CN108100208A - A kind of haze unmanned airship and haze system that manually disappears of manually disappearing - Google Patents

A kind of haze unmanned airship and haze system that manually disappears of manually disappearing Download PDF

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Publication number
CN108100208A
CN108100208A CN201711231127.4A CN201711231127A CN108100208A CN 108100208 A CN108100208 A CN 108100208A CN 201711231127 A CN201711231127 A CN 201711231127A CN 108100208 A CN108100208 A CN 108100208A
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CN
China
Prior art keywords
haze
dirigible
manually
refractive
unmanned airship
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
Application number
CN201711231127.4A
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Chinese (zh)
Inventor
李悦立
雷武涛
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN201711231127.4A priority Critical patent/CN108100208A/en
Publication of CN108100208A publication Critical patent/CN108100208A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D53/00Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/007Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by irradiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • B64B1/24Arrangement of propulsion plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • B64B1/24Arrangement of propulsion plant
    • B64B1/30Arrangement of propellers

Abstract

Invention is related to unmanned vehicle design, more particularly to a kind of haze unmanned airship and haze system that manually disappears of manually disappearing.The haze unmanned airship that manually disappears includes:Dirigible body;Flight control assemblies are arranged on dirigible body bottom portion, for controlling the heading of dirigible body;Two pieces of refractive bodies are symmetricly set on the both sides of dirigible body;Reflective regulation mechanism rotates for adjusting refractive body around refractive body.Manually disappear haze unmanned airship and the haze system that manually disappears of the present invention, unmanned airship can be tethered on high-altitude and haze layer, refractive body is unfolded on dirigible, sunlight reflection focuses on regional area, changes local atmospheric air temperature, strengthen atmosphere convection, and then global haze abatement is influenced, compared to current fog dispersal haze technology, without adding secondary energy sources, it consumes energy small, coverage is big.

Description

A kind of haze unmanned airship and haze system that manually disappears of manually disappearing
Technical field
The present invention relates to unmanned vehicle design, more particularly to a kind of haze unmanned airship and haze system that manually disappears of manually disappearing.
Background technology
One of haze accumulation causes atmosphere convection decrease, makes particle main reason is that subaerial temperature is too low Object can not dissipate;And the accumulation of haze hinders the irradiation of sunlight, reduces further Air Close To The Earth Surface temperature, further subtracts Weak convection current.
In the elimination haze technology currently existed, by the suction filtration of air, very power consumption, coverage is small; And to dispense the haze agent that disappears costly for unmanned plane, equally exists the problem of coverage is small.
The content of the invention
The object of the present invention is to provide a kind of manually disappear haze unmanned airship and the haze system that manually disappears, to solve existing elimination At least one problem existing for haze technology.
The technical scheme is that:
A kind of haze unmanned airship that manually disappears, including:
Dirigible body;
Flight control assemblies are arranged on the dirigible body bottom portion, for controllably controlling the flight of the dirigible body Direction;
Two pieces of refractive bodies are symmetricly set on the both sides of the dirigible body;
Reflective regulation mechanism for the refractive body to be fixed at the dirigible body, and controllably adjusts institute Refractive body is stated to rotate around the refractive body and the tie point of the reflective regulation mechanism.
Optionally, the flight control assemblies include:
Service module is fixed at the bottom of the dirigible body, and is filled by the service module for the dirigible body Gas;
Four the first motor are fixed by the bracket four be arranged in the same level of the service module and hang down respectively Nogata is upward;
Four propellers match respectively with first motor;
Flight controller is arranged in the service module, for controllably controlling first motor;
First information transceiver module, for receiving and transferring to control the control instruction of the flight controller;
Power-supply system is arranged in the service module, for providing power supply for the electrical appliance of the flight control assemblies.
Optionally, the reflective regulation mechanism includes:
Pedestal is fixed on the dirigible body;
First rotating shaft, both ends are arranged on by bearing hinge connection on the pedestal;
Second motor is arranged in the pedestal, for the first rotating shaft controllably to be driven to rotate;
Second shaft, one end are rotatably arranged on the middle part of the first rotating shaft, the rotation of second shaft by bearing Axis is vertical and passes through the pivot center of the first rotating shaft;
Three-motor is arranged in second shaft, for second shaft controllably to be driven to rotate;
Refractive body bearing, for the refractive body to be fixedly attached to the other end of second shaft;
Tilt controller, for controllably controlling second motor and the three-motor;
Second signal dispatcher module, for receiving and transferring to control the control instruction of the tilt controller.
Optionally, the refractive body is inflatable structure;
The reflective regulation mechanism further includes:
Venthole through being opened on the refractive body bearing, is connected with the air-filled pore of the refractive body;
Gas ducting, through the dirigible body interior is arranged on, one end is connected with the venthole, and the other end extends to The service module is inflated by the service module for the refractive body.
Optionally, the back side of the refractive body is provided with solar charging panel, for charging for the power-supply system.
The present invention also provides a kind of haze system that manually disappears, including it is at least one it is described in any one of the above embodiments manually disappear haze without People's dirigible, further includes:
Dirigible control system, for unmanned airship controllably to be controlled to fly to precalculated position, and described two pieces of control is reflective Body expansion is in predetermined angular.
Invention effect:
Manually disappearing for the present invention and manually disappears haze system at haze unmanned airship, and unmanned airship can be tethered in high-altitude and haze layer On, refractive body is unfolded on dirigible, sunlight reflection focuses on regional area, changes local atmospheric air temperature, strengthens air Convection current, and then global haze abatement is influenced, compared to current fog dispersal haze technology, without adding secondary energy sources, energy consumption is small, Coverage is big.
Description of the drawings
Fig. 1 is the structure diagram of the haze unmanned airship one of which state of the invention that manually disappears;
Fig. 2 is the structural representation at the one of visual angle of reflective regulation mechanism section in the haze unmanned airship of the invention that manually disappears Figure;
Fig. 3 is the structure diagram at another visual angle of reflective regulation mechanism section in the haze unmanned airship of the invention that manually disappears;
Fig. 4 is the structure diagram of the haze unmanned airship another kind state of the invention that manually disappears;
Fig. 5 is the haze system use principle figure of the invention that manually disappears.
Specific embodiment
To make the purpose, technical scheme and advantage that the present invention is implemented clearer, below in conjunction in the embodiment of the present invention Attached drawing, the technical solution in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class As label represent same or similar element or there is same or like element.Described embodiment is the present invention Part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiments of the present invention, ordinary skill people Member's all other embodiments obtained without creative efforts, belong to the scope of protection of the invention.Under Face is described in detail the embodiment of the present invention with reference to attached drawing.
In the description of the present invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear", The orientation or position relationship of the instructions such as "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " is based on attached drawing institutes The orientation or position relationship shown is for only for ease of the description present invention and simplifies description rather than instruction or imply signified dress It puts or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that the present invention is protected The limitation of scope.
In the elimination haze technology currently existed, by the suction filtration of air, very power consumption, coverage is small; And to dispense the haze agent that disappears costly for unmanned plane, equally exists the problem of coverage is small.Show only to change by atmospheric physics research Kind atmospheric circulation could more favorably eliminate haze, for this purpose, the present invention proposes a kind of haze unmanned airship and haze that manually disappears of manually disappearing System.
1 to Fig. 5 manually disappears haze unmanned airship and the haze system that manually disappears is done further in detail to of the invention below in conjunction with the accompanying drawings Explanation.
The present invention provides a kind of haze unmanned airship that manually disappears, dirigible body 1, flight control assemblies, reflective can be included Body 3 and reflective regulation mechanism 2.
Dirigible body 1 can select known a variety of suitable inflation airships as needed, and bottom is usually inflation/deflation Area.
Flight control assemblies are arranged on 1 bottom of dirigible body, for controllably controlling the heading of dirigible body 1, bag Include 1 up and down of control dirigible body, turn to etc..
Refractive body 3 is two pieces, is symmetricly set on the both sides of dirigible body 1;Refractive body 3 can select known a variety of suitable Reflective structure.
Reflective regulation mechanism 2 is used to refractive body 3 being fixed at dirigible body 1, and controllably adjust refractive body 3 around It refractive body 3 and the tie point of reflective regulation mechanism 2 rotates, so as to adjust the reflection angle of refractive body 3.
The present invention's manually disappears haze unmanned airship, and topology layout is reasonable, and control is simple, can controllably be tethered in high-altitude and On haze layer, refractive body is unfolded on dirigible, sunlight reflection focuses on regional area, changes local atmospheric air temperature, adds Strong atmosphere convection, and then influence global haze abatement, compared to current fog dispersal haze technology, without adding secondary energy sources, It consumes energy small, coverage is big.
In the haze unmanned airship that manually disappears of the present invention, flight control assemblies can be with a variety of suitable structures of selected as;This reality It applies in example, flight control assemblies preferably include service module 4, the first motor 5, propeller 6, flight controller, the first information and receive Send out module and power-supply system.
Service module 4 is fixed at the bottom of dirigible body 1, and can be inflated by service module 4 for dirigible body 1;Into One step, 4 installation position of service module can control dirigible center of gravity so that dirigible can be floated with perpendicular attitude in the air.
The quantity of first motor 5 is four, is fixed by the bracket is arranged in the same level of service module 4 respectively In four vertical direction, and each motor 5 has the propeller 6 to match, is changed by driving the rotation of propeller 6 Become the heading of dirigible body 1;First motor 5 is arranged on service module 4, and the position of service module 4 can control dirigible again Center of gravity, therefore, such structure cause flight more to stablize, and control simpler quick.
Flight controller can be known a variety of suitable controllers, such as microcontroller, microcomputer etc.;Flight Controller is arranged in service module 4, for controllably controlling the first motor 5;Also, flight controller is by being arranged on clothes The first information transceiver module being engaged in cabin 4, with the extraneous transmitting-receiving for carrying out control instruction.
Power-supply system is arranged in service module 4, can specifically include the components such as battery, cable;It is winged that power-supply system, which is used for, The electrical appliance of row control device and other electrical equipments provide power supply.
Further, in the haze unmanned airship that manually disappears of the invention, reflective regulation mechanism 2 can be a variety of suitable structures; In the present embodiment, preferably reflective regulation mechanism 2 include pedestal 21, first rotating shaft 22, the second shaft 23, refractive body bearing 24, partially Transcoder controller and the second signal dispatcher module.
Pedestal 21 is fixed at the left and right sides on dirigible body 1 by modes such as bolt or bondings;It is opened on pedestal 21 Equipped with groove, 22 inner hollow of first rotating shaft, both ends are arranged on by bearing hinge connection in the groove of pedestal 21;Second motor 221 are arranged in pedestal 21, power again by power-supply system, for controllably driving first by modes such as gear cooperations Shaft 22 rotates.
Second shaft, 23 one end is rotatably arranged on the middle part of first rotating shaft 22, the pivot center of the second shaft 23 by bearing Pivot center vertical and through first rotating shaft 22;Three-motor 231 is provided in the internal cavities of the second shaft 23, together Sample is powered by power-supply system, for the second shaft 23 controllably to be driven to rotate.
24 one side of refractive body bearing is fixedly connected with by refractive body 3, and opposite side is fixedly attached to the another of the second shaft 23 End.
Tilt controller is used to controllably control the rotation of the second motor 221 and three-motor 231, anti-so as to control 3 multi-angle rotation of body of light;Second signal dispatcher module, for receiving and transferring that the control of the tilt controller is controlled to refer to Order.Tilt controller is come the transmitting-receiving with extraneous progress control instruction by the second signal dispatcher module.
Further, in the haze unmanned airship that manually disappears of the invention, refractive body 3 is preferably inflatable structure;Wherein, reflective tune Section mechanism 2 further includes venthole 25, gas ducting.
Venthole 25 is connected through being opened on refractive body bearing 24 with the air-filled pore of refractive body 3;Gas ducting runs through It is arranged on inside dirigible body 1, one end is connected with venthole 25, and the other end extends to service module 4, can be by service module 4 Refractive body 3 is inflated.Further, the back side of preferably refractive body 3 is provided with solar charging panel or solar battery thin film, can be with More sufficient electric energy for service module is provided, is supplied to motor, the energy is provided for aspect adjusting, improves cruising ability.
Invention also improves a kind of haze system that manually disappears, including above-mentioned haze unmanned airship and the dirigible control system of manually disappearing System;Dirigible control system is flown for controllably control unmanned airship to precalculated position, and controls two pieces of expansion of refractive body 3 in pre- Determine angle.
The present invention is as follows in the haze system work process that manually disappears:
Under the unmanned airship state of ground, service module 4 accesses helium, and dirigible body 1 is made to inflate first and is finished;Then charge, After charging, you can release dirigible.Direction controlling is realized by propeller 6, into designated flying zone and height.Then, service Cabin 4 fills seven, being allowed to expansion becomes one with reflective effect via air-filled pore 25 by the pipeline in dirigible body 1 to inflatable body 3 The plane of fruit.According to the control instruction that ground dirigible control system is sent, adjusted instead via the reflective regulation structure 2 of the left and right sides Body of light 3 is realized the sunlight reflection to specific region and is focused on.
The above description is merely a specific embodiment, but protection scope of the present invention is not limited thereto, any Those familiar with the art in the technical scope disclosed by the present invention, all should by the change or replacement that can be readily occurred in It is included within the scope of the present invention.Therefore, protection scope of the present invention should using the scope of the claims as It is accurate.

Claims (6)

1. a kind of haze unmanned airship that manually disappears, which is characterized in that including:
Dirigible body (1);
Flight control assemblies are arranged on dirigible body (1) bottom, for controllably controlling flying for the dirigible body (1) Line direction;
Two pieces of refractive bodies (3) are symmetricly set on the both sides of the dirigible body (1);
Reflective regulation mechanism (2) for the refractive body (3) to be fixed at the dirigible body (1), and controllably adjusts The refractive body (3) is saved to rotate around the refractive body (3) and the tie point of the reflective regulation mechanism (2).
2. the haze unmanned airship according to claim 1 that manually disappears, which is characterized in that the flight control assemblies include:
Service module (4) is fixed at the bottom of the dirigible body (1), and is the dirigible sheet by the service module (4) Body (1) is inflated;
Four the first motor (5), are fixed by the bracket four be arranged in the same level of the service module (4) respectively In vertical direction;
Four propellers (6) match respectively with first motor (5);
Flight controller is arranged in the service module (4), for controllably controlling first motor (5);
First information transceiver module, for receiving and transferring to control the control instruction of the flight controller;
Power-supply system is arranged in the service module (4), for providing power supply for the electrical appliance of the flight control assemblies.
3. the haze unmanned airship according to claim 1 that manually disappears, which is characterized in that the reflective regulation mechanism (2) includes:
Pedestal (21) is fixed on the dirigible body (1);
First rotating shaft (22), both ends are arranged on by bearing hinge connection on the pedestal (21);
Second motor is arranged in the pedestal (21), for the first rotating shaft (22) controllably to be driven to rotate;
Second shaft (23), one end are rotatably arranged on the middle part of the first rotating shaft (22), second shaft by bearing (23) pivot center is vertical and passes through the pivot center of the first rotating shaft (22);
Three-motor is arranged in second shaft (23), for second shaft (23) controllably to be driven to rotate;
Refractive body bearing (24), for the refractive body (3) to be fixedly attached to the other end of second shaft (23);
Tilt controller, for controllably controlling second motor and the three-motor;
Second signal dispatcher module, for receiving and transferring to control the control instruction of the tilt controller.
4. the haze unmanned airship according to claim 2 that manually disappears, which is characterized in that the refractive body (3) is inflatable knot Structure;
The reflective regulation mechanism (2) further includes:
Venthole (25) through being opened on the refractive body bearing (24), is connected with the air-filled pore of the refractive body (3);
Gas ducting, internal through the dirigible body (1) is arranged on, one end is connected with the venthole (25), and the other end prolongs The service module (4) is extended, is inflated by the service module (4) for the refractive body (3).
5. manually disappeared haze unmanned airship according to claim 1-4 any one of them, which is characterized in that the refractive body (3) The back side is provided with solar charging panel, for charging for the power-supply system.
6. a kind of haze system that manually disappears, which is characterized in that including at least one as claim 1-5 any one of them manually disappears Haze unmanned airship, further includes:
Dirigible control system for unmanned airship controllably to be controlled to fly to precalculated position, and controls two pieces of refractive bodies (3) Expansion is in predetermined angular.
CN201711231127.4A 2017-11-29 2017-11-29 A kind of haze unmanned airship and haze system that manually disappears of manually disappearing Pending CN108100208A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711231127.4A CN108100208A (en) 2017-11-29 2017-11-29 A kind of haze unmanned airship and haze system that manually disappears of manually disappearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711231127.4A CN108100208A (en) 2017-11-29 2017-11-29 A kind of haze unmanned airship and haze system that manually disappears of manually disappearing

Publications (1)

Publication Number Publication Date
CN108100208A true CN108100208A (en) 2018-06-01

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090145999A1 (en) * 2004-09-09 2009-06-11 Porter David R Method and Apparatus for Stratospheric and Space Structures
CN201371937Y (en) * 2008-12-15 2009-12-30 曹斌 Non-maneuverable airship
CN202320770U (en) * 2011-11-02 2012-07-11 江慧卓玛 Floating airship for artificial precipitation
CN106659129A (en) * 2014-06-13 2017-05-10 Lta有限公司 Airships for weather manipulation
CN206187324U (en) * 2016-11-07 2017-05-24 深圳光启空间技术有限公司 Airship

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090145999A1 (en) * 2004-09-09 2009-06-11 Porter David R Method and Apparatus for Stratospheric and Space Structures
CN201371937Y (en) * 2008-12-15 2009-12-30 曹斌 Non-maneuverable airship
CN202320770U (en) * 2011-11-02 2012-07-11 江慧卓玛 Floating airship for artificial precipitation
CN106659129A (en) * 2014-06-13 2017-05-10 Lta有限公司 Airships for weather manipulation
CN206187324U (en) * 2016-11-07 2017-05-24 深圳光启空间技术有限公司 Airship

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Application publication date: 20180601

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