CN202464117U - Aerostat with windward opening to descend - Google Patents
Aerostat with windward opening to descend Download PDFInfo
- Publication number
- CN202464117U CN202464117U CN2012200055513U CN201220005551U CN202464117U CN 202464117 U CN202464117 U CN 202464117U CN 2012200055513 U CN2012200055513 U CN 2012200055513U CN 201220005551 U CN201220005551 U CN 201220005551U CN 202464117 U CN202464117 U CN 202464117U
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- Prior art keywords
- aerostatics
- air bag
- air
- valve
- aerostat
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Abstract
The utility model relates to an aerostat with an windward opening to descend, which comprises an air bag, wherein the lower part of the air bag is provided with a valve and a control device; the valve can be opened when a dynamic head formed by the windward descending is larger than the internal and external pressure differential of the aerostat; and the control device is used for driving the valve to open. Through the aerostat with the windward opening to descend, the potential energy of the aerostat is effectively utilized and converted into the internal energy of the aerostat to effectively replenish the air bag of the aerostat, so that the energy for descending of the aerostat is saved.
Description
Technical field
The utility model relates to the aerostatics that a kind of opening facing the wind to descend, and particularly a kind ofly utilizes gravity to descend and satisfies the aerostatics of the basic conformal of air bag in the decline stage through the opening air inlet of facining the wind.
Background technology
Existing aerostatics (comprising dirigible and captive balloon); Constantly in balloonet, enter air in the decline stage in order to keep its aerodynamic configuration needs; Generally the air intake apparatus such as tail gas with blowing engine or power plant carry out the air transportation, be characterized in that air intake apparatus forms air pressure head and can be input to the aerodynamic configuration that guarantees aerostatics in the balloonet body by actv. greatly, but shortcoming are comparatively obvious; Expenditure of energy is also very big in the decline process of aerostatics, and air intake apparatus need constantly be worked.
From the energy point of view analysis, aerostatics is in the decline process, and air intake apparatus constantly does work, and the gas transport of low-pressure state in high-pressure gasbag, is followed the decline process of aerostatics, and air intake apparatus is in the acting state always.And the potential energy in the dirigible decline process constantly reduces on the other hand, consumes in the fricting movement of decline process and air, but is not utilized.
The utility model content
The deficiency that the utility model exists to prior art just, the aerostatics that provides a kind of opening to facing the wind and descend.When descending, aerostatics is opened valve, is in the opening air inlet in right amount of state down with the wind, reduces the expenditure of energy of aerostatics in the decline process.
For addressing the above problem; The technical scheme that the utility model is taked is following: the aerostatics that a kind of opening facings the wind and descends; Comprise air bag; Said air bag below is provided with: the valve that the dynamic head that descending facings the wind forms is opened during greater than the inside and outside differential pressure of aerostatics, and the control setup that is used to drive valve open.
Said valve openings area S satisfies following formula:
Wherein: v is a descending speed, V
BallBe the aerostatics volume, T is a local temperature, and ρ is local density of air, and Δ P is the aerostatics inside and outside differential pressure, and k is a coefficient of correction.
Be provided with barrier film in the said air bag, barrier film is divided into air bag helium capsule that is positioned at the top and the air bag that is positioned at the below; Fill helium in the said helium capsule, fill air in the air bag.
Said air bag comprises helium capsule and air bag, and the helium capsule is arranged in the air bag; Fill helium in the said helium capsule, fill air in the air bag.
The beneficial effect of the utility model is: the aerostatics that the described opening of the utility model facing the wind to descend can actv. utilizes the potential energy of aerostatics; The potential energy of aerostatics is converted into ability in the aerostatics; Make the air bag of aerostatics obtain replenishing effectively, saved the needed energy in the aerostatics decline process.
Description of drawings
Fig. 1 is the utility model embodiment one said aerostatics structural representation;
Fig. 2 is the utility model embodiment one said aerostatics valve closing view;
Fig. 3 is the utility model embodiment one said aerostatics valve open view;
Fig. 4 is the said aerostatics of the utility model embodiment one view when descending;
Fig. 5 is the utility model embodiment two said aerostatics structural representations;
Among the figure: 1-air bag, 2-valve, 3-control setup, 4-helium, 5-barrier film, 6-helium capsule, 7-air bag, 8-air.
The specific embodiment
To combine concrete embodiment that the content of the utility model is described below.
Be illustrated in figure 1 as the utility model embodiment one said aerostatics structural representation.The said aerostatics of present embodiment comprises air bag 1, valve 2 and control setup 3.Air bag 1 is the main carrier of aerostatics, and set inside has barrier film 5, and barrier film 5 is divided into helium capsule 6 and air bag 7 with air bag 1 internal cavities.Helium capsule 6 is positioned at the top of air bag 1.Helium capsule 6 inside are filled with a certain amount of helium 4, mainly provide buoyancy to swim in the air by aerostatics by helium 4.Air bag 7 inside are filled with air 8, and air 8 lets aerostatics keep the inside and outside differential pressure of air bag 1, guarantees the aerodynamic configuration of aerostatics.Valve 2 and control setup 3 are arranged on the below of air bag 7, valve 2 be arranged on air bag 7 under.Air bag 1, valve 2 and control setup 3, rational weight of three and buoyancy configuration make aerostatics be in a kind of state of equilibrium.
As shown in Figure 2, be the said valve 2 closed condition scheme drawings of present embodiment, Fig. 3 is its open mode scheme drawing.The state of nature of valve 2 is in closed condition.Control setup 3 comprises sensor, and this sensor is arranged on valve 2 places.When aerostatics aloft descended, whether the dynamic head that the sensor sensing at valve 2 places facing the wind to form was greater than the inside and outside differential pressure of aerostatics.When the dynamic head that facing the wind to form during greater than the inside and outside differential pressure of aerostatics, sensor is given control setup 3 feedback signals, is driven by control setup 3 and opens valve 2, and extraneous air gets into air bags 7 through valve 2.
As shown in Figure 4, view when descending for the said aerostatics of present embodiment.Among Fig. 4, aerostatics descends with speed v.In order to realize that aerostatics can the actv. air inlet when descending; The opening of aerostatics lower end valve 2 is in state down with the wind always when aerostatics descends; Under certain descending speed v guarantees; The dynamic head that forms down with the wind is greater than the inside and outside differential pressure of aerostatics, and extraneous air can effectively get into air bags 7 through valve 2, and then additional air bag 7 in-to-in air 8.
The air inlet situation of extraneous air when the aperture area S of valve 2 directly influences aerostatics decline.When area S was excessive, the transient state suction quantity was too much, and the aerostatics descending speed is too fast, influenced its decline balance; When area S was too small, the transient state suction quantity was very few, underused the potential variation of decline.The aperture area S of the described valve 2 of the utility model satisfies following formula:
Wherein: v is a descending speed, V
BallBe the aerostatics volume, T is a local temperature, and ρ is local density of air, and Δ P is the aerostatics inside and outside differential pressure, and k is a coefficient of correction.
The opening shape of valve 2 has certain influence to coefficient of correction k, and according to the practical experience formula, general coefficient of correction k span is 0.02 ~ 0.03.
As shown in Figure 5, be the utility model embodiment two said aerostatics structural representations.Embodiment two with embodiment one key distinction is: do not have barrier film 5 in the embodiment two described air bags 1, air bag 1 comprises helium capsule 6 and air bag 7, and helium capsule 6 is set directly in the air bag 7.
The utility model is in aerostatics, to fill helium as floating empty gas, likewise, fills other the little similar light gas of density ratio density of air, also can realize the function of the utility model, and this does not break away from the essence of the utility model.
Claims (4)
1. the opening aerostatics that facings the wind and descend; Comprise air bag (1); It is characterized in that said air bag (1) below is provided with: the valve (2) that the dynamic head that descending facings the wind forms is opened during greater than the inside and outside differential pressure of aerostatics, and be used to drive the control setup (3) that valve (2) is opened.
2. the aerostatics that a kind of opening as claimed in claim 1 facings the wind and descends is characterized in that said valve (2) aperture area S satisfies following formula:
Wherein: v is a descending speed, V
BallBe the aerostatics volume, T is a local temperature, and ρ is local density of air, and Δ P is the aerostatics inside and outside differential pressure, and k is a coefficient of correction.
3. the aerostatics that facing the wind to descend of according to claim 1 or claim 2 a kind of opening; It is characterized in that; Be provided with barrier film (5) in the said air bag (1), barrier film (5) is divided into the helium capsule (6) that is positioned at the top with air bag (1) and is positioned at the air bag (7) of below; Fill helium (4) in the said helium capsule (6), fill air (8) in the air bag (7).
4. the aerostatics that facing the wind to descend of according to claim 1 or claim 2 a kind of opening is characterized in that said air bag (1) comprises helium capsule (6) and air bag (7), and helium capsule (6) is arranged in the air bag (7); Fill helium (4) in the said helium capsule (6), fill air (8) in the air bag (7).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200055513U CN202464117U (en) | 2012-01-09 | 2012-01-09 | Aerostat with windward opening to descend |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200055513U CN202464117U (en) | 2012-01-09 | 2012-01-09 | Aerostat with windward opening to descend |
Publications (1)
Publication Number | Publication Date |
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CN202464117U true CN202464117U (en) | 2012-10-03 |
Family
ID=46912300
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2012200055513U Expired - Lifetime CN202464117U (en) | 2012-01-09 | 2012-01-09 | Aerostat with windward opening to descend |
Country Status (1)
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102514706A (en) * | 2012-01-09 | 2012-06-27 | 中国电子科技集团公司第三十八研究所 | Aerostat descending with opening facing wind |
-
2012
- 2012-01-09 CN CN2012200055513U patent/CN202464117U/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102514706A (en) * | 2012-01-09 | 2012-06-27 | 中国电子科技集团公司第三十八研究所 | Aerostat descending with opening facing wind |
CN102514706B (en) * | 2012-01-09 | 2014-12-03 | 中国电子科技集团公司第三十八研究所 | Aerostat descending with opening facing wind |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20121003 Effective date of abandoning: 20141203 |
|
AV01 | Patent right actively abandoned |
Granted publication date: 20121003 Effective date of abandoning: 20141203 |
|
RGAV | Abandon patent right to avoid regrant |