CN110171556A - A kind of vane type tail gear and the spheric captive balloon with the device - Google Patents
A kind of vane type tail gear and the spheric captive balloon with the device Download PDFInfo
- Publication number
- CN110171556A CN110171556A CN201910413342.9A CN201910413342A CN110171556A CN 110171556 A CN110171556 A CN 110171556A CN 201910413342 A CN201910413342 A CN 201910413342A CN 110171556 A CN110171556 A CN 110171556A
- Authority
- CN
- China
- Prior art keywords
- vane type
- spheric
- main gasbag
- captive balloon
- pedestal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 14
- 239000007789 gas Substances 0.000 claims description 6
- 239000001307 helium Substances 0.000 claims description 5
- 229910052734 helium Inorganic materials 0.000 claims description 5
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 5
- 238000004873 anchoring Methods 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/42—Construction or attachment of stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/50—Captive balloons
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air Bags (AREA)
- Toys (AREA)
Abstract
The present invention discloses a kind of vane type tail gear and the spheric captive balloon with the device, including pedestal, rotating mechanism, support link and vane type empennage, the pedestal is arranged on spheric captive balloon, the rotating mechanism is arranged on the pedestal, and the vane type empennage is fixedly connected by the support link with the rotating mechanism;The structure setting of vane type tail gear of the present invention, can increase stability, and improve the dynamic lift and buoyancy of spheric captive balloon.
Description
Technical field
The present invention relates to aerostatics technical fields, and in particular to a kind of vane type tail gear and the spherical shape with the device
Captive balloon.
Background technique
Aerostatics is as a kind of weight for generating buoyancy by the gas for being lighter than air for being filled with inside air bag, overcoming its own
The aviation aircraft for measuring and realizing aerial buoyance lift, executing preplanned mission, with airborne period length, survival ability is strong, scouts the visual field
Feature wide, efficiency-cost ratio is high.Captive balloon is itself not drive, the aerostatics to go up to the air by buoyancy.It is by being tethered at cable
Rope is detained scheduled position in the sky, as aerial platform, be suitble to carry various communications, interference, scout, the electronics such as detection are set
It is standby.
Currently, conventional captive balloon uses the aerodynamic configuration of water-drop-shaped, empennage uses inflation soft body structure, divides three pieces in
Y shape arrangement, assigns the good aerodynamic stability of sphere.The volume of conventional captive balloon and surface area ratio are smaller, envelop materials
Weight is larger.And spheric captive balloon can greatly improve volume and surface area ratio, improve the utilization rate of material.But face
There is no the empennages adapted to guarantee the enough stability of sphere for existing ball-type captive balloon.
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 vane type tail gear, wraps
Pedestal, rotating mechanism, support link and vane type empennage are included, the pedestal is arranged on spheric captive balloon, the rotating machine
Structure is arranged on the pedestal, and the vane type empennage is fixedly connected by the support link with the rotating mechanism.
Preferably, the vane type empennage uses soft gas impermeable material, aerodynamic configuration is kept after being filled with buoyance lift gas.
Preferably, a kind of spheric captive balloon, including vane type tail gear, main gasbag, the main gasbag are spherical
Structure has annular to be provided with several vane type tail gears, the pedestal heat at the main gasbag maximum horizontal section
It closes in the main gasbag outer surface.
Preferably, filling helium valve described in being equipped on the main gasbag, the main gasbag lower inside is equipped with balloonet, described
Blower and air valve are installed below balloonet.
Preferably, the surrounding of the main gasbag, which is distributed with, is tethered at drag-line, the drag-line that is tethered at is with the longitudinal direction of the main gasbag
Plane and transverse plane of symmetry arrangement.
It is tethered at drag-line preferably, described and is connected with tether cable by Universal rotary device, the tether cable is tethered in ground
On the anchoring and mooring system of face, on tether cable described in load hanger carry.
Compared with the prior art the beneficial effects of the present invention are: the structure of vane type tail gear of the present invention is set
It sets, stability can be increased, and improve the dynamic lift and buoyancy of spheric captive balloon.
Detailed description of the invention
Fig. 1 is the topology view of the spheric captive balloon;
Fig. 2 is the topology view of the vane type tail gear.
Digital representation in figure:
1- main gasbag;2- fills helium valve;3- vane type empennage;4- balloonet;5- blower;6- air valve;7- is tethered at drag-line;8-
Universal rotary device;9- load hanger;10- tether cable;11- ground anchoring equipment;12- support link;13- rotating mechanism;14-
Pedestal.
Specific embodiment
Below in conjunction with attached drawing, the forgoing and additional technical features and advantages are described in more detail.
Spheric captive balloon of the present invention includes vane type tail gear, main gasbag 1, and the main gasbag 1 is spherical
Structure has annular to be provided with several vane type tail gears at 1 maximum horizontal section of main gasbag, described in reducing
The surface area of main gasbag 1.
Helium valve 2 is filled described in being equipped on the main gasbag 1, convenient for filling helium into the main gasbag 1;The main gasbag
1 lower inside is equipped with balloonet 4, and 1 opposing seal of the balloonet 4 and the main gasbag is equipped with wind below the balloonet 4
Machine 5 and air valve 6, for filling air into the balloonet 4.
It is tethered at the surrounding that drag-line 7 is distributed in the main gasbag 1, in general, the drag-line 7 that is tethered at is with the main gasbag 1
Fore-and-aft plane and transverse plane of symmetry arrangement.Drag-line 7 and the tether cable 10 of being tethered at is connected by Universal rotary device 8, can be protected
The tether cable 10 is held not wind.The tether cable 10 is tethered in ground anchoring equipment 11.9 carry of load hanger
On the tether cable 10.
Vane type tail gear of the present invention includes pedestal 14, rotating mechanism 13, support link 12 and vane type empennage
3,14 heat seal of pedestal is arranged on the main gasbag 1, and the rotating mechanism 13 is arranged on the pedestal 14, the blade
Formula empennage 3 is fixedly connected by the support link 12 with the rotating mechanism 13, and the vane type empennage 3 is using soft impermeable
Gas material keeps aerodynamic configuration after being filled with buoyance lift gas.It can the adjustment of vane type empennage 3 pitching by the rotating mechanism 13
Angle and fore-and-aft plane angle, the front and back vane type empennage is identical as airflow direction, and left and right empennage and balloon are presented centainly
Angle promotes the dynamic lift and stability of balloon.
The working principle of the invention is: when wind is blown from side, front empennage and rear empennage are rotated by 90 ° in setting vertically
It sets, front empennage and rear empennage is made to play the role of choke, captive balloon rotates under windage, is tethered at so as to adjust described
Balloon direction, so that the empennage of front-end and back-end faces air-flow with minimum front face area, while left and right ends empennage and balloon revolve
Certain angle of attack is changed into, the dynamic lift and stability of balloon are promoted.
The present invention can reduce the weight of system, and structure is relatively easy, and be conveniently adjusted spheric captive balloon direction, one
Determine that dynamic lift and net buoyancy can be increased under wind speed;Rectification in front of vane type empennage simultaneously, to reduce resistance.
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 (6)
1. a kind of vane type tail gear, which is characterized in that including pedestal, rotating mechanism, support link and vane type empennage, institute
It states pedestal to be arranged on spheric captive balloon, the rotating mechanism is arranged on the pedestal, and the vane type empennage passes through institute
Support link is stated to be fixedly connected with the rotating mechanism.
2. vane type tail gear as described in claim 1, which is characterized in that the vane type empennage is using soft airtight
Material keeps aerodynamic configuration after being filled with buoyance lift gas.
3. a kind of spheric captive balloon, which is characterized in that including vane type tail gear as stated in claim 1 or 2, master
Air bag, the main gasbag are spherical structure, have annular to be provided with several leaves at the main gasbag maximum horizontal section
Chip tail gear, the pedestal are heat sealing at the main gasbag outer surface.
4. spheric captive balloon as claimed in claim 3, which is characterized in that helium valve is filled described in being equipped on the main gasbag,
The main gasbag lower inside is equipped with balloonet, is equipped with blower and air valve below the balloonet.
5. spheric captive balloon as claimed in claim 4, which is characterized in that the surrounding of the main gasbag, which is distributed with, is tethered at drawing
Rope, the drag-line that is tethered at are arranged with the fore-and-aft plane of the main gasbag and transverse plane of symmetry.
6. spheric captive balloon as claimed in claim 5, which is characterized in that it is described be tethered at drag-line and tether cable pass through it is universal
Rotator is connected, and the tether cable is tethered in ground anchoring equipment, on tether cable described in load hanger carry.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910413342.9A CN110171556B (en) | 2019-05-17 | 2019-05-17 | Spherical captive balloon |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910413342.9A CN110171556B (en) | 2019-05-17 | 2019-05-17 | Spherical captive balloon |
Publications (2)
Publication Number | Publication Date |
---|---|
CN110171556A true CN110171556A (en) | 2019-08-27 |
CN110171556B CN110171556B (en) | 2021-05-25 |
Family
ID=67691511
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201910413342.9A Active CN110171556B (en) | 2019-05-17 | 2019-05-17 | Spherical captive balloon |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110171556B (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1726062A (en) * | 1928-10-16 | 1929-08-27 | Clarence C Gilman | Dirigible aircraft |
JPH08198188A (en) * | 1995-01-23 | 1996-08-06 | Kunihide Miyake | Fixed type satellite balloon |
US20100102164A1 (en) * | 2008-10-29 | 2010-04-29 | Rinaldo Brutoco | System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source |
CN104002958A (en) * | 2014-05-12 | 2014-08-27 | 上海萃智工业技术有限公司 | Airship with auxiliary wings |
CN106741813A (en) * | 2017-01-17 | 2017-05-31 | 南京柯尔航空科技有限公司 | A kind of flapping wing dirigible |
CN106741815A (en) * | 2016-12-08 | 2017-05-31 | 中国特种飞行器研究所 | A kind of captive balloon |
CN106882355A (en) * | 2017-04-01 | 2017-06-23 | 太原科技大学 | One kind rope draws positioning formula high-altitude suspension sightseeing balloon |
-
2019
- 2019-05-17 CN CN201910413342.9A patent/CN110171556B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1726062A (en) * | 1928-10-16 | 1929-08-27 | Clarence C Gilman | Dirigible aircraft |
JPH08198188A (en) * | 1995-01-23 | 1996-08-06 | Kunihide Miyake | Fixed type satellite balloon |
US20100102164A1 (en) * | 2008-10-29 | 2010-04-29 | Rinaldo Brutoco | System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source |
CN104002958A (en) * | 2014-05-12 | 2014-08-27 | 上海萃智工业技术有限公司 | Airship with auxiliary wings |
CN106741815A (en) * | 2016-12-08 | 2017-05-31 | 中国特种飞行器研究所 | A kind of captive balloon |
CN106741813A (en) * | 2017-01-17 | 2017-05-31 | 南京柯尔航空科技有限公司 | A kind of flapping wing dirigible |
CN106882355A (en) * | 2017-04-01 | 2017-06-23 | 太原科技大学 | One kind rope draws positioning formula high-altitude suspension sightseeing balloon |
Also Published As
Publication number | Publication date |
---|---|
CN110171556B (en) | 2021-05-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101883896B1 (en) | Buoyant aerial vehicle | |
EP0078713B1 (en) | Aircraft having buoyancy gas balloon | |
SA519402008B1 (en) | High endurance unmanned aerial vehicle | |
CN103661915B (en) | The controlled aerostat system of track that a kind of atural beat and sail drive | |
US11459080B2 (en) | Transformable stratospheric airship | |
CN205952280U (en) | Stratospheric dirigible of expanded letter adjustable wing | |
PT1551706E (en) | Dual hull airship controlled by thrust vectoring | |
WO2007037932A2 (en) | Airship having a central fairing to act as a stall strip and to reduce lift | |
CN205239885U (en) | Airship | |
FR2228664B1 (en) | ||
CN205686600U (en) | The aircraft that a kind of dirigible is combined with many rotors | |
CN109703730B (en) | High-altitude captive balloon and control method thereof | |
CN110171556A (en) | A kind of vane type tail gear and the spheric captive balloon with the device | |
CN109250064A (en) | Novel bionic aircraft structure with integrated buoyancy and lift high lift-drag ratio | |
JP5811384B1 (en) | Air levitation device and its air navigation | |
CN209600783U (en) | A kind of captive balloon with kite empennage | |
CN104843191B (en) | Contactless smart rain insensitive device for unmanned plane | |
CN104443343B (en) | Vector advances floated flight instruments | |
KR101378954B1 (en) | Air ballon of volume control using on-off device | |
CN109319083A (en) | A kind of axis change soft lighter-than-air flight device of buoyancy | |
CN213974490U (en) | Rotary parachute | |
CN207758994U (en) | A kind of navigation aircraft horizontal tail | |
CN108263592B (en) | Triaxial ellipsoid airship | |
CN113753214A (en) | A semi-lift airship | |
CN102085913A (en) | Novel flying saucer type aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |