CN109204770A - The patch system and method for repairing and mending of aerostatics utricule - Google Patents
The patch system and method for repairing and mending of aerostatics utricule Download PDFInfo
- Publication number
- CN109204770A CN109204770A CN201710521763.4A CN201710521763A CN109204770A CN 109204770 A CN109204770 A CN 109204770A CN 201710521763 A CN201710521763 A CN 201710521763A CN 109204770 A CN109204770 A CN 109204770A
- Authority
- CN
- China
- Prior art keywords
- utricule
- damaged
- aerostatics
- repair
- damaged area
- Prior art date
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Links
- 238000000034 method Methods 0.000 title claims abstract description 15
- 230000008439 repair process Effects 0.000 claims abstract description 74
- 239000007788 liquid Substances 0.000 claims abstract description 56
- 238000012360 testing method Methods 0.000 claims abstract description 22
- 238000000889 atomisation Methods 0.000 claims description 18
- 230000008859 change Effects 0.000 claims description 18
- 238000012545 processing Methods 0.000 claims description 12
- 238000005259 measurement Methods 0.000 claims description 6
- 230000009471 action Effects 0.000 claims description 5
- 239000003595 mist Substances 0.000 claims description 4
- 238000005086 pumping Methods 0.000 claims description 4
- 238000009688 liquid atomisation Methods 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims description 2
- 238000001802 infusion Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 abstract description 13
- 239000001307 helium Substances 0.000 abstract description 8
- 229910052734 helium Inorganic materials 0.000 abstract description 8
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 abstract description 8
- 239000002775 capsule Substances 0.000 description 12
- 239000000463 material Substances 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
-
- 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Abstract
This application discloses the patch system and method for repairing and mending of a kind of aerostatics utricule, which includes: pressure test device, multiple atmospheric pressure values of multiple air pressure mouths for obtaining utricule;Control device is electrically connected to pressure test device, judges whether utricule is damaged according to multiple atmospheric pressure values;Multiple atomising devices are electrically connected to control device, and each atomising device includes atomizing mouth, and atomizing mouth is set on the inner surface of utricule and is arranged respectively close to corresponding air pressure mouth;Control device locks the damaged area of utricule by multiple atmospheric pressure values, and corresponding atomizing mouth is driven to be atomized to repair utricule repair liquid.The damaged area of utricule is detected by pressure test device, and controls atomising device and repair liquid is atomized to repair utricule;It can be realized utricule auto-mending, time saving and energy saving, greatly save cost it is not necessary that aerostatics is dropped to ground, does not need more to bleed off utricule helium gas inside and repair, ensure that aerostatics stablizes stagnant sky.
Description
Technical field
This application involves aerostatics technical fields, it particularly relates to a kind of patch system of aerostatics utricule and repairing
Method.
Background technique
Aerostatics generally refers to aircraft that specific gravity is lighter than air, going up to the air by atmospheric buoyancy force.When aerostatics utricule goes out
Now due to various reasons caused by capsule skin breakage when, current method for repairing and mending be need to drop to aerostatics ground carry out it is artificial
Repairing;If damaged mouth is located at the top of aerostatics, it is also necessary to gas valve be opened, the intracorporal helium of capsule is released, utricule is drawn
It is repaired to ground.
But the shortcomings that current method for repairing and mending, is when being that air bag is damaged more when artificial discovery is damaged;Secondly, once
It was found that damaged carry out manual repair it is necessary to which aerostatics is dropped to ground, the time generally repaired is all long, and cost is unusual
It is high;Again, no matter capsule skin breakage size, require manually to be repaired, also need to bleed off the intracorporal helium of capsule when necessary.
Not only time-consuming and laborious, costs are largely repaired in also waste helium, waste.
For no matter capsule skin breakage size requires to drop to aerostatics into ground progress manual repair in the related technology
Problem, currently no effective solution has been proposed.
Summary of the invention
In view of the above problems in the related art, the application proposes patch system and the repairing side of a kind of aerostatics utricule
Method, can be when utricule breakage be serious, it is not necessary that aerostatics is dropped to ground, so that it may realize auto-mending utricule, significantly
Manpower and material resources are saved, guarantee aerostatics stablizes stagnant sky.
The technical solution of the application is achieved in that
According to the one aspect of the application, a kind of patch system of aerostatics utricule is provided, comprising:
Pressure test device, multiple atmospheric pressure values of multiple air pressure mouths for obtaining utricule;
Control device, is electrically connected to pressure test device, and control device judges whether utricule is damaged according to multiple atmospheric pressure values;
And
Multiple atomising devices are electrically connected to control device, and each atomising device includes atomizing mouth, and atomizing mouth is set to capsule
It is arranged on the inner surface of body and respectively close to corresponding air pressure mouth;
Wherein, control device locks the damaged area of utricule by multiple atmospheric pressure values, and drives damaged area corresponding
Atomizing mouth is atomized to repair utricule repair liquid.
In one embodiment, control device includes: processing chip, and processing chip is electrically connected with pressure test device, is located
It manages chip and judges air pressure change speed according to multiple atmospheric pressure values, and according to the damaged journey of air pressure change velocity estimated damaged area
Degree.
Wherein, control device further include: the control chip being electrically connected with processing chip controls chip according to damaged degree control
Fogging degree of the atomizing mouth processed to repair liquid;Wherein, processing chip judges the more big then atomizing mouth of damaged degree to the mist of repair liquid
Change degree is lower.
In one embodiment, control chip is electrically connected with atomizing mouth, and control atomizing mouth is atomized repair liquid, and makes
Repair liquid floats near damaged area, and the repair liquid after atomization is coated on damage zone under the action of the draught head of damaged area
Domain, to repair damaged utricule.
In one embodiment, the patch system of aerostatics utricule further comprises multiple pneumatic tubes, multiple pneumatic tubes
One end is connected with multiple air pressure mouths respectively, and the opposite other end of multiple pneumatic tubes is connect to detect multiple gas with pressure test device
Pressure value.
In one embodiment, further includes: repairing liquid container is set in the gondola of aerostatics, repairing liquid container and more
A atomising device is connected to provide repair liquid.
Wherein, atomising device further includes motor, is set in the gondola of aerostatics and is connect by hose with atomizing mouth,
Motor is for pumping repair liquid to atomizing mouth to be atomized.
In one embodiment, control device includes the Measurement &control computer being set in the gondola of aerostatics.
Wherein, pressure test device is integrated in Measurement &control computer.
According to the another aspect of the application, a kind of method for repairing and mending of aerostatics utricule is provided, comprising:
Obtain multiple atmospheric pressure values of multiple air pressure mouths of utricule;
Judge whether utricule is damaged according to multiple atmospheric pressure values;And
Determine that utricule is damaged and locks damaged area, the corresponding atomising device in driving damaged area carries out mist to repair liquid
Change, the utricule of repair liquid auto-mending breakage under the pressure difference of damaged area after atomization.
In one embodiment, judge whether utricule is damaged, specifically includes according to multiple atmospheric pressure values: based on multiple atmospheric pressure values
Air pressure change speed judge the damaged degree of damaged area.
In one embodiment, the corresponding atomising device in driving damaged area is atomized repair liquid, specifically includes: root
Corresponding atomising device is controlled according to damaged degree and carries out different degrees of atomization, and the more big then fogging degree of damaged degree is lower.
In one embodiment, the utricule damaged by the repair liquid repairing after atomization, specifically includes: after control atomization
Repair liquid floats near damaged area, damaged area is coated under the action of the draught head of damaged area, to repair breakage
Utricule.
The patch system of the aerostatics utricule of the application, control device detect the damage zone of utricule by pressure test device
Domain, and control atomising device and repair liquid is atomized to repair utricule;In utricule by breakage initiation gas leakage and damaged not tight
It can be realized utricule auto-mending when weight, even if utricule breakage is located at utricule top, drop to ground, more without by aerostatics
It does not need to bleed off utricule helium gas inside and be repaired, it is time saving and energy saving, greatly save cost, it ensure that stablizing for aerostatics is stagnant
It is empty.
Detailed description of the invention
In order to illustrate the technical solutions in the embodiments of the present application or in the prior art more clearly, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the application
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the schematic diagram according to the patch system of the aerostatics utricule of the embodiment of the present application;
Fig. 2 is the flow chart according to the method for repairing and mending of the aerostatics utricule of the embodiment of the present application.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present application, technical solutions in the embodiments of the present application carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of embodiments of the present application, instead of all the embodiments.It is based on
Embodiment in the application, those of ordinary skill in the art's every other embodiment obtained belong to the application protection
Range.
As shown in Figure 1, according to the patch system of the aerostatics utricule of the embodiment of the present application include: pressure test device (not
Show), control device 10 and multiple atomising devices 40;Wherein, pressure test device, for obtaining multiple gas of utricule 50
Press multiple atmospheric pressure values of mouth 30;Control device 10, is electrically connected to pressure test device, and control device 10 is sentenced according to multiple atmospheric pressure values
Whether disconnected utricule 50 is damaged;Multiple atomising devices 40, are electrically connected to control device 10, and each atomising device 40 includes atomization
Mouth, atomizing mouth are set on the inner surface of utricule 50 and are arranged respectively close to corresponding air pressure mouth 30;Wherein, control device
10 lock the damaged area of utricule 50 by multiple atmospheric pressure values, and the corresponding atomizing mouth in damaged area is driven to carry out repair liquid
Atomization is to repair utricule 50.
Wherein, the atmospheric pressure value size of utricule is detected by the pressure test device being connected with control device 10, and is passed through
The processing of control device 10, in the case where utricule is on-inflatable or non-deflation, if detecting any one or any number of gas
Press the atmospheric pressure value of mouth 30 abnormal, then control device 10 judges that utricule is damaged and can lock the damaged area of utricule.
Above-mentioned technical proposal, control device 10 being capable of quick lock in capsules by multiple atmospheric pressure values that pressure test device obtains
The damaged area of body, and control corresponding atomizing mouth and repair liquid is atomized to repair utricule;Leakage is caused by breakage in utricule
Gas simultaneously can be realized utricule auto-mending when damaged not serious, even if utricule breakage is located at utricule top, without by floating
Device drops to ground, does not need more to bleed off utricule helium gas inside and be repaired, time saving and energy saving, greatly save cost, guarantees
Aerostatics stablizes stagnant sky.
Wherein, it is made of for repairing the repair liquid of utricule a variety of high-molecular compounds, configures, have for capsule skin material
Higher heat resistance, wearability, water resistance, air-tightness and excellent adhesive property, and corrosiveness will not be generated to capsule skin, and
It is easy to be atomized.Just capsule skin will not be injured in mending course in this way, reach better repair efficiency, it can also be with daily maintenance capsule
Skin keeps the toughness of capsule skin.
In some embodiments, the patch system of the aerostatics utricule of the application further comprises multiple pneumatic tubes, this is more
One end of a pneumatic tube is connected with multiple air pressure mouths 30 respectively, and the opposite other end of multiple pneumatic tube and pressure test device connect
It connects to detect multiple atmospheric pressure values.
In one embodiment, control device 10 includes processing chip (not shown), handles chip and pressure test device
Electrical connection handles chip according to multiple atmospheric pressure values and judges air pressure change speed, and according to air pressure change velocity estimated damaged area
Damaged degree.For example, the air pressure change speed of atmospheric pressure value then can determine whether that damaged degree is relatively large fastly, the air pressure change of atmospheric pressure value
Speed then can determine whether that damaged degree is relatively small slowly.
Wherein, control device 10 further include with the control chip (not shown) that be electrically connected of processing chip, control chip according to
Damaged degree controls atomizing mouth to the fogging degree of repair liquid;Wherein, processing chip judges the more big then atomizing mouth pair of damaged degree
The fogging degree of repair liquid is lower.Angle is changed to say, that is to say, that damaged degree is larger, need the repair liquid of higher concentration into
Row repairing, and repair liquid concentration is also larger if fogging degree is lower.In the present embodiment, control device 10 can be according to air pressure
The air pressure change velocity estimated utricule breakage of mouth, and atomising device 40 is controlled to the fogging degree of repair liquid.Work as damage zone
When domain area is more small, fogging degree is answered relatively large;When damaged area area is larger, fogging degree answer it is relatively low, from
And guarantee to repair utricule breakage completely.
Specifically, refering to what is shown in Fig. 1, when control device 10 judges utricule breakage and has locked the damaged area of utricule,
Control device 10 can drive the atomizing mouth of atomising device 40 corresponding with the damaged area, so that repair liquid is drawn into atomization
Device is simultaneously atomized atomizing mouth to repair liquid;Air pressure change speed of the control device 10 also according to the air pressure mouth 30 of pressure abnormity
Degree judges utricule breakage, controls the fogging degree of atomising device 40: when damaged area area is more small, fogging degree
Greatly;When damaged area area is more larger, fogging degree is low;To guarantee to repair utricule breakage completely.
In one embodiment, control chip is electrically connected with atomizing mouth, and control atomizing mouth is atomized repair liquid, and makes
Repair liquid floats near damaged area, and the repair liquid after atomization is coated on damage zone under the action of the draught head of damaged area
Domain, to repair damaged utricule 50.Specifically, after due to utricule breakage, the draught head inside and outside utricule can make inside utricule
Gas (such as helium) leaks out outward;And repair liquid is in the state that diffuses after atomization in utricule, therefore reveals
Gas the repair liquid after atomization can be coated on damaged area while to outward leakage, thus realize to utricule automatically repairing
It mends.
In one embodiment, atomising device 40 further includes motor (not shown), and motor is set to the gondola 60 of aerostatics
Interior and connect with atomizing mouth by hose 41, which, which can be used for repair liquid passing through hose 41, pumps to atomizing mouth to carry out
Atomization.Specifically, atomising device 40 can be operated based on the control of control device 10, driving motor pumping repair liquid to mist
Change mouth, and then repair liquid is atomized by atomizing mouth.
As shown in Figure 1, in the present embodiment, the patch system of the aerostatics utricule of the application further include: repairing liquid container
20, which is set in the gondola 60 of aerostatics, repairing liquid container 20 be connected with above-mentioned multiple atomising devices with
Repair liquid is provided.
In the present embodiment, atomising device further includes motor, and motor is set in the gondola 60 of aerostatics and passes through hose
It is connect with atomizing mouth, motor is for pumping repair liquid to atomizing mouth to be atomized.
In the present embodiment, control device 10 is the Measurement &control computer being set in the gondola 60 of aerostatics.It should be appreciated that
Control device is also possible to be realized by other suitable hardware and/or software.
Wherein, pressure test device can be integrated in Measurement &control computer.
As shown in Fig. 2, according to an embodiment of the present application, a kind of method for repairing and mending of aerostatics utricule is additionally provided, including with
Lower step:
S12 obtains multiple atmospheric pressure values of multiple air pressure mouths of utricule;
S14 judges whether utricule is damaged according to multiple atmospheric pressure values;And
S16 determines that utricule is damaged and locks damaged area, and the corresponding atomising device in driving damaged area carries out repair liquid
Atomization passes through the utricule that the repair liquid repairing after atomization is damaged.
Above-mentioned technical proposal is capable of the damaged area of quick lock in utricule, and driving pair by multiple atmospheric pressure values of acquisition
The atomizing mouth answered is atomized to repair utricule repair liquid;Gas leakage and energy when damaged not serious are caused by breakage in utricule
Utricule auto-mending is enough realized, even if utricule breakage is located at utricule top, without aerostatics is dropped to ground, is not needed more
It bleeds off utricule helium gas inside to be repaired, time saving and energy saving, greatly save cost, ensure that aerostatics stablizes stagnant sky.
Wherein, judge whether utricule is damaged, specifically includes according to multiple atmospheric pressure values at step S12: based on multiple air pressures
The air pressure change speed of value judges the damaged degree of damaged area.
Further, the corresponding atomising device in damaged area is driven to be atomized repair liquid at step S16, it is specific to wrap
It includes: controlling the fogging degree of corresponding atomising device according to damaged degree.Wherein, the more big then fogging degree of damaged degree is lower.
In the present embodiment, can be according to the air pressure change velocity estimated utricule breakage of air pressure mouth, and atomising device is controlled to repairing
The fogging degree of fluid infusion.When damaged area area is more small, fogging degree is answered relatively large;When damaged area, area is larger
When, fogging degree answer it is relatively low, to guarantee to repair utricule breakage completely.
Further, specifically included at step S16 by the damaged utricule of the repair liquid repairing after atomization: control is atomized
Repair liquid afterwards floats near damaged area, is coated on damaged area under the action of the draught head of damaged area, with repairing
Damaged utricule.Without drive system especially, the pressure difference that will appear using damaged area itself, air-flow is acted in pressure difference
Under flowed from inside to outside by utricule, swim in the repair liquid near damaged area with the flowing of air-flow and even spread is to damage zone
Auto-mending utricule is realized in domain.
The foregoing is merely the preferred embodiments of the application, not to limit the application, all essences in the application
Within mind and principle, any modification, equivalent replacement, improvement and so on be should be included within the scope of protection of this application.
Claims (13)
1. a kind of patch system of aerostatics utricule characterized by comprising
Pressure test device, multiple atmospheric pressure values of multiple air pressure mouths for obtaining utricule;
Control device is electrically connected to the pressure test device, and the control device is according to the judgement of the multiple atmospheric pressure value
Whether utricule is damaged;And
Multiple atomising devices are electrically connected to the control device, and each atomising device includes atomizing mouth, the atomizing mouth setting
It is arranged on the inner surface of the utricule and respectively close to the corresponding air pressure mouth;
Wherein, the control device locks the damaged area of the utricule by the multiple atmospheric pressure value, and drives described broken
The corresponding atomizing mouth in damage region is atomized repair liquid to repair the utricule.
2. the patch system of aerostatics utricule according to claim 1, which is characterized in that the control device includes:
Chip is handled, the processing chip is electrically connected with the pressure test device, and the processing chip is according to the multiple gas
Pressure value judges air pressure change speed, and the damaged degree of the damaged area according to the air pressure change velocity estimated.
3. the patch system of aerostatics utricule according to claim 2, which is characterized in that the control device further include:
The control chip being electrically connected with the processing chip, the control chip control the atomizing mouth to institute according to the damaged degree
State the fogging degree of repair liquid;
Wherein, the processing chip judges that the more big then described atomizing mouth of damaged degree is lower to the fogging degree of the repair liquid.
4. the patch system of aerostatics utricule according to claim 3, which is characterized in that the control chip and the mist
Change mouth electrical connection, the repair liquid after control atomization floats near the damaged area, the air pressure in the damaged area
The damaged area is coated under the action of difference, to repair the damaged utricule.
5. the patch system of aerostatics utricule according to claim 1, which is characterized in that
The patch system of the aerostatics utricule further comprises multiple pneumatic tubes, one end of the multiple pneumatic tube respectively with institute
It states multiple air pressure mouths to be connected, the opposite other end of the multiple pneumatic tube connect described more to detect with the pressure test device
A atmospheric pressure value.
6. the patch system of aerostatics utricule according to claim 1, which is characterized in that further include:
Liquid container is repaired, is set in the gondola of aerostatics, the repairing liquid container is connected with the multiple atomising device to mention
For the repair liquid.
7. the patch system of aerostatics utricule according to claim 6, which is characterized in that
The atomising device further includes motor, is set in the gondola of aerostatics and is connect by hose with the atomizing mouth, institute
Motor is stated for pumping the repair liquid to the atomizing mouth to be atomized.
8. the patch system of aerostatics utricule according to claim 1, which is characterized in that
The control device includes the Measurement &control computer being set in the gondola of aerostatics.
9. the patch system of aerostatics utricule according to claim 8, which is characterized in that the pressure test device is integrated
In the Measurement &control computer.
10. a kind of method for repairing and mending of aerostatics utricule characterized by comprising
Obtain multiple atmospheric pressure values of multiple air pressure mouths of utricule;
Judge whether the utricule is damaged according to the multiple atmospheric pressure value;And
It determines that the utricule is damaged and locks damaged area, the corresponding atomising device in the damaged area is driven to carry out repair liquid
Atomization passes through the utricule that the repair liquid repairing after atomization is damaged.
11. the method for repairing and mending of aerostatics utricule according to claim 10, which is characterized in that according to the multiple atmospheric pressure value
Judge whether the utricule is damaged, specifically includes:
The damaged degree of the damaged area is judged based on the air pressure change speed of multiple atmospheric pressure values.
12. the method for repairing and mending of aerostatics utricule according to claim 11, which is characterized in that drive the damaged area pair
The atomising device answered is atomized repair liquid, specifically includes:
The corresponding atomising device is controlled according to damaged degree and carries out different degrees of atomization, and the damaged degree the big, is atomized journey
It spends lower.
13. the method for repairing and mending of aerostatics utricule according to claim 11, which is characterized in that by atomization after described in repair
The damaged utricule of fluid infusion repairing, specifically includes:
The repair liquid after control atomization floats near the damaged area, in the effect of the draught head of the damaged area
Under be coated on the damaged area, to repair the damaged utricule.
Priority Applications (1)
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CN201710521763.4A CN109204770B (en) | 2017-06-30 | 2017-06-30 | Repairing system and repairing method for aerostat capsule |
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CN201710521763.4A CN109204770B (en) | 2017-06-30 | 2017-06-30 | Repairing system and repairing method for aerostat capsule |
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CN109204770B CN109204770B (en) | 2024-02-23 |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001031200A (en) * | 1999-07-26 | 2001-02-06 | Agency Of Ind Science & Technol | Method and apparatus for sensing gas leakage of airship |
US20130126675A1 (en) * | 2011-11-23 | 2013-05-23 | Stratospheric Airships, Llc | Durable airship hull and in situ airship hull repair |
CN104023956A (en) * | 2011-10-11 | 2014-09-03 | 横滨橡胶株式会社 | Puncture repair fluid injection method and injection device |
CN105438160A (en) * | 2014-08-22 | 2016-03-30 | 杨洋 | Hovercraft air bag capable of being automatically repaired |
CN106347620A (en) * | 2016-10-12 | 2017-01-25 | 郭鹏 | Vacuum type buoyancy flight device based on structural mechanical design |
CN206218196U (en) * | 2016-11-25 | 2017-06-06 | 深圳光启空间技术有限公司 | The control device and system of aircraft utricule |
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2017
- 2017-06-30 CN CN201710521763.4A patent/CN109204770B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001031200A (en) * | 1999-07-26 | 2001-02-06 | Agency Of Ind Science & Technol | Method and apparatus for sensing gas leakage of airship |
CN104023956A (en) * | 2011-10-11 | 2014-09-03 | 横滨橡胶株式会社 | Puncture repair fluid injection method and injection device |
US20130126675A1 (en) * | 2011-11-23 | 2013-05-23 | Stratospheric Airships, Llc | Durable airship hull and in situ airship hull repair |
CN105438160A (en) * | 2014-08-22 | 2016-03-30 | 杨洋 | Hovercraft air bag capable of being automatically repaired |
CN106347620A (en) * | 2016-10-12 | 2017-01-25 | 郭鹏 | Vacuum type buoyancy flight device based on structural mechanical design |
CN206218196U (en) * | 2016-11-25 | 2017-06-06 | 深圳光启空间技术有限公司 | The control device and system of aircraft utricule |
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