CN206615379U - A kind of airship type aircraft - Google Patents
A kind of airship type aircraft Download PDFInfo
- Publication number
- CN206615379U CN206615379U CN201720195968.3U CN201720195968U CN206615379U CN 206615379 U CN206615379 U CN 206615379U CN 201720195968 U CN201720195968 U CN 201720195968U CN 206615379 U CN206615379 U CN 206615379U
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- CN
- China
- Prior art keywords
- air bag
- screen
- type aircraft
- hull
- gas
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- 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.)
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Abstract
The utility model provides a kind of airship type aircraft, including hull (10), the buoyance lift air bag (12) being installed in the hull, some propellers (20) for promoting the hull to move, the programmable airspeedometer (40) and some functional units of control device (30) and the connection control device are provided with the hull (10)；Some functional units include air bag control unit (50), and the air bag control unit includes the micromotor (52) and mechanical arm (54) being connected；The buoyance lift air bag (12) is provided with the gas outlet for discharging intracapsular gas, and the gas outlet is provided with gas port lid (14), and the mechanical arm (54) connects the gas port lid (14).The utility model can adjust the height of flight by changing the gas capacity in buoyance lift air bag, can effectively strengthen the stability and security of dirigible according to practical flight wind speed.
Description
【Technical field】
The utility model is related to aircraft, more particularly to a kind of airship type aircraft.
【Background technology】
Dirigible is a kind of aviation aircraft gone up to the air so as to buoyancy.Typically in the internal or external setting buoyance lift gas of dirigible
Capsule, the buoyance lift air bag is used for the gas (being commonly used for helium and hydrogen) that storage density is less than air.It is former according to Archimedes buoyancy
Reason, when the buoyancy that dirigible is subject to is more than its gravity, dirigible is just begun to ramp up to sky.Although dirigible have the hang time long,
The characteristics of launch weight is big, cost of transportation is low, but dirigible for flight when required environmental condition it is extremely strict, especially
On wind speed.If the dirigible of high-altitude flight meets larger wind speed, not only the stability of dirigible can be affected, even more serious
, it is also possible to cause peril.
【The content of the invention】
The problem of in order to overcome above-mentioned, strengthen the safety and stability performance of dirigible, wind speed can be reduced to dirigible by needing one kind badly
Harmfulness dirigible.I.e. during airship flight, the wind speed of flight is monitored in real time, and according to wind speed size, adjusted
The skyborne height and position of dirigible is saved, or carries out forced landing hedging.
The utility model provide a kind of airship type aircraft, including hull, be installed in the hull buoyance lift air bag,
Promote some propellers of the hull movement, it is characterised in that：Provided with control device and the connection control in the hull
The programmable airspeedometer and some functional units of device processed；
Some functional units include air bag control unit, and the air bag control unit includes the micromotor being connected
And mechanical arm；
The buoyance lift air bag is provided with the gas outlet for discharging intracapsular gas, and the gas outlet is provided with gas port lid, the machinery
Arm connects the gas port lid.
As a kind of preferred scheme, the programmable airspeedometer includes the measuring wind speed portion being connected and digital display part.
As a kind of preferred scheme, some functional units also include air bag and reclaim functional unit, and the air bag is reclaimed
Functional unit is provided with the winch for being used for reclaiming the buoyance lift air bag.
As a kind of preferred scheme, the hull surface is equipped with screen；Some functional units are also fixed including screen
Functional unit, the screen fixed-function unit includes the positioning lock of the fixed screen.
As a kind of preferred scheme, the hull surface is described to store up in storehouse admittedly provided with the storehouse of storing up for storing the screen
Surely there is the suspended axle being connected with disc spring one end or one side；The screen top or bottom are connected to the disc spring, lead to
Cross the disc spring backrush and be received into the suspended axle.
As a kind of preferred scheme, the hull surface is provided with the storehouse of storing up for storing the screen, and described store up in storehouse is pacified
Equipped with suspended axle and the motor for driving the suspended axle to rotate；The screen top or bottom are fixed on the suspended axle,
Rotated with the suspended axle and carry out backrush storage.
As a kind of preferred scheme, the hull also installs some propellers for being used to promote, and the propeller is fixed on
Within rotating shaft cylinder；The rotating shaft cylinder is included outside the rotating shaft inner cylinder and rotating shaft outer barrel encapsulation together, the rotating shaft inner cylinder and rotating shaft
The blast tube of interlayer formation delivery of fuel gas between cylinder.
As a kind of preferred scheme, the neck circle distribution of the rotating shaft outer barrel has some ventholes.
As a kind of preferred scheme, the bottom of the rotating shaft outer barrel is connected with the container of storage combustion gas.
As a kind of preferred scheme, the rotating shaft cylinder is connected with the control device, and the rotating shaft cylinder is additionally provided with some micro-
Igniter, some microdot firearms are corresponded to by the aperture of some ventholes respectively.
The airship type aircraft that the utility model is provided can be according to practical flight wind speed, by changing in buoyance lift air bag
Gas capacity adjusts the height of flight, can effectively strengthen the stability and security of dirigible.The utility model is provided
Aircraft, simply come with dirigible for example, but actual product is such as the aircraft of dirigible class but to be definitely not limited to such.
【Brief description of the drawings】
The utility model is described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is a kind of structural representation of dirigible provided by the utility model；
The structural representation for the dirigible that Fig. 2 is provided by another embodiment of the utility model；
Fig. 3 is the screen suspended axle structural representation of dirigible provided by the utility model；
Fig. 4 is another screen suspended axle structural representation of dirigible provided by the utility model；
Fig. 5 is the structural representation of the propeller of dirigible provided by the utility model.
【Embodiment】
With reference to Fig. 1, Fig. 1 is airship type aircraft provided by the utility model.Wherein, include hull 10, be arranged on
Hull 10 is internal or external and for storing the buoyance lift air bag 12 of buoyance lift gas, promotes the flight of hull 10 to advance and adjustment orientation
Propeller 20, the control device 30 of operational control is carried out to dirigible, the programmable airspeedometer of wind speed index in-flight is collected
40, and air bag control unit 50.
Programmable airspeedometer 40 in the utility model is the fan type airspeedometer with preprogrammed functions.Ordinary circumstance
Under, programmable airspeedometer 40 is installed to outside the hull of dirigible, the hull bottom of such as dirigible, front end, main cabin, driving cabin, window
Deng position.Need first plus to put a short cross bar in a pre-installation, then programmable airspeedometer is installed to the end of cross bar, and will
Side of the covering of the fan adjustment of airspeedometer towards dirigible., can be in multiple measurements position of hull in order to improve the precision of measuring wind speed
Put and install programmable airspeedometer 40.
Programmable airspeedometer 40 includes the measuring wind speed portion 42 being connected and digital display part 44.Wherein, for testing the speed
Flabellum occupies the major part of the area of measuring wind speed portion 42, and numerical monitor portion 44 is then provided with display screen and function button.
User can input the criteria for classifying of wind speed scale, such as instruction of input following procedure to programmable airspeedometer 40 in advance：When wind speed reaches
It is strong wind rank by the wind speed judgement during to 100 kilometers/hour or more.User can learn air speed data by display screen, or
Change is configured to the criteria for classifying of wind speed scale by function button.Meanwhile, it may be programmed the measurement data meeting of airspeedometer 40
Synchronous driving to dirigible control device 30, to make suitable emergency measure according to real-time wind speed by control device 30.
Strong wind rank is reached when programmable airspeedometer 40 detects current flight wind speed, and by measurement data synchronous driving
To control device 30, now, the buoyance lift air bag 12 to dirigible is carried out processing of losing heart by control device 30, and the flight for reducing dirigible is high
Degree strengthens the stationarity and security of dirigible with this, or even manipulation dirigible carries out urgent drop and stopped.
The discouraged processing procedure of buoyance lift air bag 12 is realized by the air bag control unit 50 of dirigible.It is provided with buoyance lift air bag 12
There is the tightly capping of a gas port lid 14 gas outlet of one control inside air bag gas capacity, the gas outlet under general state.
Air bag control unit 50 includes the micromotor 52 and mechanical arm 54 being connected, and wherein mechanical arm 54 is connected peace with gas port lid 14
Dress, mechanical arm 54 can control the opening and closing situation of gas port lid 14 under the drive of micromotor 52.Air bag control unit 50 can basis
Control device 30 is specific to be indicated to require, the gas in part or comprehensively the discharge buoyance lift air bag 12 of opening gas port lid 14.
With reference to Fig. 2, the utility model reclaims functional unit 60 provided with air bag, and air bag reclaims functional unit 60 and is provided with hank
Car 62, after gas in buoyance lift air bag 12 complete emptying, buoyance lift air bag 12 can be recovered to the original of buoyance lift air bag 12 and deposited by winch 62
Put position.
The appearance of hull 10, which is hung with screen 74, to be used to carry out advertisement and publicity.In order to ensure screen can comprehensively, completely
Ground spreads over hull appearance, and the utility model is additionally provided with screen fixed-function unit 70, and screen fixed-function unit 70 includes
To the positioning lock 72 of screen 74.The distribution of positioning lock and quantity can be considered according to actual screen size.Control device 30
It is connected with screen fixed-function unit 70.Strong wind rank is reached when programmable airspeedometer 40 detects current flight wind speed, and
By measurement data synchronous driving to control device 30, now, the positioning lock 72 to screen is sent unlock instruction by control device 30.
The latching in receive of positioning lock 72 is unclamped automatically after unlock instruction, and screen is lost after the fixation of positioning lock 72, can backrush
It is received into and is opened in the storing up within storehouse 80 of hull 10.
With reference to the embodiment of suspended axle 82 that Fig. 3 is a kind of screen 74 of the present utility model.Suspended axle 82 is secured transverse to
Store up inside storehouse 80.In order to realize the automatic rewinding function of screen, a disc spring 84, disc type bullet have also been wrung on suspended axle
Spring 84 is reserved in outermost one end and the top or bottom of screen and is connected.In the present embodiment, disc spring 84 and silver
The top of curtain 74 is connected.When screen 74 receives the locking of positioning lock 72, disc spring 84 is drawn from the spiral status of disc type
It is stretched flat straight；After positioning lock 72 unlocks screen 74, disc spring 84 actively reverts to the spiral status of disc type, and drives screen 74
Top or bottom convolution store, final screen 74 volume completely is contained in suspended axle 82, and income is to storing up among storehouse.
With reference to the embodiment of suspended axle 82 that Fig. 4 is another screen 74 of the present utility model.Suspended axle 82 can laterally live
It is arranged on and is stored up inside storehouse 80 dynamicly, and motor 86 is installed in the side of suspended axle 82.Control of the suspended axle 82 in motor 86
Under, rotated centered on the axle center of oneself.The top or bottom of screen 74 are joined directly together with suspended axle 82.In the present embodiment
In, suspended axle 82 is connected with the top of screen 74.When suspended axle 82 rotates with motor 86, the scrolling screen of suspended axle 82
Top or bottom together coiling, final screen 74 are taken in storing up among storehouse 80 by complete winding to suspended axle 82.
Fig. 5 is the structural representation of the propeller 20 of the utility model dirigible.In order to ensure that dirigible has enough promotions
Power, it is preferable that this dirigible needs to install eight or more such propellers 20.
The encapsulation of propeller 20 in the inside of rotating shaft cylinder 22, wherein, rotating shaft cylinder 22 is by an inner cylinder 24 and an outer barrel 26
The integral structure of welded closed.The bottom of outer barrel (26) is fixed with a container 27 for being used to store combustion gas.Inner cylinder 24 with it is outer
A narrow space interlayer is also reserved between cylinder 26.Blast tube 25 of the interlayer formation available for delivery of fuel gas, is stored in
Combustion gas in container 27 can be introduced within the blast tube 25.Outer barrel 26 offers some outlets in neck location circumference
Hole 262, and venthole 262 turns on blast tube 25, combustion gas can spray from venthole 262 towards propeller 20.Venthole 262
Vicinity also correspond to microdot firearm is installed, when combustion gas is spouting from venthole 262, microdot firearm simultaneously pilot gas,
Moment forms flame and jumps on propeller, and the dust being covered on propeller or the dirt being wound around are burnt, cleaned.
All building blocks of propeller 20 in the utility model are made up of resistant to elevated temperatures fire prevention material.
Embodiment presented above is only described further explanation to the utility model as a kind of preferred version, not
Constitute the utility model in all senses on limitation.For the person of ordinary skill of the art, this practicality is not being departed from newly
On the premise of type is conceived, various modifications and improvements can be made, these belong to protection domain of the present utility model.Therefore,
The protection domain of the utility model patent should be determined by the appended claims.
Claims (10)
1. a kind of airship type aircraft, including hull (10), the buoyance lift air bag (12) being installed in the hull, the propulsion ship
Some propellers (20) of body movement, it is characterised in that：It is described provided with control device (30) and connection in the hull (10)
The programmable airspeedometer (40) of control device and some functional units；
Some functional units include air bag control unit (50), and the air bag control unit includes the micromotor being connected
And mechanical arm (54) (52)；
The buoyance lift air bag (12) is provided with the gas outlet for discharging intracapsular gas, and the gas outlet is provided with gas port lid (14), described
Mechanical arm (54) connects the gas port lid (14).
2. airship type aircraft according to claim 1, it is characterised in that the programmable airspeedometer (40) includes being connected
The measuring wind speed portion (42) connect and digital display part (44).
3. airship type aircraft according to claim 1, it is characterised in that some functional units are also returned including air bag
Functional unit (60) is received, the air bag reclaims functional unit (60) and is provided with the winch for being used for reclaiming the buoyance lift air bag (12)
(62)。
4. airship type aircraft according to claim 1, it is characterised in that the hull surface is equipped with screen (74)；Institute
Stating some functional units also includes screen fixed-function unit (70), and the screen fixed-function unit (70) includes fixed described
The positioning lock (72) of screen.
5. airship type aircraft according to claim 4, it is characterised in that the hull surface is provided with the storage screen
Store up storehouse (80), it is described to store up the suspended axle (82) for being fixed with and being connected with disc spring (84) one end in storehouse；The screen
(74) top or bottom are connected to the disc spring (84), and the suspended axle is received into by the disc spring backrush.
6. airship type aircraft according to claim 4, it is characterised in that the hull surface is provided with the storage screen
Store up storehouse (80), it is described to store up the motor (86) that suspended axle (82) is provided with storehouse and drives the suspended axle to rotate；Institute
State at the top of screen (74) or bottom is fixed on the suspended axle, rotated with the suspended axle and carry out backrush storage.
7. airship type aircraft according to claim 1, it is characterised in that the propeller (20) is fixed on rotating shaft cylinder
(22) within；The rotating shaft cylinder includes the inner cylinder (24) and outer barrel (26) encapsulation together, the interlayer between the inner cylinder and outer barrel
Form the blast tube (25) of delivery of fuel gas.
8. airship type aircraft according to claim 7, it is characterised in that the neck circle distribution of the outer barrel (26) has
Some ventholes (262).
9. airship type aircraft according to claim 7, it is characterised in that the bottom of the outer barrel (26) is connected with storage
The container (27) of combustion gas.
10. airship type aircraft according to claim 8, it is characterised in that the rotating shaft cylinder (22) fills with the control
(30) connection is put, the rotating shaft cylinder is additionally provided with some microdot firearms, if some microdot firearms are corresponded to respectively is arranged on described
By the aperture for doing stomata (262).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720195968.3U CN206615379U (en) | 2017-03-02 | 2017-03-02 | A kind of airship type aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720195968.3U CN206615379U (en) | 2017-03-02 | 2017-03-02 | A kind of airship type aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206615379U true CN206615379U (en) | 2017-11-07 |
Family
ID=60231636
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720195968.3U Expired - Fee Related CN206615379U (en) | 2017-03-02 | 2017-03-02 | A kind of airship type aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206615379U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018122830A1 (en) | 2016-12-31 | 2018-07-05 | Ratti Jayant | High endurance unmanned aerial vehicle |
| CN111745649A (en) * | 2020-06-12 | 2020-10-09 | 泰华智业(天津)科技有限责任公司 | Underwater robot leveling method and device |
-
2017
- 2017-03-02 CN CN201720195968.3U patent/CN206615379U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018122830A1 (en) | 2016-12-31 | 2018-07-05 | Ratti Jayant | High endurance unmanned aerial vehicle |
| CN111745649A (en) * | 2020-06-12 | 2020-10-09 | 泰华智业(天津)科技有限责任公司 | Underwater robot leveling method and device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171107 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |