CN108860557A - The work system of more unmanned hot air dirigible airships of rotor - Google Patents

The work system of more unmanned hot air dirigible airships of rotor Download PDF

Info

Publication number
CN108860557A
CN108860557A CN201810590190.5A CN201810590190A CN108860557A CN 108860557 A CN108860557 A CN 108860557A CN 201810590190 A CN201810590190 A CN 201810590190A CN 108860557 A CN108860557 A CN 108860557A
Authority
CN
China
Prior art keywords
dirigible
hot air
rotor
unmanned
unmanned hot
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
CN201810590190.5A
Other languages
Chinese (zh)
Inventor
严伟民
王宏泽
严霁玥
马非
马一非
周桂源
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.)
Chongqing Vocational College of Transportation
Original Assignee
Chongqing Vocational College of Transportation
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 Chongqing Vocational College of Transportation filed Critical Chongqing Vocational College of Transportation
Priority to CN201810590190.5A priority Critical patent/CN108860557A/en
Publication of CN108860557A publication Critical patent/CN108860557A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/66Mooring attachments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/30Lighter-than-air aircraft, e.g. aerostatic aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

The invention discloses a kind of work systems of more unmanned hot air dirigible airships of rotor, including:It is tethered at anchoring mode and offline mode;Described to be tethered in anchoring mode, more unmanned hot air dirigible airships of rotor are connect with the motor-driven support control station of ground on-vehicle and ground on-vehicle power supply system respectively by being tethered at cable;In the offline mode, more unmanned hot air dirigible airships of rotor are operated by ground remote controller;In the hanging basket of the unmanned hot air dirigible airship of more rotors, worked by computer gas ignition and jet control system.The work system of the unmanned hot air dirigible airship of more rotors provided by the invention, easy to operate, using flexible, intelligent control is long-range to control, strong interference immunity, broad covered area;Software and hardware platform adapts to fixed station, movement station and can move the use environments such as station, and mobile loading platform adapts to vehicle-mounted, unmanned helicopter load and warship (ship) carries.Equipment requirement had not only been able to satisfy single station and has worked independently but also have multistation networking working method.

Description

The work system of more unmanned hot air dirigible airships of rotor
Technical field
The present invention relates to hot air dirigible airship fields, specifically, in particular to a kind of work of the unmanned hot air dirigible airship of more rotors System.
Background technique
There are 30,000 kilometers of land boundary lines, 1.8 ten thousand kilometers of coastline, surrounding geographical, topography, geology, environment, war in China The slightly information such as status, safety and stability, hot zones and regional location, topography and geomorphology, River Hydrology, weather vegetation, seasonal characteristic It obtains and normalization is managed and monitoring complex.
The different edge doors that relate to are different purposes, establish data detection, information Perception and the communication of each special task The information of net, acquisition is this department's use, provides the narrow range of shared information, uses the less of shared information.Regional platform sense Know that equipment type is more, personnel equipment's goods and materials type is also more, nets that discrete, agreement is nonstandard, Lu Tonglian is obstructed, information is not melted more The phenomenon that logical, perception information can not be shared.
Summary of the invention
In order to solve problems in the prior art, the embodiment of the invention provides a kind of work of more unmanned hot air dirigible airships of rotor System.The technical solution is as follows:
On the one hand, a kind of work system of unmanned hot air dirigible airship of more rotors is provided, including:It is tethered at anchoring mode and flight Mode;It is described to be tethered in anchoring mode, more unmanned hot air dirigible airships of rotor by be tethered at cable respectively with the motor-driven branch of ground on-vehicle Control station is helped to connect with ground on-vehicle power supply system;In the offline mode, more unmanned hot air dirigible airships of rotor pass through ground Remote control device operation;In the hanging basket of the unmanned hot air dirigible airship of more rotors, pass through computer gas ignition and jet control system Work.
Further, described be tethered in cable is provided with mooring guy, feed cable and data communication cable;
The mooring guy is used for the unmanned hot air dirigible airship of the more rotors of mooring;The feed cable is supplied for dirigible rotor motor Electricity;The data communication cable is used for transmission data information.
Further, in the offline mode, more unmanned hot air dirigible airships of rotor rely on fuel gas bottle entrained by hanging basket Gas ignition work, when measure working sensor value reach make dirigible be able to maintain rise air pressure when, start dirigible on be The work of cable electronics trip gear, is tethered at cable and loosens with dirigible, and dirigible is kept by hanging the work of the combustion gas in fuel gas bottle entrained by storehouse Rising lift of the dirigible in setting height.
Further, in the offline mode, more unmanned hot air dirigible airships of rotor are by hanging standby electricity entrained by storehouse Pond power supply takes equipment power supply by dirigible rotor motor and dirigible, and the instruction that dirigible receives ground remote controller is calculated according to winged control Machine, electricity adjust parameter value set by computer to make winged control and posture operation work;Wherein, described to hang the electricity of battery entrained by storehouse Support the work of dirigible equipment in source
It further, further include landing gear structure;The landing gear structure uses universal elastic the three of air spring assembly Corner bracket structure undercarriage.
Further, the unmanned hot air dirigible airship of more rotors is filled and is propped up by fuel gas bottle fuel gas injection utricule capsula interna hot gas Support dirigible shell;
Ship cabin, ship capsule structure material:Using the shell of streamlined carbon fiber light-high-strength material glass reinforced plastic, there is higher pressure-bearing Ability, heat-resistant fireproof, and the utricule of the double-layer air bag material with good air-tightness.
Technical solution bring beneficial effect provided in an embodiment of the present invention is:
The work system of the unmanned hot air dirigible airship of more rotors provided by the invention, easy to operate, using flexible, intelligent control, Long-range control, strong interference immunity, broad covered area;Software and hardware platform adapts to fixed station, movement station and can move station etc. using ring Border, and mobile loading platform adapts to vehicle-mounted, unmanned helicopter load and warship (ship) carries.Equipment requirement had both been able to satisfy single independent work of standing Make that there is multistation networking working method again.
Detailed description of the invention
To describe the technical solutions in the embodiments of the present invention more clearly, make required in being described below to embodiment Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings other Attached drawing.
Fig. 1 is a kind of module diagram of the work system of more unmanned hot air dirigible airships of rotor of the embodiment of the present invention.
Specific embodiment
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with attached drawing to embodiment party of the present invention Formula is described in further detail.
The present invention provides a kind of work system of unmanned hot air dirigible airship of more rotors is provided, referring to Fig. 1, more rotors nobody The work system 10 of hot air dirigible airship includes:It is tethered at anchoring mode 100 and offline mode 200;It is described to be tethered in anchoring mode 100, The unmanned hot air dirigible airship of more rotors by be tethered at cable respectively with the motor-driven support control station of ground on-vehicle and ground on-vehicle power supply be System connection;In the offline mode 200, more unmanned hot air dirigible airships of rotor are operated by ground remote controller;More rotations In the hanging basket of the unmanned hot air dirigible airship of the wing, worked by computer gas ignition and jet control system.
Further, described be tethered in cable is provided with mooring guy, feed cable and data communication cable;
The mooring guy is used for the unmanned hot air dirigible airship of the more rotors of mooring;The feed cable is supplied for dirigible rotor motor Electricity;The data communication cable is used for transmission data information.
Further, in the offline mode, more unmanned hot air dirigible airships of rotor rely on fuel gas bottle entrained by hanging basket Gas ignition work, when measure working sensor value reach make dirigible be able to maintain rise air pressure when, start dirigible on be The work of cable electronics trip gear, is tethered at cable and loosens with dirigible, and dirigible is kept by hanging the work of the combustion gas in fuel gas bottle entrained by storehouse Rising lift of the dirigible in setting height.
Further, in the offline mode, more unmanned hot air dirigible airships of rotor are by hanging standby electricity entrained by storehouse Pond power supply takes equipment power supply by dirigible rotor motor and dirigible, and the instruction that dirigible receives ground remote controller is calculated according to winged control Machine, electricity adjust parameter value set by computer to make winged control and posture operation work;Wherein, described to hang the electricity of battery entrained by storehouse Support the work of dirigible equipment in source.
It further, further include landing gear structure;The landing gear structure is using universal elastic tripod structure undercarriage.
Further, the unmanned hot air dirigible airship of more rotors is filled and is propped up by fuel gas bottle fuel gas injection utricule capsula interna hot gas Support dirigible shell;
Ship cabin, ship capsule structure material:Using the shell of streamlined carbon fiber light-high-strength material glass reinforced plastic, there is higher pressure-bearing Ability, heat-resistant fireproof, and the utricule of the double-layer air bag material with good air-tightness.
In the present embodiment, the unmanned hot air dirigible airship main working parameters of more rotors are additionally provided:
The unmanned hot air dirigible airship ship capsule volume of the more rotors of I type:120 cubic metres;Carry payload:28kg;Maximum wind resistance energy Power:4-6 grades of wind;
The unmanned hot air dirigible airship ship capsule volume of the more rotors of II type:220 cubic metres;Carry payload:76kg;Maximum wind resistance energy Power:4-6 grades of wind;
Landing gear structure:Universal elasticity tripod structure undercarriage;
It is tethered at cable:Dedicated low elastic force, (the band quick grafting of waterproof of high intensity 6mm polyethylene rope+1.5mm*2 feed cable Plug special)+data communication cable;
It is tethered at cable total length:250m is tethered at cable total weight:16.5kg;
Note:Once supporting system using aerial, ground support system will be disposably detached from.
Flight cruise speed:2~12,000 ms/h;
Max-endurance:The max-endurance 4.6 of unmanned hot air dirigible airship after remote control makes to be tethered at cable tripping Hour;
Ship cabin, ship capsule structure material:Using the shell of streamlined carbon fiber light-high-strength material glass reinforced plastic, there is higher pressure-bearing Ability, heat-resistant fireproof, and the utricule of the double-layer air bag material with good air-tightness;
Erection and time for lift off:≤30mins
Combustion gas form:High pressure gas cylinder, propane (liquefied petroleum gas, natural gas)
Specifically, in the present embodiment, the work system of more unmanned hot air dirigible airships of rotor is tracked flat using three axis autonomous stabilisations Platform, effective mission payload are 60kg;The autonomous height-lock control operation mode of remote control/Beidou/GPS;It is one-touch independently to take off, hang Stop, cruise, land, it is all executable round the clock scout, take photo by plane, aerial survey, pipeline inspection, deep woods fire prevention, rescue and relief work etc. it is various The task that misfortune nearly weighs;The task devices such as laser radar (LiDAR), thermal infrared imager, video camera, laser ranging can be carried.
Technical solution bring beneficial effect provided in an embodiment of the present invention is:
The work system of the unmanned hot air dirigible airship of more rotors provided by the invention, easy to operate, using flexible, intelligent control, Long-range control, strong interference immunity, broad covered area;Software and hardware platform adapts to fixed station, movement station and can move station etc. using ring Border, and mobile loading platform adapts to vehicle-mounted, unmanned helicopter load and warship (ship) carries.Equipment requirement had both been able to satisfy single independent work of standing Make that there is multistation networking working method again.
The foregoing is merely a prefered embodiment of the invention, is not intended to limit the invention, all in the spirit and principles in the present invention Within, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention.

Claims (6)

1. a kind of work system of the unmanned hot air dirigible airship of more rotors, which is characterized in that including:It is tethered at anchoring mode and flight mould Formula;It is described to be tethered in anchoring mode, more unmanned hot air dirigible airships of rotor by be tethered at cable respectively with the motor-driven support of ground on-vehicle Control station is connected with ground on-vehicle power supply system;In the offline mode, more unmanned hot air dirigible airships of rotor are distant by ground Control device operation;In the hanging basket of the unmanned hot air dirigible airship of more rotors, pass through computer gas ignition and jet control system work Make.
2. the work system of more unmanned hot air dirigible airships of rotor as described in claim 1, which is characterized in that described to be tethered at setting in cable There are mooring guy, feed cable and data communication cable;
The mooring guy is used for the unmanned hot air dirigible airship of the more rotors of mooring;The feed cable is powered for dirigible rotor motor;Institute It states data communication cable and is used for transmission data information.
3. the work system of more unmanned hot air dirigible airships of rotor as described in claim 1, which is characterized in that in the offline mode, The unmanned hot air dirigible airship of more rotors relies on the gas ignition work of fuel gas bottle entrained by hanging basket, when measuring working sensor value Reach make dirigible be able to maintain rise air pressure when, start dirigible on heaving pile electronics trip gear work, be tethered at cable and dirigible pine De-, dirigible keeps dirigible in the rising lift of setting height by hanging the work of the combustion gas in fuel gas bottle entrained by storehouse.
4. the work system of more unmanned hot air dirigible airships of rotor as claimed in claim 3, which is characterized in that in the offline mode In, more unmanned hot air dirigible airships of rotor are taken by hanging battery-backed power source entrained by storehouse by dirigible rotor motor and dirigible and are set Available electricity, dirigible receive the instruction of ground remote controller according to flight control computer, and it is winged that electricity adjusts parameter value set by computer to make Control and posture run work;Wherein, described to hang the support dirigible equipment work of battery power supply entrained by storehouse.
5. the work system of more unmanned hot air dirigible airships of rotor as described in claim 1, which is characterized in that further include undercarriage knot Structure;The landing gear structure uses the universal elastic tripod structure undercarriage of air spring assembly.
6. the work system of more unmanned hot air dirigible airships of rotor as described in claim 1, which is characterized in that the unmanned heat of more rotors Gas dirigible fills by fuel gas bottle fuel gas injection utricule capsula interna hot gas and supports dirigible shell;
Ship cabin, ship capsule structure material:Using the shell of streamlined carbon fiber light-high-strength material glass reinforced plastic, there is higher pressure-bearing energy Power, heat-resistant fireproof, and the utricule of the double-layer air bag material with good air-tightness.
CN201810590190.5A 2018-06-08 2018-06-08 The work system of more unmanned hot air dirigible airships of rotor Pending CN108860557A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810590190.5A CN108860557A (en) 2018-06-08 2018-06-08 The work system of more unmanned hot air dirigible airships of rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810590190.5A CN108860557A (en) 2018-06-08 2018-06-08 The work system of more unmanned hot air dirigible airships of rotor

Publications (1)

Publication Number Publication Date
CN108860557A true CN108860557A (en) 2018-11-23

Family

ID=64338544

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810590190.5A Pending CN108860557A (en) 2018-06-08 2018-06-08 The work system of more unmanned hot air dirigible airships of rotor

Country Status (1)

Country Link
CN (1) CN108860557A (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201941973U (en) * 2010-12-07 2011-08-24 襄樊宏伟航空器有限责任公司 Mooring hot air airship floating platform
CN202783764U (en) * 2012-09-11 2013-03-13 襄阳宏伟航空器有限责任公司 Hanging device for mooring hot-gas airship
CN204415705U (en) * 2015-02-02 2015-06-24 岳德强 Mooring type fire-fighting scounting aeroplane
CN105083521A (en) * 2015-09-18 2015-11-25 深圳市惠通环宇科技有限公司 Airship
US20150375842A1 (en) * 2011-03-01 2015-12-31 John Ciampa Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images
CN105947168A (en) * 2016-06-04 2016-09-21 郑州中德美游乐设备有限公司 Multi-rotor manned craft adopting helium balloon to overcome part of gravity
CN107054610A (en) * 2017-06-01 2017-08-18 北京天宇新超航空科技有限公司 The scheme of kite balloon airship in sky when a kind of long
CN107176283A (en) * 2017-06-30 2017-09-19 襄阳宏伟航空器有限责任公司 One kind automatically controls unmanned fire balloon

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201941973U (en) * 2010-12-07 2011-08-24 襄樊宏伟航空器有限责任公司 Mooring hot air airship floating platform
US20150375842A1 (en) * 2011-03-01 2015-12-31 John Ciampa Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images
CN202783764U (en) * 2012-09-11 2013-03-13 襄阳宏伟航空器有限责任公司 Hanging device for mooring hot-gas airship
CN204415705U (en) * 2015-02-02 2015-06-24 岳德强 Mooring type fire-fighting scounting aeroplane
CN105083521A (en) * 2015-09-18 2015-11-25 深圳市惠通环宇科技有限公司 Airship
CN105947168A (en) * 2016-06-04 2016-09-21 郑州中德美游乐设备有限公司 Multi-rotor manned craft adopting helium balloon to overcome part of gravity
CN107054610A (en) * 2017-06-01 2017-08-18 北京天宇新超航空科技有限公司 The scheme of kite balloon airship in sky when a kind of long
CN107176283A (en) * 2017-06-30 2017-09-19 襄阳宏伟航空器有限责任公司 One kind automatically controls unmanned fire balloon

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
谢辉: "《无人机应用基础》", 28 February 2018, 西北工业大学出版社 *
钱正在: "《军事航空航天技术概论》", 31 January 2014, 国防工业出版社 *

Similar Documents

Publication Publication Date Title
US10479503B2 (en) Suspended load stability systems and methods
US11359604B2 (en) Method for reducing oscillations in wind turbine blades
JP2019156397A (en) Flight unit and control method of flight unit
CN206777637U (en) Unmanned plane provided with ground fire plant
CN201362362Y (en) Composite power multipurpose unmanned aerial vehicle
CN102991671A (en) Compound coaxial contra-rotating helicopter
CN107416172A (en) A kind of full visual angle monitoring and method based on intelligent aerostatics platform
CN108860557A (en) The work system of more unmanned hot air dirigible airships of rotor
CN206039299U (en) Agricultural unmanned aerial vehicle , electronic governor and control system thereof
CN207809782U (en) A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device
KR20180024731A (en) The rotor blade Drone safety landing pack

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20181123