 6. dispensing a traction rope; 7. a protective airbag; 8. a first tie-up point; 9. the second is a point.
Detailed Description
The technical scheme of the invention is further described below through the attached drawings and the embodiments.
Unless defined otherwise, technical or scientific terms used herein should be given the ordinary meaning as understood by one of ordinary skill in the art to which this invention belongs.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.
Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art. Such other embodiments are also within the scope of the present invention.
It should also be understood that the above-mentioned embodiments are only for explaining the present invention, the protection scope of the present invention is not limited thereto, and any person skilled in the art should be able to cover the protection scope of the present invention by equally replacing or changing the technical scheme and the inventive concept thereof within the scope of the present invention.
Techniques, methods, and apparatus known to one of ordinary skill in the relevant art may not be discussed in detail, but are intended to be considered part of the specification where appropriate.
The disclosures of the prior art documents cited in the present specification are incorporated by reference in their entirety into the present invention and are therefore part of the present disclosure.
Example 1
As shown in the figure, the stratospheric airship offshore release system comprises an airship 1 and a ship 2 for transporting the airship 1, wherein a helium storage tank 3 is arranged on the ship 2, a barometer is arranged at the outlet of the helium storage tank 3, a winch 4 is arranged on one side of the helium storage tank 3, the winch 4 is connected with one end of a lifting traction rope 5, the other end of the lifting traction rope 5 is connected with the bottom of the airship 1, the bottom of the airship 1 is further connected with a release traction rope 6, the other end of the release traction rope 6 is connected with the bottom plate of the ship 2, and protective airbags 7 are arranged on two sides of the winch 4. When there is wind, mainly there is side wind, the bag body will scratch the ship board, and the protection air bag 7 plays the protection role.
The lifting haulage rope 5 is provided with two, is provided with first tie-up point 6 on the lifting haulage rope 5, and the release haulage rope 6 is provided with one, is provided with second tie-up point 9 on the release haulage rope 6.
The invention also provides a stratospheric airship offshore issuing method, which comprises the following steps:
s1, performing assembly and test work on a ship by the airship, and protecting the whole airship to avoid the influence of offshore environment, wherein the ship is in a standby state;
developing the final assembly specifically comprises: the bag body is unfolded, a boat-mounted part is arranged, and a traction rope is connected and released and the traction rope is lifted;
and (3) expanding the bag body: the bag body material is flexible composite cloth, is in a streamline shape like a water drop, has a size of more than hundred meters and a width of more than twenty meters, and is usually required to be folded and packed into a smaller size (the length is less than 20 m) after the bag body is processed so as to be convenient to transport. After the capsule is in place, the capsule is fully unfolded.
Mounting a boat-mounted part: the bag body is provided with an interface for installing components, and the components to be installed comprise a gas release valve, beidou communication, a solar cell panel, an energy storage battery, a propulsion propeller, an avionic and measurement and control nacelle, a mission nacelle, an electrified communication cable and the like.
After the assembly is completed, testing work is carried out, and the testing work specifically comprises the following steps: after the installation is completed, whether each component is normally electrified and works or not is tested, and whether signals are normally transmitted or not is tested.
The protection is specifically as follows: the waterproof cloth is paved at the bottom of the airship in advance, the whole airship is covered by the waterproof cloth from the upper part of the airship after the assembly is completed, and the waterproof cloth at the bottom is sealed by a zipper.
S2, after receiving the departure command, the ship carries the airship to go to the target area, and meanwhile, the optimal airship issuing point is researched, judged and selected. The wind speed of the optimal airship release point is less than 3m/s, and no rainfall exists. After reaching the release point, the ship monitors the offshore wind speed in real time, and adjusts the direction of the ship in real time according to the wind direction, so that the wind direction is blown to the head of the airship from the tail of the airship, and simultaneously adjusts the navigational speed in real time, so that the wind speed is consistent with the advancing speed of the ship;
s3, after meeting the release conditions, the release conditions are that the wind speed is less than 3m/S and no rainfall exists. The lifting traction rope is released from the winch to be connected with the airship, and the airship is connected with the releasing traction rope. Opening a helium storage tank to rapidly fill helium into the airship until the designed inflation amount is reached, wherein the head of the airship is in a vertical state and is traction-controlled by a winch;
s4, after the issuing command is obtained, the winch releases the lifting traction rope, the airship is gradually lifted under the action of the buoyancy force until the airship is tethered by the tail issuing traction rope, and the buoyancy force is completely transferred to the issuing traction rope, so that the lifting traction rope is not stressed.
In the process, the winch can move to the tail part while releasing the rope, so as to control the airship to lift.
If the state of the airship is abnormal in the process, the winch can be reversely operated, and the airship is restored to the state of the step S3.
S5, confirming that the upper parts and the electric appliances of the airship can work normally, and after the capsule body is not damaged. The remote control cutting device sequentially releases the first mooring point and the second mooring point to restrict the rope, and the airship releases the lift-off in a non-forming mode.
The remote control cutting device is arranged on the lifting traction rope at one end of the airship and the upper part for releasing the traction rope, and is one of an initiating explosive device separator and a mechanical separator.
Therefore, the stratospheric airship offshore issuing system and the stratospheric airship offshore issuing method are adopted, the airship is transported by a ship, and the works such as assembly, detection and protection are carried out on the ship, so that a large-scale airship warehouse is not needed, and the issuing work is more convenient; the airship is distributed on the sea, the distribution area can be selected according to the actual weather condition, the distribution place is not fixed, and the problem that a fixed airship warehouse is easy to monitor is solved; the airship can be brought to a designated area for release, so that the problem of maneuvering release and quick deployment of the airship is solved; the problem that a plurality of airships can be issued at the same time is solved.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present invention and not for limiting it, and although the present invention has been described in detail with reference to the preferred embodiments, it will be understood by those skilled in the art that: the technical scheme of the invention can be modified or replaced by the same, and the modified technical scheme cannot deviate from the spirit and scope of the technical scheme of the invention.
Claims (9)
1. An offshore stratospheric airship issuing system, characterized in that: including the airship and be used for transporting the ship of airship, be provided with the helium storage tank on the ship, the exit of helium storage tank is provided with the barometer, one side of helium storage tank is provided with the hoist engine, the hoist engine is connected with the one end of lifting haulage rope, the other end and the airship bottom of lifting haulage rope link to each other, the airship bottom still is connected with the release haulage rope, the other end and the ship bottom plate of release haulage rope link to each other, the hoist engine both sides are provided with protection gasbag.
2. An offshore stratospheric airship issuing system according to claim 1, wherein: the lifting haulage rope is provided with two, be provided with first tie point on the lifting haulage rope, the release haulage rope is provided with one, be provided with the second tie point on the release haulage rope.
3. An offshore release method of a stratospheric airship is characterized in that: the method comprises the following steps:
s1, performing assembly and test work on a ship by the airship, and protecting the whole airship to avoid the influence of offshore environment, wherein the ship is in a standby state;
s2, after receiving a departure command, carrying the airship by the ship to a target area, and meanwhile, researching, judging and selecting an optimal airship issuing point; after reaching the release point, the ship monitors the offshore wind speed in real time, and adjusts the direction of the ship in real time according to the wind direction, so that the wind direction is blown to the head of the airship from the tail of the airship, and simultaneously adjusts the navigational speed in real time, so that the wind speed is consistent with the advancing speed of the ship;
s3, after meeting the release conditions, the winch releases the lifting traction rope to be connected with the bottom of the airship, the bottom of the airship is connected with the release traction rope, then a helium storage tank is opened to rapidly charge helium into the airship until the designed inflation amount is reached, and the head of the airship is in a vertical state and is controlled by traction of the winch;
s4, after the issuing command is obtained, the winch releases the lifting traction rope, the airship is gradually lifted under the action of buoyancy until the airship is tethered by the tail issuing traction rope, and the buoyancy is completely transferred to the issuing traction rope; in the process, the winch can also release the lifting traction rope and move towards the tail of the ship, so that the airship is controlled to lift;
s5, after confirming that the state of the airship is normal, the remote control cutting device sequentially releases the constraint ropes of the first mooring point and the second mooring point, and the airship releases and lifts off in a non-forming mode.
4. A stratospheric airship marine dispensing method as recited in claim 3, wherein: in step S1, developing the final assembly specifically includes: the bag body is unfolded and a boat-mounted part is installed;
after the assembly is completed, testing work is carried out, wherein the testing work comprises the step of electrifying and detecting the on-board components and the step of detecting signal transmission.
5. A stratospheric airship marine dispensing method as recited in claim 3, wherein: in step S1, the protection specifically includes: the waterproof cloth is paved at the bottom of the airship in advance, and after the assembly is completed, the whole airship is covered by the waterproof cloth from the upper part of the airship and is sealed with the waterproof cloth at the bottom through a zipper.
6. A stratospheric airship marine dispensing method as recited in claim 3, wherein: in the step S2, the wind speed of the optimal airship issuing point is less than 3m/S, and no rainfall exists.
7. A stratospheric airship marine dispensing method as recited in claim 3, wherein: in the step S3, the release condition is that the wind speed is less than 3m/S and no rainfall exists.
8. A stratospheric airship marine dispensing method as recited in claim 3, wherein: in step S5, the airship is in a normal state, namely the upper parts of the airship and the electric appliances can work normally, and the capsule body is not damaged.
9. A stratospheric airship marine dispensing method as recited in claim 3, wherein: in step S5, the remote control cutting device is arranged on the lifting traction rope at one end of the airship and the upper part for releasing the traction rope, and is one of an initiating explosive device separator and a mechanical separator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310571857.8A CN116353812A (en) | 2023-05-22 | 2023-05-22 | Offshore issuing system and method for stratospheric airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310571857.8A CN116353812A (en) | 2023-05-22 | 2023-05-22 | Offshore issuing system and method for stratospheric airship |
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| CN116353812A true CN116353812A (en) | 2023-06-30 |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108032985A (en) * | 2017-12-05 | 2018-05-15 | 哈尔滨工程大学 | Kite balloon airship system based on the comprehensive monitoring of marine desired target area |
| CN108128437A (en) * | 2017-11-22 | 2018-06-08 | 北京天恒长鹰科技股份有限公司 | Dirigible lets system fly away and dirigible lets method fly away |
| CN108163179A (en) * | 2017-12-06 | 2018-06-15 | 湖南航天远望科技有限公司 | A kind of near space aerostatics distribution method and dispensing apparatus |
| US20180237141A1 (en) * | 2011-06-13 | 2018-08-23 | Stephen B. Heppe | Airship launch from a cargo airship with a payload return vehicle |
| CN112537433A (en) * | 2020-12-11 | 2021-03-23 | 中国人民解放军63660部队 | Top open-close type offshore aerostat flying platform |
| CN114476994A (en) * | 2021-12-28 | 2022-05-13 | 中国特种飞行器研究所 | Novel offshore independent winch winding and unwinding system |
-
2023
- 2023-05-22 CN CN202310571857.8A patent/CN116353812A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180237141A1 (en) * | 2011-06-13 | 2018-08-23 | Stephen B. Heppe | Airship launch from a cargo airship with a payload return vehicle |
| CN108128437A (en) * | 2017-11-22 | 2018-06-08 | 北京天恒长鹰科技股份有限公司 | Dirigible lets system fly away and dirigible lets method fly away |
| CN108032985A (en) * | 2017-12-05 | 2018-05-15 | 哈尔滨工程大学 | Kite balloon airship system based on the comprehensive monitoring of marine desired target area |
| CN108163179A (en) * | 2017-12-06 | 2018-06-15 | 湖南航天远望科技有限公司 | A kind of near space aerostatics distribution method and dispensing apparatus |
| CN112537433A (en) * | 2020-12-11 | 2021-03-23 | 中国人民解放军63660部队 | Top open-close type offshore aerostat flying platform |
| CN114476994A (en) * | 2021-12-28 | 2022-05-13 | 中国特种飞行器研究所 | Novel offshore independent winch winding and unwinding system |
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