CN102815392A - Balance adjusting system for airship - Google Patents
Balance adjusting system for airship Download PDFInfo
- Publication number
- CN102815392A CN102815392A CN2012102870861A CN201210287086A CN102815392A CN 102815392 A CN102815392 A CN 102815392A CN 2012102870861 A CN2012102870861 A CN 2012102870861A CN 201210287086 A CN201210287086 A CN 201210287086A CN 102815392 A CN102815392 A CN 102815392A
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- airship
- dirigible
- balance
- ballasting
- adjusting system
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Abstract
The invention relates to the technical field of balance control on a large-size air flying platform, such as an airship and specifically relates to a balance adjusting system for the airship. The invention provides the balance adjusting system for the airship, in order to solve the problems in the prior art that the response speed is low and the dynamic balance of the airship cannot be realized. According to the technical scheme provided by the invention for solving the problems in the prior art, the balance adjusting system for the airship comprises a ballast and a pump set, wherein the ballast is arranged on a platform; the pump set is arranged on the platform; the ballast is composed of a plurality of ballast containers; and the pump set is respectively communicated with the ballast containers through a valve switch. The balance adjusting system for the airship has the advantages of simple structure, easiness in implementation, low manufacturing and use costs and further development of the airship application.
Description
Technical field
The present invention relates to the balance control technical field of large-scale floating hollow panels such as dirigible, be specifically related to a kind of dirigible balance regulation system.
Technical background
Dirigible is as a kind of general purpose vehicle, and prospect is widely used in the General Aviation field.Dirigible (or other large-scale floating hollow panels) in flight course along with the variation of the factors such as passenger shift position of the consumption of fuel oil, lift-launch; Ship body load can redistribute thereupon; Thereby cause the hull flight attitude to change, influence the normal operation of dirigible.Under the inclination serious situation, damage the hull structure easily, influence control flight attitude, when more serious, threaten flight safety, cause personal casualty.In order to address this problem; Dirigible (or other large-scale floating hollow panels) all comprises balance induction system, balance control system and balance regulation system; The flight attitude of balance induction system induction dirigible; Its signal in real time is sent into balance control system, and balance control system is according to this signal control balance regulation system action.Existing dirigible balance regulation system is realized balance with the fixedly ballace that is provided with on the platform usually, and the problem of existence is: speed of response is slow, can not realize instant balance, can not realize the dynamical equilibrium of dirigible.
Summary of the invention
The present invention will provide a kind of dirigible balance regulation system, and is slow to overcome the speed of response that prior art exists, and can not realize the difficult problem of dirigible dynamical equilibrium.
In order to overcome the problem that prior art exists; The present invention realizes through following technical proposals: a kind of dirigible balance regulation system; Comprise the ballace that is provided with on the platform; Its special character is: also comprise the pump group that is provided with on the platform, described ballace is several ballasting containers, and the pump group is connected with several ballasting containers respectively through valve switch.
Above-mentioned ballasting container comprises preceding ballasting container, back ballasting container, left ballasting container and right ballasting container.
Be provided with the water or the anti-freezer of good fluidity in the above-mentioned ballasting container.
Compared with prior art, advantage of the present invention is:
1. the present invention is according to the geometric configuration and the size of dirigible (or floating in the air hollow panel); Utilize " lever principle " and " law of connected vessels "; Realize the DYNAMIC DISTRIBUTION of dirigible (or floating hollow panel) counterweight object in the air; In flight course, adjust the distribution of weight of liquid in container at any time, reach the purpose of adjusting airship flight attitude dynamical equilibrium at any time.
2. simple in structure, implement easily, and manufacturing cost and use cost is low, and the purposes of dirigible is further expanded.
Description of drawings:
Fig. 1 is a structural representation of the present invention;
Wherein, ballace container, 5-left side ballace container, the right ballace container of 6-behind 1-pump group, 2-valve switch, the preceding ballace container of 3-, the 4-.
The specific embodiment:
To combine accompanying drawing that the present invention is at length explained below.
A kind of dirigible balance regulation system; Comprise the pump group 1 and several ballasting containers that are provided with on the platform; Pump group 1 is connected with several ballasting containers respectively through valve switch 2, and said ballasting container comprises preceding ballasting container 3, back ballasting container 4, left ballasting container 5 and right ballasting container 6.In the ballasting container, be provided with the anti-freezer of good fluidity.
Ballasting container (its amount of capacity is set according to actual needs such as dirigible sizes, and material is advisable with lightweight, firm material) is set respectively in the flat-bed front, rear, left and right of dirigible.The ballasting container is connected to pump group 1 respectively through pipeline, and the valve switch 2 on every pipeline is that one normally closed electrically operated valve is set at least, and pump group 1 can be provided with one or more two-way liquid pumps according to actual needs.
In whole dirigible, balance balance induction installation is fixed in hull and configures initial equilibrium conditions.At dirigible in operational process; The balance induction system is monitored the dirigible state of equilibrium and in real time through data line or the wireless terminal control system that outputs signal to; Terminal control system is according to condition of setting and the data that obtain from balance sensor; The real-time current state of equilibrium of compare of analysis dirigible, whether computational analysis dirigible state of equilibrium remains in the state range of setting.If the dirigible state of equilibrium in the state range of setting, then continues to keep present situation, exceed the state range of setting up to state of equilibrium.When state of equilibrium exceeds the state range of setting; Through calculating identification, device of the present invention is given in output balance adjustment instruction by terminal control system, and pump group 1 in apparatus of the present invention and corresponding valve switch 2 obtain instruction; Make pump group 1 start working; Simultaneously corresponding valve switch 2 is opened, and redistributes the liquid distribution state in the adjustment ballasting container, and the size of wherein adjusting speed and flow rate of liquid, circulation passage sectional area are relevant; Flow rate of liquid is bigger, the speed of the bigger then adjustment of circulation passage sectional area is big more, otherwise more little.The balance adjustment continues to carry out; Find that up to terminal control system signal indicating airship flight attitude adjusted that the balance induction system provides is to setting state of equilibrium; Just return to again within the state of equilibrium scope of setting, at this moment, terminal control system instruction pump group 1 quits work; Close all valve switchs 2 of opening simultaneously, valve switch 2 returns to normally off.
Under each typical state of equilibrium of dirigible, dirigible state of equilibrium control system is as shown in the table to the mode of dirigible Adjustment System:
More than combine the accompanying drawing specific embodiments of the invention to be described; But these explanations can not be understood that to have limited scope of the present invention; Protection scope of the present invention is limited the claims of enclosing, and any change on claim of the present invention basis all is protection scope of the present invention.
Claims (3)
1. dirigible balance regulation system; Comprise the ballace that is provided with on the platform; It is characterized in that: also comprise the pump group (1) that is provided with on the platform, described ballace is several ballasting containers, and pump group (1) is connected with several ballasting containers respectively through valve switch (2).
2. according to the said dirigible balance regulation system of claim 1, it is characterized in that: said ballasting container comprises preceding ballasting container (3), back ballasting container (4), left ballasting container (5) and right ballasting container (6).
3. according to claim 1 or 2 said dirigible balance regulation systems, it is characterized in that: the water or the anti-freezer that are provided with good fluidity in the said ballasting container.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102870861A CN102815392A (en) | 2012-08-14 | 2012-08-14 | Balance adjusting system for airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102870861A CN102815392A (en) | 2012-08-14 | 2012-08-14 | Balance adjusting system for airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102815392A true CN102815392A (en) | 2012-12-12 |
Family
ID=47299928
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012102870861A Pending CN102815392A (en) | 2012-08-14 | 2012-08-14 | Balance adjusting system for airship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102815392A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105730684A (en) * | 2016-01-29 | 2016-07-06 | 安徽工程大学 | Multi-rotor gunship helicopter |
| CN109250061A (en) * | 2018-11-14 | 2019-01-22 | 北京空天高科技有限公司 | Stratospheric airship device for adjusting posture |
| CN109250062A (en) * | 2018-11-14 | 2019-01-22 | 北京空天高科技有限公司 | A kind of stratospheric airship device for adjusting posture |
| CN109398672A (en) * | 2018-11-14 | 2019-03-01 | 北京空天高科技有限公司 | Liquid bidirectional pumping system and the stratospheric airship device for adjusting posture for using it |
| CN110712736A (en) * | 2019-11-11 | 2020-01-21 | 青田极石航空科技有限公司 | Balancing weight adjusting equipment for aviation equipment |
| CN112660366A (en) * | 2020-12-24 | 2021-04-16 | 重庆工程职业技术学院 | Unmanned aerial vehicle survey and drawing flight stable control device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2774305A (en) * | 1952-07-09 | 1956-12-18 | Thomas W Fitzgerald | Rocket steering system |
| US2807428A (en) * | 1953-07-15 | 1957-09-24 | Vibrane Corp | Aircraft with enclosed rotor |
| CN101052563A (en) * | 2004-06-21 | 2007-10-10 | Ltas控股股份有限公司 | Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments |
| CN202848018U (en) * | 2012-08-14 | 2013-04-03 | 党化宁 | Balance adjusting system for airship |
-
2012
- 2012-08-14 CN CN2012102870861A patent/CN102815392A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2774305A (en) * | 1952-07-09 | 1956-12-18 | Thomas W Fitzgerald | Rocket steering system |
| US2807428A (en) * | 1953-07-15 | 1957-09-24 | Vibrane Corp | Aircraft with enclosed rotor |
| CN101052563A (en) * | 2004-06-21 | 2007-10-10 | Ltas控股股份有限公司 | Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments |
| CN202848018U (en) * | 2012-08-14 | 2013-04-03 | 党化宁 | Balance adjusting system for airship |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105730684A (en) * | 2016-01-29 | 2016-07-06 | 安徽工程大学 | Multi-rotor gunship helicopter |
| CN105730684B (en) * | 2016-01-29 | 2018-02-02 | 安徽工程大学 | A kind of more rotor armed helicopters |
| CN109250061A (en) * | 2018-11-14 | 2019-01-22 | 北京空天高科技有限公司 | Stratospheric airship device for adjusting posture |
| CN109250062A (en) * | 2018-11-14 | 2019-01-22 | 北京空天高科技有限公司 | A kind of stratospheric airship device for adjusting posture |
| CN109398672A (en) * | 2018-11-14 | 2019-03-01 | 北京空天高科技有限公司 | Liquid bidirectional pumping system and the stratospheric airship device for adjusting posture for using it |
| CN109250061B (en) * | 2018-11-14 | 2023-08-15 | 北京空天高技术中心(有限合伙) | Stratospheric airship attitude adjusting device |
| CN109250062B (en) * | 2018-11-14 | 2024-03-15 | 北京空天高科技有限公司 | Stratospheric airship attitude adjusting device |
| CN109398672B (en) * | 2018-11-14 | 2024-03-15 | 北京空天高科技有限公司 | Liquid bidirectional pump system and stratospheric airship attitude adjusting device adopting same |
| CN110712736A (en) * | 2019-11-11 | 2020-01-21 | 青田极石航空科技有限公司 | Balancing weight adjusting equipment for aviation equipment |
| CN110712736B (en) * | 2019-11-11 | 2020-10-27 | 青田极石航空科技有限公司 | Balancing weight adjusting equipment for aviation equipment |
| CN112660366A (en) * | 2020-12-24 | 2021-04-16 | 重庆工程职业技术学院 | Unmanned aerial vehicle survey and drawing flight stable control device |
| CN112660366B (en) * | 2020-12-24 | 2023-08-08 | 重庆工程职业技术学院 | Unmanned aerial vehicle survey and drawing flight stability control device |
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| PB01 | Publication | ||
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20121212 |