CN205952280U - Stratospheric dirigible of expanded letter adjustable wing - Google Patents
Stratospheric dirigible of expanded letter adjustable wing Download PDFInfo
- Publication number
- CN205952280U CN205952280U CN201620929759.2U CN201620929759U CN205952280U CN 205952280 U CN205952280 U CN 205952280U CN 201620929759 U CN201620929759 U CN 201620929759U CN 205952280 U CN205952280 U CN 205952280U
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- dirigible
- ship
- expanded letter
- balloonet
- pressure system
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
Stratospheric dirigible of expanded letter adjustable wing is including wide hull, solar power system, vector propeller, pressure system and flight control system, the length of wide hull is 2.1~2.5 with the proportion of width: 1, wide hull upper portion is laid and is installed solar power system, installing at the both sides of wide hull and the rear portion of wide hull of vector propeller symmetry, aerifing or gassing work of wide hull is accomplished to the pressure system, solar power system is the vector propeller, pressure system and flight control system power supply, flight control system respectively with solar power system, vector propeller and pressure system electric connection, and control solar power system respectively, vector propeller and pressure system work, the dirigible is the platykurtic, greatly increased solar power system lay the area, change light energy into sufficient electric power driven vector propeller, make dirigible power pure, the proportion is best simultaneously, flight is got up controllability and bearing capacity and is being shown and promote.
Description
Technical field
This utility model is related to dirigible field, more particularly, to the stratospheric airship field of expanded letter adjustable wing.
Background technology
At the beginning of 21 century, stratospheric airship enjoys the concern of each big country, and prediction application spreads all over civilian, police, quasi- army
With, military etc.；At present, it is applied to the civil areas such as ocean research, rescue and relief work, urban traffic control stratospheric airship more.
Stratospheric airship is a kind of aerostatics being lighter than air, relies on aerostatic buoyancy to stay sky, can be with long-term suspension in advection
Floor height is empty, is that it provides energy source and power by solar energy, and carries propulsion system, have be independent of airport or runway can achieve vertical
Landing, can hover in arbitrary geographic position overhead, run height and exceed blank pipe scope, be not subject to troposphere adverse weather conditions, can
All-weather round-the-clock continuously works, and except needing ground control's data to accept treatment facility, with little need for other ground
Face infrastructure are supported, various aspects have impayable advantage.
But current stratospheric airship technology is not also very ripe, and mostly blimp shape is drop -shaped list kayak body, leads to too
Sun can lay limited area by TRT, adds that luminous energy transfer power is limited, thus limiting the power of dirigible, dirigible power is not
In the case of foot, dirigible wind loading rating is just weak, and whether controlled ability or bearing capacity are all extremely limited for whole dirigible, but
If simple only consider to increase the upper surface area of dirigible, the resistance that excessive dirigible is subject to is just big, and maneuverability reduces, and controls
Get up inconvenience, be not very practical.
Content of the invention
For the deficiencies in the prior art, technical problem to be solved in the utility model is to provide a kind of expanded letter adjustable wing
Stratospheric airship, dirigible is in flat, considerably increases the laying area of device of solar generating, luminous energy is changed into enough
, so that dirigible power is full, ratio is optimal simultaneously for electrical energy drive vector propeller, flight get up controllability and bearing capacity notable
Lifting.
This utility model solves its technical problem and be employed technical scheme comprise that：
The stratospheric airship of expanded letter adjustable wing, including wide hull, device of solar generating, vector propeller, pressure system
And flight control system；The ratio of the length of described wide hull and width is 2.1～2.5:1, the laying of wide hull top is provided with the sun
Energy TRT, vector propeller is symmetrically installed on wide hull, and pressure system completes inflation or the venting work of wide hull
Make, device of solar generating is vector propeller, pressure system and flight control system are powered, flight control system respectively with solar electrical energy generation
Device, vector propeller and pressure system electrical connection, and control device of solar generating, vector propeller and pressure system respectively
Work.
Optimum, described wide hull is to be combined by three single utricules, and a single utricule is located at centre, two single utricules
Positioned at both sides, and the head of single utricule of centre protrudes from the head of single utricule of both sides；Middle single utricule horizontal level is high
In single utricule of both sides, that is, three single utricules surround a gondola space in middle single utricule bottom.
Optimum, described single utricule includes main gasbag and the balloonet being arranged within main gasbag, and described balloonet is divided into
Front balloonet and rear balloonet, main gasbag, front balloonet and rear balloonet complete to inflate or exit work by pressure system respectively
Make, fill helium in main gasbag, in balloonet, fill air, the total measurement (volume) of balloonet accounts for the 93% of entirely wide hull volume, main gasbag
Total measurement (volume) accounts for the 7% of entirely wide hull volume.
Optimum, described pressure system includes aerator and venting valve, and aerator and venting valve are installed in single capsule
On body, aerator is used for inflating in single utricule, and venting valve is used for the venting of single utricule.
Optimum, this dirigible also includes the variable ship wing, aileron, empennage and rudder face, and two ship wings are respectively arranged in dirigible
The both sides in portion, aileron is arranged at ship wing rear portion, and aileron can adjust angle with respect to the ship wing, and empennage includes being arranged at dirigible afterbody
Double tailplanes of both sides and be arranged at dirigible afterbody top double vertical tails, rudder face is arranged at empennage rear portion, and rudder face
Angle can be adjusted with respect to empennage.
Optimum, the described ship wing is framing structure, and top is installed with the solaode of device of solar generating,
Ship wing energy folding shrinking or tiling launch, and the framing structure of the ship wing is by carbon fiber, titanium-aluminium alloy or nickel-titanium alloy material system
Become.
Optimum, this dirigible also includes ship and carries equipment protecting equipment, and ship carries equipment protecting equipment and is just difficult to dirigible is overweight
During often flight, ship load equipment is launched away, and opens the parachute being fixed on ship load equipment, protection ship carries equipment safety and
Land.
Optimum, this dirigible also includes landing buffer device, and two single utricule bottoms of both sides are respectively provided with installation to be had
Land buffer unit, described buffer unit just activates to open when dirigible lands.
Optimum, the both sides of described dirigible are installed with three vector propellers, and the fixing peace in rear portion of dirigible respectively
Equipped with two vector propellers, vector propeller uses carbon fiber skeletal support, and inside suspension screen hangs load and is arranged on dirigible.
Optimum, described device of solar generating uses thin film or non-crystal silicon solar cell.
As shown from the above technical solution, the stratospheric airship of the expanded letter adjustable wing that this utility model provides, dirigible is in flat
Shape, the length of wide hull and the ratio of width are 2.1～2.5:1, considerably increase the laying area of device of solar generating, will
Luminous energy changes into enough electrical energy drive vector propellers so that dirigible power is full, fly controllability and bearing capacity
It is obviously improved.
Brief description
Accompanying drawing 1 is the structural representation of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 2 is the top view of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 3 is the right view of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 4 is the front view of the stratospheric airship of expanded letter adjustable wing.
In figure：Single utricule 1, main gasbag 2, front balloonet 3, rear balloonet 4, the ship wing 5, aileron 6, empennage 7, rudder face 8, vector
Propeller 9, device of solar generating 10, landing buffer device 11.
Specific embodiment
In conjunction with accompanying drawing of the present utility model, the technical scheme of utility model embodiment is further elaborated.
Referring to the drawings shown in 1, the stratospheric airship of expanded letter adjustable wing includes wide hull, device of solar generating 10, vector
Propeller 9, pressure system, flight control system, the ship wing 5, aileron 6, empennage 7, rudder face 8, landing buffer device 11 and ship carry equipment and protect
Protection unit.
Referring to the drawings shown in 4, wide hull is to be formed by single utricule 1 connected combination as three, the length of wide hull with
The ratio of width is 2.1～2.5:1, a single utricule 1 is located at centre, and two single utricules 1 are located at both sides, and single utricule of centre
1 head protrudes from the head of single utricule 1 of both sides；Middle single utricule 1 horizontal level is higher than single utricule 1 of both sides, and that is, three
Individual single utricule 1 surrounds a gondola space in middle single utricule 1 bottom, and this gondola space can be placed ship and be carried equipment or institute
Want freight.
Referring to the drawings shown in 2, single utricule 1 includes main gasbag 2 and the balloonet being arranged within main gasbag 2, described pair gas
Capsule is divided into front balloonet 3 and rear balloonet 4, and main gasbag 2, front balloonet 3 and rear balloonet 4 are completed to inflate by pressure system respectively
Or deflation operations, fill helium in main gasbag 2, in balloonet, fill air, the total measurement (volume) of balloonet accounts for whole wide hull volume
93%, the total measurement (volume) of main gasbag 2 accounts for the 7% of entirely wide hull volume；Pressure system include aerator and venting valve, aerator and
Venting paired being arranged on main gasbag 2, front balloonet 3 and rear balloonet 4 of valve, aerator is used for inflating, and venting valve is used
In venting.
Installation at least 5,600 square metres of device of solar generating 10 can be laid in wide hull top, and solar electrical energy generation fills
Put 10 and use thin film or non-crystal silicon solar cell, the area coverage of solaode is 2 times about of water-drop-shaped list ship capsule.
Referring to the drawings shown in 3, vector propeller 9 is symmetrically installed on the both sides of wide hull and the rear portion of wide hull, dirigible
Both sides be installed with three vector propellers 9 respectively, and the rear portion of dirigible is installed with two vector propellers 9, one
Eight vector propellers 9 installed altogether can provide the power of 1,020KW, and vector propeller 9 uses carbon fiber skeletal support, interior
Portion's suspension screen hangs load and is arranged on dirigible；Pressure system completes inflation or the deflation operations of wide hull, and solar electrical energy generation fills
To put 10 be vector propeller 9, pressure system and flight control system are powered, flight control system respectively with device of solar generating 10, vector
Propeller 9 and pressure system electrical connection, and control device of solar generating 10, vector propeller 9 and pressure system work respectively.
Dirigible also includes the ship wing 5, aileron 6, empennage 7 and rudder face 8, two meters on the downside of thin film or non-crystal silicon solar cell edge
Place's installation settings ship wing 5, the two secondary ship wings 5 are respectively arranged at the both sides in the middle part of dirigible, and aileron 6 is arranged at the ship wing 5 rear portion, and aileron
6 can adjust angle with respect to the ship wing 5, and empennage 7 includes being arranged at double tailplanes of dirigible two sides of tail and is arranged at dirigible tail
Double vertical tails on the top in portion, rudder face 8 is arranged at empennage 7 rear portion, and rudder face 8 can adjust angle with respect to empennage 7.The ship wing 5
It is framing structure, and top is installed with the solaode of device of solar generating 10, the ship wing 5 can folding shrinking or flat
Drawout, the framing structure of the ship wing 5 is made up of carbon fiber, titanium-aluminium alloy or nickel-titanium alloy material.The sun of laying on the ship wing 5
Can provide more sufficient energy for dirigible so that the solaode area coverage of wide hull is water-drop-shaped list ship capsule 3 by battery
About times.
Single utricule 1 bottom of two of both sides is respectively provided with and is provided with landing buffer device 11, and described buffer unit is in dirigible
Just activate to open during landing；Ship carry equipment protecting equipment dirigible is overweight be difficult to normal flight when, by ship load equipment launch away,
And open the parachute being fixed on ship load equipment, protection ship carries equipment safety and lands.
The suitable length-width ratio of this dirigible makes the solaode of laying on dirigible be significantly larger than the dirigible of conventional list utricule,
There is enough power to tackle troposphere, also have enough power to adjust flight attitude, from main regulation flying height, keep necessarily high
Degree cruise, properly completes more multitask, tackles various situations.
Claims (10)
1. expanded letter adjustable wing stratospheric airship it is characterised in that：This dirigible includes wide hull, device of solar generating（10）、
Vector propeller（9）, pressure system and flight control system；The ratio of the length of described wide hull and width is 2.1～2.5:1, wide
The laying of hull top is provided with device of solar generating（10）, vector propeller（9）It is symmetrically installed on wide hull, pressure system
System completes inflation or the deflation operations of wide hull, device of solar generating（10）For vector propeller（9）, pressure system and fly
Control system power supply, flight control system respectively with device of solar generating（10）, vector propeller（9）Electrically connect with pressure system, and
Control device of solar generating respectively（10）, vector propeller（9）With pressure system work.
2. expanded letter adjustable wing according to claim 1 stratospheric airship it is characterised in that：Described wide hull is by three
Single utricule（1）Combine, a single utricule（1）It is located at centre, two single utricules（1）Positioned at both sides, and single utricule of centre
（1）Head protrude from single utricule of both sides（1）Head；Middle single utricule（1）Horizontal level is higher than single utricule of both sides
（1）, i.e. three single utricules（1）In middle single utricule（1）Bottom surrounds a gondola space.
3. expanded letter adjustable wing according to claim 2 stratospheric airship it is characterised in that：Described single utricule（1）Including
Main gasbag（2）Be arranged on main gasbag（2）Internal balloonet, described balloonet is divided into front balloonet（3）With rear balloonet
（4）, main gasbag（2）, front balloonet（3）With rear balloonet（4）Respectively inflation or deflation operations, main gas are completed by pressure system
Capsule（2）In fill helium, fill air in balloonet, the total measurement (volume) of balloonet accounts for the 93% of entirely wide hull volume, main gasbag（2）'s
Total measurement (volume) accounts for the 7% of entirely wide hull volume.
4. expanded letter adjustable wing according to claim 3 stratospheric airship it is characterised in that：Described pressure system includes rousing
Blower fan and venting valve, aerator and venting valve are installed on single utricule, and aerator is used for inflating in single utricule, venting
Valve is used for the venting of single utricule.
5. the expanded letter adjustable wing according to any one in claim 1-4 stratospheric airship it is characterised in that：This dirigible
Also include the ship wing（5）, aileron（6）, empennage（7）And rudder face（8）, two ship wings（5）It is respectively arranged at the both sides in the middle part of dirigible, secondary
The wing（6）It is arranged at the ship wing（5）Rear portion, and aileron（6）Can be with respect to the ship wing（5）Adjust angle, empennage（7）Including being arranged at dirigible
Double tailplanes of two sides of tail and the double vertical tails being arranged at dirigible afterbody top, rudder face（8）It is arranged at empennage（7）Afterwards
Portion, and rudder face（8）Can be with respect to empennage（7）Adjust angle.
6. expanded letter adjustable wing according to claim 5 stratospheric airship it is characterised in that：The described ship wing（5）It is skeleton
Structure, and top is installed with device of solar generating（10）Solaode, the ship wing（5）Can folding shrinking or tiling
Launch.
7. expanded letter adjustable wing according to claim 6 stratospheric airship it is characterised in that：This dirigible also includes ship load and sets
Standby protection device, ship carry equipment protecting equipment dirigible is overweight be difficult to normal flight when, ship load equipment is launched away, and opens
It is fixed on the parachute on ship load equipment, protection ship carries equipment safety and lands.
8. expanded letter adjustable wing according to claim 7 stratospheric airship it is characterised in that：This dirigible also includes landing delaying
Flushing device（11）, two single utricules of both sides（1）Bottom is respectively provided with and is provided with landing buffer device（11）, described buffer unit
Just activate to open when dirigible lands.
9. expanded letter adjustable wing according to claim 8 stratospheric airship it is characterised in that：The both sides of described dirigible are respectively
It is installed with three vector propellers（9）, and the rear portion of dirigible is installed with two vector propellers（9）, vector propulsion
Device（9）Using carbon fiber skeletal support, inside suspension screen hangs load and is arranged on dirigible.
10. expanded letter adjustable wing according to claim 9 stratospheric airship it is characterised in that：Described solar electrical energy generation dress
Put（10）Using thin film or non-crystal silicon solar cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620929759.2U CN205952280U (en) | 2016-08-24 | 2016-08-24 | Stratospheric dirigible of expanded letter adjustable wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620929759.2U CN205952280U (en) | 2016-08-24 | 2016-08-24 | Stratospheric dirigible of expanded letter adjustable wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205952280U true CN205952280U (en) | 2017-02-15 |
Family
ID=57977289
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620929759.2U Active CN205952280U (en) | 2016-08-24 | 2016-08-24 | Stratospheric dirigible of expanded letter adjustable wing |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639305A (en) * | 2018-06-30 | 2018-10-12 | 达天飞艇（宁夏）有限公司 | Stratospheric airship with full dynamic formula front wing and mobile counterweight |
| CN109250064A (en) * | 2018-09-29 | 2019-01-22 | 中国人民解放军国防科技大学 | Novel bionic aircraft structure with integrated buoyancy and lift high lift-drag ratio |
| CN110466730A (en) * | 2019-08-24 | 2019-11-19 | 哈尔滨工业大学 | A kind of dirigible construction design method based on air bag diaphragm and inflation ring skeleton |
| CN110979623A (en) * | 2019-12-13 | 2020-04-10 | 中国特种飞行器研究所 | Near-ground safe landing protection system for airship |
| CN111055989A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Small multi-vector airship |
| CN117614100A (en) * | 2024-01-24 | 2024-02-27 | 中国科学院空天信息创新研究院 | Aircraft energy supply control system, method, device, equipment and medium |
-
2016
- 2016-08-24 CN CN201620929759.2U patent/CN205952280U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639305A (en) * | 2018-06-30 | 2018-10-12 | 达天飞艇（宁夏）有限公司 | Stratospheric airship with full dynamic formula front wing and mobile counterweight |
| CN109250064A (en) * | 2018-09-29 | 2019-01-22 | 中国人民解放军国防科技大学 | Novel bionic aircraft structure with integrated buoyancy and lift high lift-drag ratio |
| CN110466730A (en) * | 2019-08-24 | 2019-11-19 | 哈尔滨工业大学 | A kind of dirigible construction design method based on air bag diaphragm and inflation ring skeleton |
| CN110466730B (en) * | 2019-08-24 | 2023-05-19 | 哈尔滨工业大学 | Airship structure design method based on air bag diaphragm and inflatable ring framework |
| CN110979623A (en) * | 2019-12-13 | 2020-04-10 | 中国特种飞行器研究所 | Near-ground safe landing protection system for airship |
| CN111055989A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Small multi-vector airship |
| CN117614100A (en) * | 2024-01-24 | 2024-02-27 | 中国科学院空天信息创新研究院 | Aircraft energy supply control system, method, device, equipment and medium |
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| GR01 | Patent grant |