CN104627358A - Rotor wing and balloon composite aircraft and control method thereof - Google Patents
Rotor wing and balloon composite aircraft and control method thereof Download PDFInfo
- Publication number
- CN104627358A CN104627358A CN201510074917.0A CN201510074917A CN104627358A CN 104627358 A CN104627358 A CN 104627358A CN 201510074917 A CN201510074917 A CN 201510074917A CN 104627358 A CN104627358 A CN 104627358A
- Authority
- CN
- China
- Prior art keywords
- balloon
- aircraft
- rotor
- combined type
- control setup
- 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
Links
Landscapes
- Toys (AREA)
Abstract
The invention relates to a rotor wing and balloon composite aircraft and a control method thereof. The aircraft comprises a rotor wing aircraft assembly comprising an engine body, blades arranged on the engine body, a steering engine for controlling the blades, and a driving device, a balloon connected with the engine body, and a light gas generator or a high-pressure gas cylinder connected with the balloon, and a control device for controlling the flight of the aircraft and the light gas generator or high-pressure gas cylinder to fill the balloon with air or stop filling the balloon with air. Accordingly, the rotor wing and balloon composite aircraft provided by the invention can be used for overcoming the technical problems that the hover work time of a rotor wing aircraft is relatively short and the flight speed of a balloon aircraft is relatively slow in the prior art.
Description
Technical field
The present invention relates to vehicle technology field, particularly a kind of rotor and balloon combined type aircraft and control method thereof.
Background technology
By lift producing method, existing aircraft can be divided into Fixed Wing AirVehicle, rotor craft and balloon type aircraft etc. several.
Wherein, common Fixed Wing AirVehicle mainly produces lift by wing and carrys out balance airplane weight, power system is mainly used to overcome aircraft flight resistance, therefore the power much smaller than aircraft weight just can allow fixed wing aircraft lift off, so Fixed Wing AirVehicle has, speed is fast, load carrying ability is large, voyage and the cruise time long, but its manoevreability is relatively poor, and landing distance, and require special quality runway or special launching and recovering equipment, have a strong impact on and hinder fixed wing aircraft in the remote application without special machine Performance Area.
Rotor craft rotates generation lift by blade and carrys out the trimmed flight amount of thinking highly of, the component being produced horizontal direction by the inclination of tilting frame makes aircraft change course, the rotating speed of multi-rotor aerocraft then by changing each rotor makes many rotors change attitude, thus the component producing horizontal direction provides the power of its horizontal motion, so rotary aircraft to have manoevreability good, can vertical takeoff and landing and low feature is required to landing site, but the rotor efficiency be directly connected with power system can not show a candle to Fixed Wing AirVehicle, therefore power consumption is very large, and small-sized rotor craft adopts battery as power resources usually, limit by rotor efficiency and battery technology, cause the rotor craft hang time short, particularly many rotor wing unmanned aerial vehicles aircraft of present stage, about most of stagnant empty flight time only has half an hour.
Balloon type aircraft is by having hang time overlength and requiring low advantage to landing site, but its flying speed is comparatively slow, and manoevreability is also poor.
Summary of the invention
The object of this invention is to provide a kind of rotor and balloon combined type aircraft, it can overcome the technical matters that the stagnant empty work-hours of rotor craft in prior art is shorter and balloon flighter flying speed is slower.Present invention also offers the control method of a kind of above-mentioned rotor and balloon combined type aircraft.
A kind of rotor provided by the invention and balloon combined type aircraft, comprising:
Rotor craft assembly, comprises body, is arranged at the blade of described body, for controlling steering wheel and the actuating device of described blade;
Be connected to the balloon of described body and the light gas producer be connected with described balloon or high-pressure gas bottle;
Inflate in described balloon for controlling aircraft flight and the described light gas producer of control or high-pressure gas bottle or stop the control setup of inflation.
Preferably, also comprise balloon and shed release gear, described control setup controls described balloon and sheds release gear and discharge described balloon.
Preferably, described body is provided with balloon accommodation device, is accommodated in described balloon accommodation device before described balloon inflation, and during described balloon inflation, described balloon accommodation device is opened, and rises to make described balloon.
Preferably, the quantity of described balloon is one, and the center of gravity line of lift and described aircraft that described balloon puts on described aircraft coincides.
Preferably, the quantity of described balloon is multiple, and the lift that balloon described in each puts on described aircraft is uniformly distributed centered by the center of gravity line of described aircraft.
Preferably, release gear shed by described balloon is the cutting tool that can cut off balloon and described aircraft connecting rope, and described cutting tool comprises cutter body and for driving the cutting driving device of cutter body, described control setup controls described cutting driving device action; Or release gear shed by described balloon is the flexible linear shaped charge that connecting rope cuts off by the High Temperature High Pressure that explosive charge can be utilized to produce.
Preferably, the propulsion source of described actuating device is battery or driving engine.
Present invention also offers the control method of a kind of rotor and balloon combined type aircraft, comprise step:
S1, control setup receives instruction of taking off, and starts rotor craft assembly;
S2, aircraft flies to predeterminated position, and control setup sends balloon inflation instruction, and light gas producer or high-pressure gas bottle are inflated balloon, after balloon is charged to preset pressure, stops inflation;
S3, loading device carries out work operations;
S4, after loading device fulfils assignment, control setup controls aircraft and makes a return voyage.
Preferably, after described step S3, also step is comprised:
S31, described control setup controls described balloon and sheds release gear and discharge described balloon.
Rotor provided by the invention and balloon combined type aircraft, the blade of the described body that comprising: rotor craft assembly, comprise body, is arranged at, for controlling steering wheel and the actuating device of described blade; Release gear shed by the balloon and the balloon that are connected to described body; The control setup that release gear discharges described balloon is shed for controlling aircraft flight and controlling described balloon.Setting like this, rotor provided by the invention and balloon combined type aircraft, aircraft is in the process of cruising, and balloon can not be inflated, but provides power by the blade of rotor craft, ensures the flying speed of aircraft.Fly to destination, when carrying out stagnant idle job, control setup can control light gas producer or high-pressure gas bottle is inflated to balloon, and balloon can play and improve lift effect, and then aircraft can long stagnant idle job.Therefore, rotor provided by the invention and balloon combined type aircraft, it can overcome the technical matters that the rotor craft hang time is shorter and balloon flighter flying speed is slower.
Present invention also offers the control method of a kind of rotor and balloon combined type aircraft, comprise step:
S1, control setup receives instruction of taking off, and starts rotor craft assembly;
S2, aircraft flies to predeterminated position, and control setup sends balloon inflation instruction, and light gas producer or high-pressure gas bottle are inflated balloon, after balloon is charged to preset pressure, stops inflation;
S3, loading device carries out work operations;
S4, after loading device fulfils assignment, control setup controls aircraft and makes a return voyage.
Obviously, by control method provided by the invention, the technical matters that the rotor craft hang time is shorter and balloon flighter flying speed is slower can be overcome equally.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments of the invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to the accompanying drawing provided.
Fig. 1 is aerocraft system module diagram in the specific embodiment of the invention.
Detailed description of the invention
A kind of rotor that this detailed description of the invention provides and balloon combined type aircraft, it can overcome the technical matters that the stagnant empty work-hours of rotor craft in prior art is shorter and balloon flighter flying speed is slower.This detailed description of the invention additionally provides the control method of a kind of above-mentioned rotor and balloon combined type aircraft.
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
Please refer to Fig. 1, the rotor that this detailed description of the invention provides and balloon combined type aircraft, comprise rotor craft assembly, balloon, light gas producer or high-pressure gas bottle and control setup.
Wherein, rotor craft assembly comprises body, is arranged at the blade of body, for controlling steering wheel and the actuating device of blade, the propulsion source of this actuating device can also can be driving engine for battery; Balloon is connected to body, and light gas producer or high-pressure gas bottle are connected with balloon, for being filled with light gas in balloon.Control setup is inflated for controlling aircraft flight and control light gas producer or high-pressure gas bottle or stops inflation in balloon.
Setting like this, the rotor that this detailed description of the invention provides and balloon combined type aircraft, aircraft is in the process of cruising, and balloon can not be inflated, but provides power by the blade of rotor craft, ensures the flying speed of aircraft.Fly to destination when carrying out stagnant idle job, control setup can control light gas producer or high-pressure gas bottle is inflated to balloon, and balloon can play and improve lift effect, and then aircraft can long stagnant idle job.Therefore, the rotor that this detailed description of the invention provides and balloon combined type aircraft, it can overcome the technical matters that the rotor craft hang time is shorter and balloon flighter flying speed is slower.
In the preferred version of this detailed description of the invention, aircraft can also comprise balloon and shed release gear, and control setup controls balloon and sheds release gear release balloon.Setting like this, when aircraft needs to make a return voyage, can shed release gear discharged by balloon by balloon, in the process that aircraft makes a return voyage, balloon can not produce resistance, ensure that aircraft makes a return voyage speed.
In addition, can be provided with balloon accommodation device in the body of aircraft, be accommodated in balloon accommodation device before balloon inflation, during balloon inflation, balloon accommodation device is opened, and rises to make balloon.This balloon accommodation device can be the box body being provided with switch gate, and control setup can be opened by master cock door, after switch gate is opened, can rise during balloon inflation from switch gate.
It should be noted that, in this detailed description of the invention, the quantity of balloon can be one, also can be multiple.
When balloon quantity is one, the center of gravity line of lift and aircraft that balloon puts on aircraft coincides.When the quantity of balloon is multiple, the lift that each balloon puts on aircraft is uniformly distributed centered by the center of gravity line of aircraft.Setting like this, can ensure that aircraft has good stability when stagnant idle job.
Release gear shed by above-mentioned balloon can be the cutting tool that can cut off balloon and aircraft connecting rope, and cutting tool comprises cutter body and for driving the cutting driving device of cutter body, control setup controls cutting driving device action.Such as, cutting driving device can be cylinder or hydraulic actuating cylinder, by this body action of action carry its tools of cylinder or hydraulic actuating cylinder, to cut off rope.Or the flexible linear shaped charge that connecting rope can cut off for the High Temperature High Pressure that explosive charge can be utilized to produce by release gear shed by balloon.
This detailed description of the invention additionally provides the control method of a kind of rotor and balloon combined type aircraft, comprises step:
S1, control setup receives instruction of taking off, and starts rotor craft assembly;
S2, aircraft flies to predeterminated position, and control setup sends balloon inflation instruction, and light gas producer or high-pressure gas bottle are inflated balloon, after balloon is charged to preset pressure, stops inflation;
S3, loading device carries out work operations;
S4, after loading device fulfils assignment, control setup controls aircraft and makes a return voyage.
By control method provided by the invention, aircraft is in the process of cruising, and balloon is in the state of packing up, and ensure that the flying speed of aircraft.In time flying to destination and carry out stagnant idle job, control setup controls light gas producer or high-pressure gas bottle is inflated balloon, and balloon is risen, and then plays the effect promoting aircraft, ensures that aircraft can long-time stagnant idle job.
Further, after step s 3, also step is comprised:
S31, described control setup controls described balloon and sheds release gear and discharge described balloon.
Setting like this, when aircraft complete stagnant idle job need to make a return voyage time, balloon is shed release gear and is discharged by balloon, and aircraft can not be subject to the impact of balloon in the process of making a return voyage, and then ensure that the speed of making a return voyage.
To the above-mentioned explanation of the disclosed embodiments, professional and technical personnel in the field are realized or uses the present invention.To be apparent for those skilled in the art to the multiple amendment of these embodiments, General Principle as defined herein can without departing from the spirit or scope of the present invention, realize in other embodiments.Therefore, the present invention can not be restricted to these embodiments shown in this article, but will meet the widest scope consistent with principle disclosed herein and features of novelty.
Claims (9)
1. rotor and a balloon combined type aircraft, is characterized in that, comprising:
Rotor craft assembly, comprises body, is arranged at the blade of described body, for controlling steering wheel and the actuating device of described blade;
Be connected to the balloon of described body and the light gas producer be connected with described balloon or high-pressure gas bottle;
Inflate in described balloon for controlling aircraft flight and the described light gas producer of control or high-pressure gas bottle or stop the control setup of inflation.
2. rotor as claimed in claim 1 and balloon combined type aircraft, is characterized in that, also comprise balloon and shed release gear, and described control setup controls described balloon and sheds release gear and discharge described balloon.
3. rotor as claimed in claim 2 and balloon combined type aircraft, it is characterized in that, described body is provided with balloon accommodation device, be accommodated in described balloon accommodation device before described balloon inflation, during described balloon inflation, described balloon accommodation device is opened, and rises to make described balloon.
4. the rotor as described in any one of claim 1-3 and balloon combined type aircraft, is characterized in that, the quantity of described balloon is one, and the center of gravity line of lift and described aircraft that described balloon puts on described aircraft coincides.
5. the rotor as described in any one of claim 1-3 and balloon combined type aircraft, is characterized in that, the quantity of described balloon is multiple, and the lift that balloon described in each puts on described aircraft is uniformly distributed centered by the center of gravity line of described aircraft.
6. rotor as claimed in claim 2 and balloon combined type aircraft, it is characterized in that, release gear shed by described balloon is the cutting tool that can cut off balloon and described aircraft connecting rope, and described cutting tool comprises cutter body and for driving the cutting driving device of cutter body, described control setup controls described cutting driving device action; Or release gear shed by described balloon is the flexible linear shaped charge that connecting rope cuts off by the High Temperature High Pressure that explosive charge can be utilized to produce.
7. rotor as claimed in claim 1 and balloon combined type aircraft, it is characterized in that, the propulsion source of described actuating device is battery or driving engine.
8. a control method for rotor and balloon combined type aircraft, is characterized in that, comprise step:
S1, control setup receives instruction of taking off, and starts rotor craft assembly;
S2, aircraft flies to predeterminated position, and control setup sends balloon inflation instruction, and light gas producer or high-pressure gas bottle are inflated balloon, after balloon is charged to preset pressure, stops inflation;
S3, loading device carries out work operations;
S4, after loading device fulfils assignment, control setup controls aircraft and makes a return voyage.
9. the control method of rotor as claimed in claim 8 and balloon combined type aircraft, is characterized in that, after described step S3, also comprise step:
S31, described control setup controls described balloon and sheds release gear and discharge described balloon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510074917.0A CN104627358A (en) | 2015-02-12 | 2015-02-12 | Rotor wing and balloon composite aircraft and control method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510074917.0A CN104627358A (en) | 2015-02-12 | 2015-02-12 | Rotor wing and balloon composite aircraft and control method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104627358A true CN104627358A (en) | 2015-05-20 |
Family
ID=53206708
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510074917.0A Pending CN104627358A (en) | 2015-02-12 | 2015-02-12 | Rotor wing and balloon composite aircraft and control method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104627358A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105799908A (en) * | 2016-05-04 | 2016-07-27 | 北方民族大学 | Unmanned aerial vehicle device working on heavy load condition and control method |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3008665A (en) * | 1958-03-17 | 1961-11-14 | Frank N Piasecki | Helicopter and balloon aircraft unit |
| US4995572A (en) * | 1989-06-05 | 1991-02-26 | Piasecki Aircraft Corporation | High altitude multi-stage data acquisition system and method of launching stratospheric altitude air-buoyant vehicles |
| CN201161307Y (en) * | 2008-01-18 | 2008-12-10 | 南京理工大学 | Wire dragging type time-delay cutting apparatus |
| CN101327843A (en) * | 2007-08-15 | 2008-12-24 | 张首鸣 | Small-sized aerial craft anti-fall energy-saving auxiliary lifting system |
| CN201848899U (en) * | 2010-09-27 | 2011-06-01 | 北京送变电公司 | Rope cutting-off device |
| CN103112580A (en) * | 2012-12-12 | 2013-05-22 | 樊荣 | Balloon flying machine |
| CN203921198U (en) * | 2014-06-04 | 2014-11-05 | 黄河科技学院 | Distance type pesticide spraying device |
| WO2014207732A1 (en) * | 2013-06-28 | 2014-12-31 | Paolo Bellezza Quater | A multi-rotor aircraft |
| CN204507251U (en) * | 2015-02-12 | 2015-07-29 | 中电科（德阳广汉）特种飞机系统工程有限公司 | A kind of rotor and balloon combined type aircraft |
-
2015
- 2015-02-12 CN CN201510074917.0A patent/CN104627358A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3008665A (en) * | 1958-03-17 | 1961-11-14 | Frank N Piasecki | Helicopter and balloon aircraft unit |
| US4995572A (en) * | 1989-06-05 | 1991-02-26 | Piasecki Aircraft Corporation | High altitude multi-stage data acquisition system and method of launching stratospheric altitude air-buoyant vehicles |
| CN101327843A (en) * | 2007-08-15 | 2008-12-24 | 张首鸣 | Small-sized aerial craft anti-fall energy-saving auxiliary lifting system |
| CN201161307Y (en) * | 2008-01-18 | 2008-12-10 | 南京理工大学 | Wire dragging type time-delay cutting apparatus |
| CN201848899U (en) * | 2010-09-27 | 2011-06-01 | 北京送变电公司 | Rope cutting-off device |
| CN103112580A (en) * | 2012-12-12 | 2013-05-22 | 樊荣 | Balloon flying machine |
| WO2014207732A1 (en) * | 2013-06-28 | 2014-12-31 | Paolo Bellezza Quater | A multi-rotor aircraft |
| CN203921198U (en) * | 2014-06-04 | 2014-11-05 | 黄河科技学院 | Distance type pesticide spraying device |
| CN204507251U (en) * | 2015-02-12 | 2015-07-29 | 中电科（德阳广汉）特种飞机系统工程有限公司 | A kind of rotor and balloon combined type aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105799908A (en) * | 2016-05-04 | 2016-07-27 | 北方民族大学 | Unmanned aerial vehicle device working on heavy load condition and control method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11142309B2 (en) | Convertible airplane with exposable rotors | |
| CN204489181U (en) | Variable motor angle four axle vertical takeoff and landing fixed-wing compound unmanned plane | |
| EP3087003B1 (en) | An unmanned aerial vehicle | |
| CN105173073A (en) | Composite lift force type unmanned aerial vehicle realizing vertical take-off and landing | |
| CN106586001A (en) | Multimode and multi-based unmanned aerial vehicle with tailed flying wing configuration | |
| CN202728574U (en) | Composite aircraft with fixed wing and electric multiple propellers combined and with helicopter function | |
| CN103043212A (en) | Combined aircraft composed of fixed wing and electric multi-rotor wing | |
| RU2000114837A (en) | SYSTEM FOR TRANSFORMING A SELF-SUPPORTED HORIZONTAL FLIGHT PLANE AND A HORIZONTAL TAKE-OFF IN A HYBRID COMBINED SELF-SUPPORTED HORIZONTAL FLIGHT AROUND | |
| CN201419624Y (en) | Double-bypass propeller aerocar capable of vertical taking off and landing | |
| CN204507251U (en) | A kind of rotor and balloon combined type aircraft | |
| CN104260875B (en) | The resistance to crash feature of agricultural plant protection unmanned plane | |
| CN110683045A (en) | Aircraft with a flight control device | |
| CN105314110A (en) | Unmanned aerial vehicle with umbrella | |
| CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
| CN206218213U (en) | A kind of culvert type bionic Aircraft | |
| CN202728571U (en) | Private aircraft | |
| CN102849211A (en) | Variable power vertical short-distance takeoff landing aircraft with fixed wings | |
| CN204660024U (en) | A kind of dish-type rotor unmanned helicopter | |
| RU147731U1 (en) | AIRCRAFT | |
| CN104627358A (en) | Rotor wing and balloon composite aircraft and control method thereof | |
| CN206087302U (en) | All -wing aircraft formula ducted fan VTOL unmanned aerial vehicle | |
| CN113401350A (en) | Ducted aircraft | |
| CN105523182A (en) | Vertaplane with front tilting rotor wing and rear tilting rotor wing | |
| CN205034339U (en) | Bimodal air travel equipment | |
| CN209209026U (en) | A kind of combined type aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into 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: 20150520 |