CN109720534A - A kind of stratospheric airship - Google Patents
A kind of stratospheric airship Download PDFInfo
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- CN109720534A CN109720534A CN201910148447.6A CN201910148447A CN109720534A CN 109720534 A CN109720534 A CN 109720534A CN 201910148447 A CN201910148447 A CN 201910148447A CN 109720534 A CN109720534 A CN 109720534A
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- stratospheric airship
- mount
- air bag
- power system
- rigid frame
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- 238000005183 dynamical system Methods 0.000 claims abstract description 21
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 15
- 239000001307 helium Substances 0.000 claims description 12
- 229910052734 helium Inorganic materials 0.000 claims description 12
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 9
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 239000002002 slurry Substances 0.000 claims description 4
- 238000009434 installation Methods 0.000 abstract description 12
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 238000005516 engineering process Methods 0.000 abstract description 3
- 239000000463 material Substances 0.000 description 14
- 238000000034 method Methods 0.000 description 9
- 239000007789 gas Substances 0.000 description 8
- 238000013461 design Methods 0.000 description 7
- 239000005437 stratosphere Substances 0.000 description 6
- 239000010410 layer Substances 0.000 description 5
- 230000005855 radiation Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000005611 electricity Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000002775 capsule Substances 0.000 description 3
- 239000002346 layers by function Substances 0.000 description 3
- 238000004364 calculation method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000001447 compensatory effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
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- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention relates to airship technology fields, provide a kind of stratospheric airship, and the stratospheric airship includes: rigid frame, are formed in hull surface；And mount for power system, the mount for power system include the truss structure in prism-frustum-shaped, wherein the bottom of truss structure is overlapped on rigid frame；And the top of truss structure is for installing dynamical system.The present invention is by overlapping mount for power system on rigid frame, it overcomes the shortcomings that gondola installation mount for power system in stratospheric airship bottom is also easy to produce wave motion, making the wave motion trend of stratospheric airship horizontal flight is inhibited, to reduce bottom gondola resistance, reduces power energy consumption.Meanwhile keeping truss structure more stable by the support force and pulling force of the pulling force of more oblique pull tensioning ropes or more oblique pull supporting rods.In addition, improving the anti-superpressure ability of dirigible by the rigid frame constituted using rigid reinforcing ring and rod piece.
Description
Technical field
The present invention relates to airship technology fields, and in particular to a kind of stratospheric airship.
Background technique
The phenomenon that there are over-temp and over-pressures due to the influence stratospheric airship of solar radiation under stratosphere environment, for advection
The overall system design of layer dirigible proposes high requirement.According to the existing soft knot of the hot simulation calculation of stratospheric airship finite element
The stratospheric airship thermal balance temperature difference of structure is greater than the heat resistance of stratospheric airship, is easy to appear the phenomenon that safety coefficient is less than 1.
This result may generate subversive influence to the development of stratospheric airship.Solving the problems, such as stratospheric airship over-temp and over-pressure is
Stratospheric airship one of problem in the urgent need to address is developed at present.
Specifically: 1, over-temp and over-pressure refers to stratospheric airship in working depth internal air temperature liter after by solar radiation
The phenomenon that ship inside and outside differential pressure that height causes gas expansion to be formed is more than dirigible scope of design.2, the thermal balance temperature difference refers to using limited
First thermal analysis software simulation calculation go out stratospheric airship after by solar radiation full ship highest mean value temperature and night full ship it is minimum
The difference of mean value temperature.3, heat resistance refer to stratospheric airship in working depth the stratospheric airship utricule after solar radiation
Intensity can endure the limiting value of gas average temperature rising in dirigible.4, when three balances refer to stratospheric system totality Top-layer Design Method
The energy balance of use, thermal balance, weight balancing, these three balances intercouple: energy balance refers to stratospheric airship in work
Make height and work region round the clock between generated power of solar cell and battery electric power storage total amount must satisfy stratosphere fly
Ship round the clock between wind resistance institute's electricity demand and the electricity consumption of dirigible system and task system electricity consumption total electricity；Thermal balance refers to stratosphere
Dirigible working depth after by solar radiation internal air temperature raising cause internal gas to expand the ship internal and external pressure difference to be formed
No more than the pressure-resistant range of dirigible design；Weight balancing refers to that stratospheric airship is equal in the air quality that working depth arranges
Gaseous mass in stratospheric airship quality and ship.
And it is generally empty using soft structure and in addition air bag storage helium, the storage of interior air bag in the stratospheric airship ground at present
The mode of gas needs to solve the superthermal On The Problem Of Overpressure of stratospheric airship by reinforcing envelop materials tensile resistance come compensatory,
Bring envelop materials overweight and increased costs problem.
Meanwhile general low-to-medium altitude dirigible is all gondola to be placed on to bottom, and use and be mounted on mount for power system
Method on gondola.Engine support is placed on and crosses general goal apart from dirigible centre of buoyancy downwards by this method, unreasonable due to being laid out
Propulsion system efficiency is seriously affected；The influence of torque easily occurs the wave of dipping and heaving in dirigible horizontal flight simultaneously
Formula state of flight, this wave state of flight need to pay more energy relative to the stratospheric airship of horizontal flight.And
Since bottom gondola is prominent, dirigible resistance coefficient is increased, also dirigible is further made to need to pay more energy.
American lockheed Martin Corporation uses blimp installation two in terms of stratosphere blimp master-plan
The method of side engine support.Vertical rod is specifically stood on into the blimp external surface with gas stiffness by collet.
Then binding in wire is pulled out by the external door curtain made of cloth and is divided into multiple directions tension vertical rod, connection dynamical system installation at the top of vertical rod
Dynamical system is mounted on mounting platform by platform.But this method must be set up making more greatly in stratospheric airship inside and outside differential pressure
The outer utricule of dirigible, which reaches certain gas elastic stiffness, to be carried out.And the external door curtain made of cloth causes the resistance coefficient of stratospheric airship to increase
Greatly.
Therefore, designing a kind of new structural stratospheric airship is a technical problem to be solved urgently.
Summary of the invention
The present invention provides a kind of stratospheric airship, so overcome at least to a certain extent due to the relevant technologies limitation and
One or more problem caused by defect.
Other characteristics and advantages of the invention will be apparent from by the following detailed description, or partially by the present invention
Practice and acquistion.
An example embodiment according to the present invention, discloses a kind of stratospheric airship, and the stratospheric airship includes:
Rigid frame is formed in hull surface；And
Mount for power system, the mount for power system include the truss structure in prism-frustum-shaped, wherein
The bottom of truss structure is overlapped on rigid frame；And
The top of truss structure is for installing dynamical system.
An example embodiment according to the present invention, wherein the top of truss structure is linked with dynamical system fixed platform,
Dynamical system is mounted in dynamical system fixed platform.
An example embodiment according to the present invention, wherein dynamical system includes blade and motor.
An example embodiment according to the present invention, wherein terrace with edge is triangular platform, truncated rectangular pyramids or five terrace with edges.
An example embodiment according to the present invention, the mount for power system further include more oblique pull tensioning ropes, are appointed
It is bound respectively with rigid frame and truss structure at the both ends of one oblique pull tensioning rope.
An example embodiment according to the present invention, wherein oblique pull tensioning rope includes tensioning steel wire.
An example embodiment according to the present invention, the mount for power system further include more oblique pull supporting rods, are appointed
The both ends of one oblique pull supporting rod are linked with rigid frame and truss structure respectively.
An example embodiment according to the present invention, wherein the quantity of the mount for power system is even number, difference position
In the two sides of stratospheric airship.
An example embodiment according to the present invention, wherein the mount for power system is located at the tail portion of stratospheric airship.
An example embodiment according to the present invention, wherein rigid frame is located at hull surface wholly or partially.
An example embodiment according to the present invention, wherein rigid frame is made of reinforcing ring and rod piece.
An example embodiment according to the present invention, the stratospheric airship further include: interior air bag, filled with helium in interior air bag
Gas；And the outer air bag of interior air bag is surrounded, filled with air in the space between the utricule of outer air bag and the utricule of interior air bag, wherein
Rigid frame is formed in the outer surface of outer air bag.
An example embodiment according to the present invention, wherein interior air bag is by multiple along the cabin that dirigible is axially successively arranged
Air bag is constituted.
An example embodiment according to the present invention, the stratospheric airship further include Non-tailstock empennage and course tail slurry.
According to certain embodiments of the present invention, it by overlapping mount for power system on rigid frame, overcomes flat
Fluid layer dirigible bottom gondola installation mount for power system causes propulsion system to be laid out unreasonable the shortcomings that being also easy to produce wave motion, makes
The wave motion trend of stratospheric airship horizontal flight is inhibited, to reduce bottom gondola resistance, reduces power energy consumption.
Other embodiments according to the present invention pass through the pulling force or more oblique pull support rods of more oblique pull tensioning ropes
The support force and pulling force of part keep truss structure more stable.
Other embodiments according to the present invention pass through rigid frame, the rope constituted using rigid reinforcing ring and rod piece
The hard and soft mixed structure of the compositions such as rope and high-intensitive outer air bag envelop materials, improves the anti-superpressure ability of outer air bag.
Other embodiment according to the present invention is set by the intracapsular utricule for setting subdivision of air bag, helium outside zero-pressure superpressure
Meter scheme improves the utilization rate of envelop materials intensity.
It should be understood that the above general description and the following detailed description are merely exemplary, this can not be limited
Invention.
Detailed description of the invention
Its example embodiment is described in detail by referring to accompanying drawing, above and other target of the invention, feature and advantage will
It becomes more fully apparent.
Fig. 1 shows the 3 D stereo of the mount for power system of the stratospheric airship of an example embodiment according to the present invention
Figure.
Fig. 2 shows the mount for power system of the stratospheric airship of an example embodiment according to the present invention in stratospheric airship
The front view of upper installation site.
Fig. 3 shows the mount for power system of the stratospheric airship of an example embodiment according to the present invention in stratospheric airship
The side view of upper installation site.
Fig. 4 shows the side view see-through view of the stratospheric airship of an example embodiment according to the present invention.
Specific embodiment
Example embodiment is described more fully with reference to the drawings.However, example embodiment can be real in a variety of forms
It applies, and is not understood as limited to embodiment set forth herein；On the contrary, thesing embodiments are provided so that the present invention will be comprehensively and complete
It is whole, and the design of example embodiment is comprehensively communicated to those skilled in the art.Identical appended drawing reference indicates in figure
Same or similar part, thus repetition thereof will be omitted.
In addition, described feature, structure or characteristic can be incorporated in one or more implementations in any suitable manner
In example.In the following description, many details are provided to provide and fully understand to the embodiment of the present invention.However,
It will be appreciated by persons skilled in the art that technical solution of the present invention can be practiced without one or more in specific detail,
Or it can be using other methods, constituent element, device, step etc..In other cases, it is not shown in detail or describes known side
Method, device, realization or operation are to avoid fuzzy each aspect of the present invention.
Block diagram shown in the drawings is only functional entity, not necessarily must be corresponding with physically separate entity.
I.e., it is possible to realize these functional entitys using software form, or realized in one or more hardware modules or integrated circuit
These functional entitys, or these functional entitys are realized in heterogeneous networks and/or processor device and/or microcontroller device.
Flow chart shown in the drawings is merely illustrative, it is not necessary to including all content and operation/step,
It is not required to execute by described sequence.For example, some operation/steps can also decompose, and some operation/steps can close
And or part merge, therefore the sequence actually executed is possible to change according to the actual situation.
It should be understood that although herein various assemblies may be described using term first, second, third, etc., these groups
Part should not be limited by these terms.These terms are to distinguish a component and another component.Therefore, first group be discussed herein below
Part can be described as the second component without departing from the teaching of concept of the present invention.As used herein, term " and/or " include associated
All combinations for listing any of project and one or more.
It will be understood by those skilled in the art that attached drawing is the schematic diagram of example embodiment, module or process in attached drawing
Necessary to not necessarily implementing the present invention, therefore it cannot be used for limiting the scope of the invention.
It is an object of the invention to disclose a kind of stratospheric airship, the stratospheric airship includes: rigid frame, is formed in
Hull surface；And mount for power system, the mount for power system include the truss structure in prism-frustum-shaped, wherein truss structure
Bottom be overlapped on rigid frame；And the top of truss structure is for installing dynamical system.The present invention passes through in rigid frame
Mount for power system is overlapped on frame, is overcome and is also easy to produce wave motion in stratospheric airship bottom gondola installation mount for power system
The shortcomings that, so that the wave motion trend of stratospheric airship horizontal flight is inhibited, to reduce bottom gondola resistance, reduces dynamic
Power energy consumption.Meanwhile keeping truss structure more stable by more oblique pull tensioning rope/oblique pull support rod pulling force/support forces.This
Outside, by the rigid frame constituted using rigid reinforcing ring and rod piece, the anti-superpressure ability of dirigible external capsule is improved.Further,
By the intracapsular utricule design scheme for setting subdivision of air bag, helium outside zero-pressure superpressure, the utilization rate of envelop materials intensity is improved.
The mount for power system of stratospheric airship of the invention is specifically described with reference to the accompanying drawing, wherein Fig. 1 shows
The 3 dimensional drawing of the mount for power system of the stratospheric airship of an example embodiment according to the present invention out；Fig. 2 shows bases
The front view of mount for power system installation site on stratospheric airship of the stratospheric airship of an example embodiment of the invention；
Fig. 3 shows the mount for power system of the stratospheric airship of an example embodiment according to the present invention installation position on stratospheric airship
The side view set；Fig. 4 shows the front perspective view of the stratospheric airship of an example embodiment according to the present invention.
As shown in Figure 1-3, stratospheric airship includes: rigid frame 5, it is formed in hull surface；And mount for power system,
The mount for power system includes the truss structure 2 in prism-frustum-shaped, in which: the bottom of truss structure 2 is overlapped on rigid frame 5
On；And the top of truss structure 2 is for installing dynamical system.The present invention on rigid frame by overlapping dynamical system branch
Frame overcomes the shortcomings that gondola installation mount for power system in stratospheric airship bottom is also easy to produce wave motion, flies stratosphere
The wave motion trend of ship horizontal flight is inhibited, to reduce bottom gondola resistance, reduces power energy consumption.
An example embodiment according to the present invention, the wherein top of truss structure 2 and 6 chain of dynamical system fixed platform
It connects, dynamical system is mounted in dynamical system fixed platform 6.
An example embodiment according to the present invention, wherein dynamical system includes blade 3 and motor 4.But the present invention is unlimited
In this, it is also possible to other kinds of dynamical system.
An example embodiment according to the present invention, wherein terrace with edge is triangular platform, truncated rectangular pyramids or five terrace with edges ... etc., according to need
Depending on wanting, it is not limited to them.
An example embodiment according to the present invention, the mount for power system further include more oblique pull tensioning ropes/tiltedly
Draw supporting rod 1, the both ends of any oblique pull tensioning rope/oblique pull supporting rod respectively with rigid frame and truss structure binding/
It is fixed.Keep truss structure more stable by more oblique pull tensioning rope/oblique pull supporting rod pulling force/support forces.
An example embodiment according to the present invention, wherein oblique pull tensioning rope/oblique pull supporting rod 1 includes tensioning steel
Silk/carbon fibre member bar depending on also can according to need, is not limited to them, for example oblique pull tensioning rope is also possible to by other
Rope with high-intensitive and certain elasticity while elastic metallic yarn or carbon fiber are constituted.
Meanwhile being opened close to tensioning steel wire/rod piece of blade to both sides oblique pull, to avoid blade and tensioning steel wire/rod piece
Movement interference.
An example embodiment according to the present invention, wherein the quantity of the mount for power system is that even number (such as can be
2,4 or 6 ... is a etc.), it is located at the two sides of stratospheric airship.
An example embodiment according to the present invention, wherein the mount for power system is located at the tail portion of stratospheric airship.
That is, can be according to specific propulsion mode/dynamical system arrangement of stratospheric airship by dynamical system
Bracket is set to the two sides of stratospheric airship, the tail portion of stratospheric airship or the two sides and the tail that are set to stratospheric airship simultaneously
Portion.
An example embodiment according to the present invention, wherein rigid frame is located at hull surface wholly or partially.?
That is mount for power system of the invention be not limited to be applied only to rigid stratospheric airship (hull surface it is whole
Stratospheric airship with rigid frame) on, the rigid outer framework in part (such as only ring can be also arranged on soft stratospheric airship
Around the rigid outer framework of annular of a certain section of kayak body, without being the rigid outer framework for surrounding or surrounding entire kayak body), utilize part
The rigidity installation mount for power system of rigid outer framework structure.
An example embodiment according to the present invention, wherein rigid frame 5 is made of reinforcing ring 51 and rod piece 52.Pass through benefit
The rigid frame constituted with rigid reinforcing ring and rod piece, can be improved the anti-superpressure ability of dirigible.
An example embodiment according to the present invention, wherein reinforcing ring can rigid material composition.Specifically, reinforcing ring can
It selects by having certain rigidity and material elastic and that weight is lighter to constitute.
An example embodiment according to the present invention, the stratospheric airship further include: interior air bag 9, in interior air bag filled with
Helium；And in surrounding air bag outer air bag 8, filled with air in the space between the utricule of outer air bag and the utricule of interior air bag,
Wherein the outer surface of the utricule of outer air bag forms the surface of the rigid stratospheric airship, and rigid frame 5 is formed in outer air bag
Outer surface.
The power of the stratospheric airship of the air bag layout type of outer air bag storage helium, interior air bag storage air of the invention
System frame structure as the utricule of outer air bag eliminate anti-helium leakage functional layer necessary to traditional stratospheric airship and
Enhance stress layer, therefore the intensity of outer air bag envelop materials is improved in same outer air bag envelop materials surface density.
Further, around outer 8 outer surface of air bag, setting covers in other words in outer gas multiple reinforcing rings 51 in rigid frame 5
Capsule outer surface, to further improve the anti-superpressure ability of outer air bag.
It can see by above example embodiment, the mount for power system of stratospheric airship of the invention utilizes rigidity
The hard and soft mixed structure of the compositions such as frame and high-intensitive outer capsule material that reinforcing ring and rod piece are constituted, improves the anti-of outer air bag
Superpressure ability.
An example embodiment according to the present invention, wherein interior air bag 9 is by multiple along the cabin that dirigible is axially successively arranged
Interior air bag 10 is constituted.
An example embodiment according to the present invention, the isolation rope maintained between air bag by reinforcing ring in two neighboring cabin
The isolation (as shown in Figure 4) of rope 13.
An example embodiment according to the present invention, wherein the utricule of interior air bag includes that anti-helium leakage functional layer (is not schemed
Show).
An example embodiment according to the present invention, wherein the utricule of outer air bag does not include anti-helium leakage functional layer, from
And it reduces costs and weight.
An example embodiment according to the present invention, wherein outer air bag is the outer air bag of zero-pressure superpressure.
It can see by above example embodiment, the mount for power system of stratospheric airship of the invention passes through zero-pressure
Superpressure outer air bag, the intracapsular utricule design scheme for setting subdivision of helium, improve the utilization rate of envelop materials intensity.Simultaneously also further
Improve the overall security, reliability and damage pipe ability of the mount for power system of stratospheric airship.
The safety evaluation that carried out to the utricule structure of stratospheric airship of the invention the result shows that:
1, the requirement of superthermal superpressure can be met in superthermal situation.
2, reinforcing ring and rope constraint are increased, the requirement to envelop materials reduces.
Conclusion: the superthermal superpressure countermeasure of the mount for power system scheme of stratospheric airship of the invention is effective, and same
When reduce weight and cost.
An example embodiment according to the present invention, the stratospheric airship further include Non-tailstock empennage 11 and course tail slurry
12, wherein course tail slurry 12 is used to change the course of dirigible.
By above detailed description, those skilled in the art is it can be readily appreciated that stratosphere according to an embodiment of the present invention
Dirigible has one or more of the following advantages.
According to certain embodiments of the present invention, it by overlapping mount for power system on rigid frame, overcomes flat
Fluid layer dirigible bottom gondola installation mount for power system causes propulsion system to be laid out unreasonable the shortcomings that being also easy to produce wave motion, makes
The wave motion trend of stratospheric airship horizontal flight is inhibited, to reduce bottom gondola resistance, reduces power energy consumption.
According to certain embodiments of the present invention, pass through the pulling force or more oblique pull supporting rods of more oblique pull tensioning ropes
Support force and pulling force keep truss structure more stable.
Other embodiments according to the present invention pass through rigid frame, the rope constituted using rigid reinforcing ring and rod piece
The hard and soft mixed structure of the compositions such as rope and high-intensitive outer air bag envelop materials, improves the anti-superpressure ability of outer air bag.
Other embodiment according to the present invention is set by the intracapsular utricule for setting subdivision of air bag, helium outside zero-pressure superpressure
Meter scheme improves the utilization rate of envelop materials intensity.
Those skilled in the art after considering the specification and implementing the invention disclosed here, will readily occur to of the invention its
Its embodiment.This application is intended to cover any variations, uses, or adaptations of the invention, these modifications, purposes or
Person's adaptive change follows general principle of the invention and including the undocumented common knowledge in the art of the present invention
Or conventional techniques.The description and examples are only to be considered as illustrative, and true scope and spirit of the invention are by proposing
Claim is pointed out.
It should be understood that the present invention is not limited to the precise structure already described above and shown in the accompanying drawings, and
And various modifications and changes may be made without departing from the scope thereof.The scope of the present invention is limited only by the attached claims.
Claims (14)
1. a kind of stratospheric airship, which is characterized in that the stratospheric airship includes:
Rigid frame is formed in hull surface；And
Mount for power system, the mount for power system include the truss structure in prism-frustum-shaped, wherein
The bottom of truss structure is overlapped on rigid frame；And
The top of truss structure is for installing dynamical system.
2. stratospheric airship according to claim 1, which is characterized in that wherein the top of truss structure and motor are fixed flat
The chain of stations connects, and dynamical system is mounted in motor fixed platform.
3. stratospheric airship according to claim 2, which is characterized in that wherein dynamical system includes blade and motor.
4. stratospheric airship according to claim 1 to 3, which is characterized in that wherein terrace with edge is triangular platform, tetragonous
Platform or five terrace with edges.
5. stratospheric airship according to claim 1 to 3, which is characterized in that the mount for power system further includes
More oblique pull tensioning ropes, the both ends of any oblique pull tensioning rope are bound with rigid frame and truss structure respectively.
6. according to the stratospheric airship any in claim 5, which is characterized in that wherein oblique pull tensioning rope includes tensioning
Steel wire.
7. stratospheric airship according to claim 1 to 3, which is characterized in that the mount for power system further includes
The both ends of more oblique pull supporting rods, any oblique pull supporting rod are linked with rigid frame and truss structure respectively.
8. stratospheric airship according to claim 1 to 3, which is characterized in that the wherein mount for power system
Quantity is even number, is located at the two sides of stratospheric airship.
9. stratospheric airship according to claim 1 to 3, which is characterized in that the wherein mount for power system position
In the tail portion of stratospheric airship.
10. stratospheric airship according to claim 1, which is characterized in that wherein rigid frame is located at the office on hull surface
Portion.
11. according to claim 1 or stratospheric airship described in 10, which is characterized in that wherein rigid frame is by reinforcing ring and bar
Part is constituted.
12. according to claim 1 or stratospheric airship described in 10, further includes:
Interior air bag, filled with helium in interior air bag；And
The outer air bag of air bag in surrounding, filled with air in the space between the utricule of outer air bag and the utricule of interior air bag, wherein firmly
Formula frame is formed in the outer surface of outer air bag.
13. stratospheric airship according to claim 12, which is characterized in that in wherein air bag by it is multiple along dirigible it is axial according to
Air bag is constituted in the cabin of secondary arrangement.
14. stratospheric airship according to claim 1 to 3, which is characterized in that further include Non-tailstock empennage and boat
To tail slurry.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910148447.6A CN109720534A (en) | 2019-02-28 | 2019-02-28 | A kind of stratospheric airship |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910148447.6A CN109720534A (en) | 2019-02-28 | 2019-02-28 | A kind of stratospheric airship |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111806668A (en) * | 2020-07-17 | 2020-10-23 | 上海交通大学 | Semi-rigid type fish bone structure airship based on bionics |
| CN114379761A (en) * | 2022-02-17 | 2022-04-22 | 青岛飞宇航空科技有限公司 | Structure of rigid support of air bag |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070034740A1 (en) * | 2005-08-12 | 2007-02-15 | Li Hiu Y | Transformable airship |
| US20070075184A1 (en) * | 2005-10-05 | 2007-04-05 | Marimon Thomas L | Direct mounted propulsion for non-rigid airships |
| US20100001128A1 (en) * | 2008-07-07 | 2010-01-07 | Morehead John P | Retracting Air Cushioned Landing System for Air Vehicles |
| CN104590533A (en) * | 2014-12-24 | 2015-05-06 | 中国特种飞行器研究所 | Novel deformable airship |
| CN106240785A (en) * | 2016-08-24 | 2016-12-21 | 达天飞艇（宁夏）有限公司 | The method of the stratospheric airship stable state lifting of auxiliary liter of balloon belt expanded letter adjustable wing |
| CN107672774A (en) * | 2017-08-24 | 2018-02-09 | 北京航空航天大学 | A kind of dirigible motor helical oar light structures device |
| CN108725741A (en) * | 2018-05-31 | 2018-11-02 | 北京空天高科技有限公司 | A kind of new structural rigid stratospheric airship |
| CN109050866A (en) * | 2018-06-29 | 2018-12-21 | 范超然 | A kind of dirigible |
| CN209600780U (en) * | 2019-02-28 | 2019-11-08 | 北京空天高科技有限公司 | A kind of mount for power system of stratospheric airship |
| CN209852555U (en) * | 2019-02-28 | 2019-12-27 | 北京空天高科技有限公司 | Stratospheric airship |
-
2019
- 2019-02-28 CN CN201910148447.6A patent/CN109720534A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070034740A1 (en) * | 2005-08-12 | 2007-02-15 | Li Hiu Y | Transformable airship |
| US20070075184A1 (en) * | 2005-10-05 | 2007-04-05 | Marimon Thomas L | Direct mounted propulsion for non-rigid airships |
| US20100001128A1 (en) * | 2008-07-07 | 2010-01-07 | Morehead John P | Retracting Air Cushioned Landing System for Air Vehicles |
| CN104590533A (en) * | 2014-12-24 | 2015-05-06 | 中国特种飞行器研究所 | Novel deformable airship |
| CN106240785A (en) * | 2016-08-24 | 2016-12-21 | 达天飞艇（宁夏）有限公司 | The method of the stratospheric airship stable state lifting of auxiliary liter of balloon belt expanded letter adjustable wing |
| CN107672774A (en) * | 2017-08-24 | 2018-02-09 | 北京航空航天大学 | A kind of dirigible motor helical oar light structures device |
| CN108725741A (en) * | 2018-05-31 | 2018-11-02 | 北京空天高科技有限公司 | A kind of new structural rigid stratospheric airship |
| CN109050866A (en) * | 2018-06-29 | 2018-12-21 | 范超然 | A kind of dirigible |
| CN209600780U (en) * | 2019-02-28 | 2019-11-08 | 北京空天高科技有限公司 | A kind of mount for power system of stratospheric airship |
| CN209852555U (en) * | 2019-02-28 | 2019-12-27 | 北京空天高科技有限公司 | Stratospheric airship |
Non-Patent Citations (1)
| Title |
|---|
| 赵新路: "平流层飞艇总体设计优化方法研究", 《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》, no. 01, pages 1 - 78 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111806668A (en) * | 2020-07-17 | 2020-10-23 | 上海交通大学 | Semi-rigid type fish bone structure airship based on bionics |
| CN111806668B (en) * | 2020-07-17 | 2022-06-03 | 上海交通大学 | Semi-hard formula fish bone structure dirigible based on it is bionical |
| CN114379761A (en) * | 2022-02-17 | 2022-04-22 | 青岛飞宇航空科技有限公司 | Structure of rigid support of air bag |
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