CN110341926A - A kind of stratosphere aerostatics and height adjusting method - Google Patents
A kind of stratosphere aerostatics and height adjusting method Download PDFInfo
- Publication number
- CN110341926A CN110341926A CN201910597228.6A CN201910597228A CN110341926A CN 110341926 A CN110341926 A CN 110341926A CN 201910597228 A CN201910597228 A CN 201910597228A CN 110341926 A CN110341926 A CN 110341926A
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- CN
- China
- Prior art keywords
- diaphragm
- tensioning
- adjustment device
- volume adjustment
- convex lobe
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Classifications
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- 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
Abstract
The present invention discloses a kind of stratosphere aerostatics and height adjusting method, including volume adjustment device and convex lobe body of revolution sphere；The convex lobe body of revolution sphere includes the reinforcing rib between film utricule and the adjacent diaphragm that several diaphragms are formed, and the balloon body is made to form the equally distributed rotation body structure of several convex lobe annulars；The quantity of the convex lobe on the balloon body is adjusted in the volume adjustment device, to change the volume of the balloon body；The direct acting object of height control method is buoyance lift gas inside utricule in the present invention；The present invention in height adjustment, do not do work to utricule outside air medium by executing agency, compares the height adjusting method of traditional rudder face and vector power, has low energy consumption, efficient advantage.
Description
Technical field
The present invention relates to aerostatics technical fields, and in particular to a kind of stratosphere aerostatics and height adjusting method.
Background technique
Since dirigible is born within 1852, the type and control mode of aerostatics have obtained development by leaps and bounds.Early stage dirigible one
As using rudder face be used as flight control means, by lifting control surface deflection generation aerodynamic moment, change the pitch attitude of kayak body,
To adjust height using the aerodynamic lift of kayak body.With the development of dynamical system, more vectored thrusts start to be applied to aerostatics,
By deflection propeller plane or the puff prot direction of turbojet engine, so that change dynamical system directly drives power side
To realizing the adjustment of flying height.
Above-mentioned conventional flight control means have done a large amount of function to air dielectric when controlling aerostatics lifting, wherein only
Some acts on aerostatics lifting.
In view of the above drawbacks, creator of the present invention obtains the present invention by prolonged research and practice finally.
Summary of the invention
To solve above-mentioned technological deficiency, the technical solution adopted by the present invention is, provides a kind of stratosphere aerostatics, including
Volume adjustment device and balloon body；The balloon body includes between film utricule and the adjacent diaphragm that several diaphragms are formed
Reinforcing rib makes the balloon body form the equally distributed rotation body structure of several convex lobe annulars；The volume adjustment device
The quantity of the convex lobe on the balloon body is adjusted, to change the volume of the balloon body.
Preferably, the volume adjustment device is provided with tensioned portion and bracing cable, several tensionings are provided in the tensioned portion
Hole, the bracing cable sequentially pass through each tensioning hole, and the phase in each tensioning hole is adjusted by the stretch-draw effect of the bracing cable
To position, to realize the folding or expansion to the convex lobe.
Preferably, the tensioned portion is set as several strip tension bands, two tension bands are respectively arranged at same described
The two sides of diaphragm；The tension band includes fixed side and free side, and the fixed side is fixed with the diaphragm side
It connects, is provided with several tensioning holes on the free side, and the tensioning hole of the diaphragm two sides is staggered.
Preferably, the tensioned portion is set as several blocky tensioning blocks, the tensioning block is in the two sides of the same diaphragm
While being staggered, the tensioning block is fixedly connected with the diaphragm side, and the tensioning is provided in the tensioned portion
Hole.
Preferably, the tensioning hole for being located at the same side of the diaphragm is in the same plane；It is adjusted in the volume
In a free state, the tensioning hole of the same diaphragm two sides is respectively in two different planes device,
When the volume adjustment device is in tensioning state, the tensioning hole of the same diaphragm two sides can be at same plane
On.
Preferably, being provided with the diaphragm of the tensioned portion and the diaphragm interval of the not set tensioned portion is set
It sets.
Preferably, a kind of height adjusting method of the stratosphere aerostatics are as follows: rise and adjust: the bracing cable is loosened, quilt
The convex lobe expansion folded, so that the film utricule be made to be unfolded, volume increases, and buoyancy increases, to realize that height rises；
Decline is adjusted: the bracing cable is shunk, and the part convex lobe is folded, so that the film utricule be made to be compressed, volume reduces, and is floated
Power reduces, to realize that height declines.
The beneficial effects of the present invention are the direct of: traditional rudder face control and the control of vector driving force compared with the prior art
Acting object is utricule outside air, and the direct acting object of height control method is buoyance lift gas inside utricule in the present invention；
The present invention does not do work to air dielectric, compares rudder face and vector power in height adjustment, has low energy consumption, efficiently
The advantages of rate.
Detailed description of the invention
Fig. 1 is the partial sectional view of the volume adjustment device；
Fig. 2 is the partial elevation view of the volume adjustment device；
Fig. 3 is shape view of the balloon body in two states；
Fig. 4 is the flow chart of the height adjusting method.
Digital representation in figure:
1- diaphragm；2- tensioned portion；3- bracing cable；4 one tensioning holes.
Specific embodiment
Below in conjunction with attached drawing, the forgoing and additional technical features and advantages are described in more detail.
Stratosphere aerostatics of the present invention includes volume adjustment device and balloon body, by swollen to balloon body inflation
The swollen high-altitude floating for realizing the stratosphere aerostatics, it is quiet to adjust the balloon body stereomutation by the volume adjustment device
To realize the height adjustment of the stratosphere aerostatics, the volume adjustment device is set on the balloon body buoyancy.
The balloon body includes the reinforcing rib between film utricule and the adjacent diaphragm 1 that several diaphragms 1 are formed, makes institute
More convex lobe rotation body structures that balloon body forms geometry are stated, i.e., each diaphragm 1 is formed under the reinforcing rib and internal pressure effect
Convex lobe, to form the equally distributed rotation body structure of several convex lobe annulars；The volume adjustment device is adjustable described
The quantity of the convex lobe on balloon body, to change the volume of the balloon body.
As depicted in figs. 1 and 2, Fig. 1 is the partial sectional view of the volume adjustment device；Fig. 2 is volume adjustment dress
The partial elevation view set；Specifically, the volume adjustment device is provided with tensioned portion 2 and bracing cable 3, it is arranged in the tensioned portion 2
There are several tieholens 4, the bracing cable 3 sequentially passes through each tensioning hole 4, adjustable each by the stretch-draw effect of the bracing cable 3
The relative position in the tensioning hole 4, to realize the folding or expansion to the convex lobe.
Preferably, the tensioned portion 2 may be configured as several strip tension bands, two tension bands are respectively arranged at same institute
State the two sides of diaphragm 1；The tension band includes fixed side and free side, the fixed side and 1 side of diaphragm
It is fixedly connected, several tensioning holes 4 is provided on the free side, and the tensioning hole 4 of 1 two sides of the diaphragm is handed over
Mistake setting.
Likewise, the tensioned portion 2 may be alternatively provided as several blocky tensioning blocks, the tensioning block is in the same diaphragm 1
Two sides be staggered, the tensioning block is fixedly connected with 1 side of diaphragm, and is provided in the tensioned portion 2
The tensioning hole 4.
The tensioning hole 4 positioned at the same side of the diaphragm 1 is in the same plane；At the volume adjustment device
When free state, the tensioning hole 4 of same 1 two sides of diaphragm is respectively in two different planes, i.e. two sides
The tensioning hole 4 on side is in interleaved state；When the volume adjustment device is in tensioning state, same 1 liang of the diaphragm
The tensioning hole 4 of side can be on same plane.
Preferably, be provided with the tensioned portion 2 the diaphragm 1 and the not set tensioned portion 2 the diaphragm 1 can between
Every setting.
Specifically, working as the volume adjustment device in a free state, the bracing cable 3 is in the state that do not exert a force, setting
The diaphragm 1 between two tensioned portions 2 external drum under the action of film utricule air pressure inside forms the convex lobe；
When the volume adjustment device is in tensioning state, the bracing cable 3 exerts a force, and the staggered tensioning hole 4 is furthered, thus will
The two sides of the diaphragm 1 are furthered, to the diaphragm 1 be folded under the pulling force effect of the bracing cable 3 to described in reduction
The quantity of the convex lobe on balloon body.
The tensioned portion 2 and position that the film utricule connects can the Chong Die bonding pad of adjacent two diaphragm 1 position,
The position of the i.e. described reinforcing rib, to avoid the tensioned portion 2 that the influence film utricule itself is arranged.
As shown in figure 3, the volume adjustment device is under free state when using the setting of the tensioned portion 2 interval,
40 convex lobes are provided on the film utricule；The volume adjustment device is under tensioning state, the film utricule
On be provided with 20 convex lobes.
The tensioning of the bracing cable 3 and loosening can be used existing tensioning equipment and realize, one end of bracing cable is solid as will be described
The top other end for being scheduled on the film utricule is pullled winding by rotating electric machine etc. and is realized.
Moving up and down for aerostatics is controlled by the volume adjustment device, recycles different height wind speed and direction
Regularity, to control the flight path of aerostatics.It is exactly of the invention for increasing a volume adjustment device to aerostat
The control to the flight path of aerostat may be implemented using this device in emphasis, so that aerostat be made to rely on without making
Resident flight can be realized within a certain area with complicated power device.
The direct acting object of traditional rudder face control and the control of vector driving force is utricule outside air, height in the present invention
The direct acting object of control method is buoyance lift gas inside utricule.The present invention is not situated between to air in height adjustment
Matter acting, compares rudder face and vector power, has low energy consumption, efficient advantage.
As shown in figure 4, the height adjusting method of stratosphere aerostatics of the present invention are as follows: rise and adjust: the bracing cable is put
Pine, the convex lobe expansion being folded, so that the film utricule be made to be unfolded, volume increases, and buoyancy increases, to realize height
Rise；Decline is adjusted: the bracing cable is shunk, and the part convex lobe is folded, so that the film utricule be made to be compressed, volume subtracts
Small, buoyancy reduces, to realize that height declines.
The film that convex lobe is shunk in the present invention is in relaxed state, does not almost stress, load transfer to tension cable；It does not receive
Contracting convex lobe, film stress remain unchanged, and when volume change, utricule will not generate stress concentration.In addition, volume of the present invention becomes
When change, it is able to maintain aerostatics low-resistance sweeping appearance, there is better aeroperformance.
The foregoing is merely presently preferred embodiments of the present invention, is merely illustrative for the purpose of the present invention, and not restrictive
's.Those skilled in the art understand that in the spirit and scope defined by the claims in the present invention many changes can be carried out to it,
It modifies or even equivalent, but falls in protection scope of the present invention.
Claims (7)
1. a kind of stratosphere aerostatics, which is characterized in that including volume adjustment device and balloon body；The balloon body includes several
The reinforcing rib between film utricule and the adjacent diaphragm that diaphragm is formed makes the balloon body form several convex lobe annulars
Equally distributed rotation body structure；The volume adjustment device adjusts the quantity of the convex lobe on the balloon body, to change
State the volume of balloon body.
2. stratosphere aerostatics as described in claim 1, which is characterized in that the volume adjustment device be provided with tensioned portion and
Bracing cable is provided with several tieholens in the tensioned portion, and the bracing cable sequentially passes through each tensioning hole, passes through the bracing cable
The relative position in each tensioning hole is adjusted in stretch-draw effect, the convex lobe is folded or is unfolded.
3. stratosphere aerostatics as claimed in claim 2, which is characterized in that the tensioned portion is set as several strip tensionings
Band, two tension bands are respectively arranged at the two sides of the same diaphragm；The tension band includes fixed side and free side
Portion, the fixed side are fixedly connected with the diaphragm side, and several tensioning holes, and institute are provided on the free side
The tensioning hole for stating diaphragm two sides is staggered.
4. stratosphere aerostatics as claimed in claim 2, which is characterized in that the tensioned portion is set as several blocky tensionings
Block, the tensioning block are staggered in the two sides of the same diaphragm, and the tensioning block fixes company with the diaphragm side
It connects, and is provided with the tensioning hole in the tensioned portion.
5. stratosphere aerostatics as described in claim 3 or 4, which is characterized in that described in the same side of the diaphragm
It is in the same plane to be tensioned hole；The volume adjustment device in a free state, the institute of the same diaphragm two sides
Tensioning hole is stated to be respectively in two different planes, when the volume adjustment device is in tensioning state, the same film
The tensioning hole of piece two sides can be on same plane.
6. stratosphere aerostatics as claimed in claim 2, which is characterized in that be provided with the diaphragm and not of the tensioned portion
The diaphragm interval setting of the tensioned portion is set.
7. a kind of height adjusting method of stratosphere aerostatics as claimed in claim 6 characterized by comprising rising tone
Section: the bracing cable is loosened, and the convex lobe expansion being folded, so that the film utricule be made to be unfolded, volume increases, and buoyancy increases
Add, to realize that height rises；Decline is adjusted: the bracing cable is shunk, and the part convex lobe is folded, to make the film capsule
Body is compressed, and volume reduces, and buoyancy reduces, to realize that height declines.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910597228.6A CN110341926A (en) | 2019-07-03 | 2019-07-03 | A kind of stratosphere aerostatics and height adjusting method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910597228.6A CN110341926A (en) | 2019-07-03 | 2019-07-03 | A kind of stratosphere aerostatics and height adjusting method |
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| Publication Number | Publication Date |
|---|---|
| CN110341926A true CN110341926A (en) | 2019-10-18 |
Family
ID=68178122
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910597228.6A Pending CN110341926A (en) | 2019-07-03 | 2019-07-03 | A kind of stratosphere aerostatics and height adjusting method |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1424232A (en) * | 2001-12-07 | 2003-06-18 | 宇宙科学研究所长 | Pressure-proof balloon |
| CN102205875A (en) * | 2010-12-29 | 2011-10-05 | 中国特种飞行器研究所 | Umbrella unfolding type airship air bag |
| CN102673771A (en) * | 2012-05-23 | 2012-09-19 | 上海交通大学 | Air floating aircraft with variable configuration |
| CN103303457A (en) * | 2013-06-06 | 2013-09-18 | 北京新誉防务技术研究院有限公司 | Soft and hard hybrid airship and control method thereof |
| CN104859834A (en) * | 2015-05-20 | 2015-08-26 | 王树强 | Low-energy-consumption fast controllable-change static ascending and descending device |
-
2019
- 2019-07-03 CN CN201910597228.6A patent/CN110341926A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1424232A (en) * | 2001-12-07 | 2003-06-18 | 宇宙科学研究所长 | Pressure-proof balloon |
| CN102205875A (en) * | 2010-12-29 | 2011-10-05 | 中国特种飞行器研究所 | Umbrella unfolding type airship air bag |
| CN102673771A (en) * | 2012-05-23 | 2012-09-19 | 上海交通大学 | Air floating aircraft with variable configuration |
| CN103303457A (en) * | 2013-06-06 | 2013-09-18 | 北京新誉防务技术研究院有限公司 | Soft and hard hybrid airship and control method thereof |
| CN104859834A (en) * | 2015-05-20 | 2015-08-26 | 王树强 | Low-energy-consumption fast controllable-change static ascending and descending device |
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Application publication date: 20191018 |