CN106394853A - Airship - Google Patents
Airship Download PDFInfo
- Publication number
- CN106394853A CN106394853A CN201510799977.9A CN201510799977A CN106394853A CN 106394853 A CN106394853 A CN 106394853A CN 201510799977 A CN201510799977 A CN 201510799977A CN 106394853 A CN106394853 A CN 106394853A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- dirigible
- air bag
- cabin
- wing
- 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.)
- Pending
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Classifications
-
- 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
- B64B1/60—Gas-bags surrounded by separate containers of inert gas
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention discloses an airship which comprises a fuselage air bag and fuselage back wing air bags. A horizontal space structure cabin is arranged in a fuselage belly. The fuselage back wing air bags are arranged on the airship, the length of the airship is reduced, and left and right swinging of the airship is stabilized; and the cabin is arranged at the bottom in the fuselage belly, and the good streamline surface is obtained by the airship.
Description
Technical field
The present invention relates to a kind of airflight device, belong to dirigible field.
Background technology
Dirigible belongs to one kind of aerostatics, is the aviation providing lift using the gas being lighter than air
Device.The lighter-than-air gas that the lift that dirigible obtains is full of essentially from its inside, such as hydrogen, helium
Gas etc..The general all more preferable helium of safety in utilization of modern dirigible are providing lift.Electromotor provides
Power is used primarily in dirigible and moves horizontally.
Typically from structure, dirigible can be divided into three types:Rigid airship, blimp and soft
Formula dirigible;Rigid airship generally has rigid skeleton, be provided with skeleton multiple non-pressurized air chambers or
Balloon is to provide lift, and generally the internal pressure not against air chamber to maintain their shape;Half
Rigid airship generally maintains their shape using some pressure in air bag, but also can have gas
Capsule base section skeleton;Non- rigid airship generally keeps theirs using the pressure exceeding ambient air pressure
Shape.Also have mixed type dirigible, the element of other type airship can be added, including for supporting load
Skeleton.Mixed type dirigible can also be the dirigible overweighting air, therefore can be with their propulsion system
Keep aloft lift with shape to produce.Dirigible divides someone and nobody two classes, also fastens and does not fasten
System is not.The range of application that dirigible is commonly used include Standard, carry out communicating, environmental monitoring, advertisement
Publicity, scientific research etc. service.
Content of the invention
The invention provides a kind of manned airship, it is mainly used in manned gliding.
A kind of dirigible, including fuselage, is that one or more air bags are constituted, is made up of gas impermeable material,
As artificial materials such as terylene, dacrons, in air bag, it is filled with the gas lighter than atmospheric density;Fuselage
Abdominal part is provided with multiple fin air bags, and fin air bag is connected with setting rope band between cabin, in cabin
Operation rope band adjusts fin bladder shape and controls heading, when fin air bag can be used for dirigible landing,
Dirigible and the strong point on ground;Fuselage both sides can be provided with inflatable wing, is provided with wing in wing
Support arm;Fuselage is ellipse, and length and width ratio are more than 1, and width is more than 1 with aspect ratio.
One or more fuselage ridge wings, the fuselage ridge wing is made up of air bag, positioned at fuselage air bag back,
It is made up of gas impermeable material, in air bag, be filled with the gas lighter than atmospheric density;The fuselage ridge wing and machine
As demountable structure, the fuselage ridge wing MM loading capacity of different volumes can be chosen.
Cabin is located at fuselage air bag abdominal part inner bottom part, and cabin top comprises concave shape and cabin top edge tool
There is steam vent, prevent gas gas in fuselage air bag from assembling in nacelle top, cabin top is recessed can be set
It is placed in front portion or the rear portion of cabin;In cabin, manned mode includes for horizontal, and the number that carries is single
People or double, cabin is provided with skeleton for moulding, and cabin skeleton can be connected with wing frame arm.
It is provided with personnel locus scalable device in cabin, for adjusting the center of gravity of dirigible, controlled with this winged
Ship heading.
It is provided with suspender belt in fuselage air bag, connect cabin and fuselage ridge wing air bag, be used for preventing fuselage
Air bag excessive deformation because of nacelle weight.The fuselage air bag afterbody of dirigible or abdominal part can be provided with non-gas
The wing of bellows, for balancing or adjusting heading.Dirigible is provided with power set, positioned at fuselage
The back of air bag, avris, abdominal part or afterbody, when power set are located at afterbody, afterbody sets
It is equipped with auxiliary balloon and adjusts aft weight balance, fuselage air bag and fuselage ridge wing balloon surface can set
It is equipped with solar attachment and storage device, is that power set are powered, dynamic control is set in cabin
Device processed, for controlling size switch and the airship flight direction of power set.Dirigible can be provided with
Balloonet, balloonet for isolating construction and can be connected with safety rope with dirigible, and balloonet lifting flies
Ship highly after separate with dirigible, balloonet is reclaimed by safety rope;Balloonet may be located at nacelle top,
Nacelle top balloonet can be exitted, for adjusting dirigible weight.Dirigible can be connected with safety rope, flies
Ship safety rope can also provide electric power for dirigible simultaneously, and dirigible safety rope can be connected with weight balancing
Chain, is contacted to earth by moiety by weight balancing chain and adjusts dirigible weight.Dirigible of the present invention not to rigid, half
Rigid, soft and mixed type is limited.
A kind of dirigible of the present invention, is provided with fuselage ridge wing air bag, reduces the length of dirigible, subtract
Lack dirigible radius of turn, improve the mobility of dirigible;Cabin is located at belly inner bottom part, carries
Supply good stream shape surface, decrease resistance and the thrust power of airship flight;By at back
Power set can be placed in fuselage back and both sides, thus reducing by setting twin fuselage ridge wing air bag
Power set top-heavy impact for dirigible, can also reduce the pendulum in navigation tangent plane direction for the dirigible
Dynamic;Because fuselage ridge wing air bag exist, by be provided with fuselage air bag suspender belt connect cabin and
Fuselage ridge wing air bag, can prevent fuselage air bag because of nacelle weight excessive deformation, can also simultaneously
Form concave space in fuselage air bag abdominal part to be used for forming cabin;Dirigible of the present invention is mainly used in single flying
OK, by fuselage air bag suspender belt, can form, in belly, the cabin including horizontal space structure.
Brief description
Fig. 1 is the side schematic view of the first dirigible of the present invention;Fig. 2 is the first dirigible of the present invention
Front schematic view;Fig. 3 is the side schematic view of second dirigible of the present invention;Fig. 4 is the present invention second
Plant the front schematic view of dirigible;Fig. 5 is the first generalized section with second dirigible of the present invention;
Fig. 6 is that the cabin skeleton of second dirigible of the present invention is connected with power set schematic diagram.Wherein, 1,
Fuselage air bag;2nd, fuselage ridge wing air bag;3rd, cabin;4th, power set;5th, fin air bag;
Suspender belt in 6 fuselage air bags;7, cabin skeleton.
Specific embodiment
Fig. 1 and Fig. 2 is side and the front schematic view of the first dirigible of the present invention;Fig. 5 is the present invention
The generalized section of the first dirigible, describes the present invention's in detail with reference to Fig. 1, Fig. 2 and Fig. 5
Device.Dirigible fuselage air bag 1 height shown in Fig. 1 is 2.3 meters, 7 meters of length, and width is 5 meters,
Air bag is made up of polyester fiber, is filled with helium, as depicted in figs. 1 and 2 in air bag;Fuselage air bag
1 back is provided with two fuselage ridge wing air bags 2, highly for 3 meters, 1.7 meters of width, and length is 6
Rice, air bag is made up of polyester fiber, is filled with helium, as depicted in figs. 1 and 2 in air bag;Fuselage
It is provided with suspender belt 6 in fuselage air bag, as shown in figure 5, it connects fuselage ridge wing air bag in air bag 1
2 and cabin 3, cabin 3 is located at fuselage air bag 1 bottom, is embedded in fuselage, cabin 3 bottom is
The moulding frame of aluminum, is to upwarp structure before and after cabin 3 top, and is provided with steam vent, be used for preventing machine
Body airbag gas are assembled in nacelle top;Fuselage air bag 1 abdominal part is provided with 4 fin air bags 5, such as
Shown in Fig. 1 and Fig. 2, fin air bag 5 contacts to earth when can land as dirigible the strong point;Fin air bag
5 can arrange the volume with increasing, and can be with analogy fuselage ridge wing air bag 2, now fin
Air bag 5 can be provided with connecting rope and be connected with cabin 3, and in cabin, human pilot can pass through connecting rope
Adjust fin air bag 5 shape, to control dirigible to navigate by water direction up and down with this;Refer herein to fish
Fin air bag 5 can be replaced using the non-gasbag-type fin wing.Dirigible can be connected with safety rope, safety rope
Can be fixed on guide rail and mobile object, be navigated by water by safe wire saws with this dirigible.
Fig. 3 and Fig. 4 is side and the front schematic view of second dirigible of the present invention;Fig. 5 is the present invention
The generalized section of second dirigible, describes the present invention in detail with reference to Fig. 3, Fig. 4 and Fig. 5
Device.Dirigible fuselage air bag 1 height shown in Fig. 3 is 2.3 meters, 7 meters of length, and width is
5 meters, air bag is made up of polyester fiber, is filled with helium, as shown in Figure 3 and Figure 4 in air bag;
Fuselage air bag 1 back is provided with two fuselage ridge wing air bags 2, highly for 3 meters, width 1.7
Rice, length is 6 meters, and air bag is made up of polyester fiber, is filled with helium in air bag, such as Fig. 3 and
Shown in Fig. 4;It is provided with suspender belt 6 in fuselage air bag, as shown in figure 5, it is even in fuselage air bag 1
Pick and carry ridge wing air bag 2 and cabin 3 on the body, cabin 3 is located at fuselage air bag 1 bottom, embedded fuselage
In air bag, cabin 3 bottom is aluminum cabin skeleton 7, and wherein two skeletons upwarp and are fixed with a left side
Right each two power set 4 are propeller, and as shown in Fig. 6, Fig. 3 and Fig. 4, propeller 4 pushes away
Dynamic direction controllable adjustable;It is horizontal driver's cabin in cabin, and have and be supplied to human pilot and exist
All around sliding rail device in cabin, for adjusting dirigible mass centre changing dirigible navigation direction;Machine
It is to upwarp structure before and after the top of cabin 3, and is provided with steam vent, be used for preventing fuselage airbag gas from existing
Nacelle top is assembled;Fuselage air bag 1 abdominal part is provided with 4 fin air bags 5, such as Fig. 3 and Fig. 4
Shown, fin air bag 5 contacts to earth when can land as dirigible the strong point;Fin air bag 5 can set
Put the volume with increasing, and can be with analogy fuselage ridge wing air bag 2, now fin air bag 5
Connecting rope can be provided be connected with cabin 3, in cabin, human pilot can be adjusted by connecting rope
Fin air bag 5 shape, to control dirigible to navigate by water direction up and down with this.Fin noted herein
Air bag 5 can be replaced using the non-gasbag-type fin wing.The back of fuselage air bag 1 can be provided with dynamic
Power apparatus, by cabin skeleton, two upwarp skeleton in top closure, are formed ellipse around fuselage air bag
Circle skeleton, fuselage back power set are arranged on oval skeleton.Dirigible can be connected with weight and adjust
Pitch chain, is contacted to earth by adjustment of weight chain part and the length of connecting rope adjusts height and the water of dirigible
Flat navigation.Dirigible can be provided with balloonet in fuselage air bag bottom, balloonet can with inflation/deflation with
This adjusts the raising and lowering of dirigible.
The present invention is elaborated by examples detailed above, the present invention can also be realized using other examples simultaneously,
The present invention is not limited to above-mentioned instantiation, and the therefore present invention is limited by scope.
Claims (10)
1. a kind of dirigible it is characterised in that:Including:
Fuselage, is that one or more air bags are constituted, is made up of gas impermeable material, is filled with ratio in air bag
The light gas of atmospheric density;
One or more fuselage ridge wings, the fuselage ridge wing is made up of air bag, positioned at fuselage air bag back,
It is made up of gas impermeable material, in air bag, be filled with the gas lighter than atmospheric density;
Cabin, in belly inner bottom part, embedded fuselage and fuselage air bag, under cabin top comprises
Concave shape and cabin top edge has steam vent, prevents gas gas in fuselage air bag from gathering in nacelle top
Collection;
It is provided with suspender belt in fuselage air bag, connect cabin and fuselage ridge wing air bag.
2. device as claimed in claim 1 it is characterised in that:Described belly is provided with
Multiple fin air bags, fin air bag is connected with setting rope band between cabin, adjusts for operation rope band in cabin
Section fin bladder shape controls heading.
3. device as claimed in claim 2 it is characterised in that:The described fuselage ridge wing and machine
As demountable structure, the fuselage ridge wing MM loading capacity of different volumes can be chosen.
4. device as claimed in claim 1 it is characterised in that:Described fuselage both sides can set
It is equipped with inflatable wing, in wing, be provided with wing frame arm.
5. device as claimed in claim 1 it is characterised in that:Described dirigible setting is dynamic
Device, positioned at the back of fuselage air bag, avris, abdominal part or afterbody, power set are located at afterbody
When, afterbody is provided with auxiliary balloon and adjusts aft weight balance, fuselage air bag and the fuselage ridge wing
Balloon surface can be provided with solar attachment and storage device, is that power set are powered.
6. device as claimed in claim 1 it is characterised in that:Manned mode in described cabin
For horizontal, and the number that carries is single or double, and cabin is provided with skeleton for moulding, cabin bone
Frame can be connected with wing frame arm.
7. device as claimed in claim 1 it is characterised in that:Described dirigible is provided with secondary gas
Capsule, balloonet for isolating construction and can be connected with safety rope with dirigible, and balloonet lifting dirigible is high
Separate with dirigible after degree, balloonet may be located at nacelle top, nacelle top balloonet can be exitted, use
In regulation dirigible weight.
8. device as claimed in claim 1 it is characterised in that:Described dirigible can be connected with
Safety rope, dirigible safety rope can provide electric power for dirigible, and dirigible safety rope can be connected with weight and put down
Weighing apparatus chain, is contacted to earth by moiety by weight balancing chain and adjusts dirigible weight.
9. device as claimed in claim 1 it is characterised in that:Described fuselage is ellipse,
Length and width ratio are more than 1, and width is more than 1 with aspect ratio.
10. device as claimed in claim 1 it is characterised in that:Described dirigible afterbody can set
It is equipped with one or more empennages.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2015104517948 | 2015-07-28 | ||
CN201510451794 | 2015-07-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106394853A true CN106394853A (en) | 2017-02-15 |
Family
ID=58007853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510799977.9A Pending CN106394853A (en) | 2015-07-28 | 2015-11-19 | Airship |
Country Status (1)
Country | Link |
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CN (1) | CN106394853A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109250061A (en) * | 2018-11-14 | 2019-01-22 | 北京空天高科技有限公司 | Stratospheric airship device for adjusting posture |
CN110733669A (en) * | 2019-10-24 | 2020-01-31 | 北京空间技术研制试验中心 | Spacecraft re-entry capsule mass center dynamic adjusting device |
-
2015
- 2015-11-19 CN CN201510799977.9A patent/CN106394853A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109250061A (en) * | 2018-11-14 | 2019-01-22 | 北京空天高科技有限公司 | Stratospheric airship device for adjusting posture |
CN109250061B (en) * | 2018-11-14 | 2023-08-15 | 北京空天高技术中心(有限合伙) | Stratospheric airship attitude adjusting device |
CN110733669A (en) * | 2019-10-24 | 2020-01-31 | 北京空间技术研制试验中心 | Spacecraft re-entry capsule mass center dynamic adjusting device |
CN110733669B (en) * | 2019-10-24 | 2021-06-18 | 北京空间技术研制试验中心 | Spacecraft re-entry capsule mass center dynamic adjusting device |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170215 |