CN102730179A - Combined lifting force deformation airship - Google Patents
Combined lifting force deformation airship Download PDFInfo
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- CN102730179A CN102730179A CN2011100907462A CN201110090746A CN102730179A CN 102730179 A CN102730179 A CN 102730179A CN 2011100907462 A CN2011100907462 A CN 2011100907462A CN 201110090746 A CN201110090746 A CN 201110090746A CN 102730179 A CN102730179 A CN 102730179A
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Abstract
The invention provides an airship. The airship has the characteristics of low cost, high safety, feasible speed and environmental friendliness. The modern airship utilizes incombustible helium with the extremely high safety and the inert gas characteristic determines that the airship can safely descend even if the airship is seriously damaged in the air. The invention provides a novel airship design technical scheme which can change the size of an airship body, has a gesture control capability and has a faster flying speed compared with the existing airship; and a lifting force for ascending and descending is supplied for the novel airship by hot air which is cheap and easy to manufacture, and gas, such as the helium, which has low density and light weight. By releasing the hot air, the volume of the airship body is reduced, the flying resistance is reduced and the flying mode is changed into an airplane navigation flying mode; and in a navigation front flying phase, the lifting force is supplied by an aerodynamic lift airship body which is similar with a wing shape, and an airship wing.
Description
Technical field
The present invention relates to the dirigible field, relate to the dirigible technical field of high-speed flight that can the conversion offline mode by it.
Background technology
Dirigible has with low cost, and is safe, and speed is feasible, environmental characteristics, what modern dirigible used is the high non-flammable helium of safety, even if its inert gas characteristics determined its be badly damaged in the high-altitude also can safe falling; The dirigible load carrying ability is much larger than aircraft; Efficiency-cost ratio is also worthwhile compared to common vehicle; Someone did statistics, saw from speed, and the dirigible of existing exploitation has had the speed more than 150 kilometers; Be enough to part and replace our traditional passenger traffic mode of the crowded labor energy day by day, and greatly alleviate our energy and the nervous situation of traffic.From landform; China is the many countries in a mountain region; The whole nation mostly area is covered by the mountain region, if merely from the conventional floor traffic program, and traditional highway and railway surface construction; So a kind of lighter-than-air flight device of cheapness; Be the basic solution of everything problem, we also can spend huge fund again is that non-remunerative highway construction has been carried out in the remote corner of noon many traditional approachs ungetable with the cost of destroying environmental protection, and several flights that just have every day that we will do pass through.It is reported have a kind of novel aircrafts to be named as Dynalifter now, have dirigible, characters of aircraft concurrently, in light weight, the advantage that load is big of dirigible arranged, have the stable handling of aircraft again.Traditional dirigible can swim in the air always, and Dynalifter then quickens to obtain lift through helium and runway.Different according to circumstances, helium can provide 30% to 80% lift, and the driving engine propelling unit lift hull and the ship wing provide remaining lift through ground taxi, i.e. running take off vertical landing.
Summary of the invention
Cause greatly in view of the intrinsic build of dirigible; Wind resistance rain ability; The attitude control ability is poor; Defectives such as the huge building cost of boathouse height; The present invention provides a kind of hull size that can change to have the attitude control ability and the existing airship flight speed novel airship design technology project faster that compares, in this novel airship technical scheme is served as reasons the hull of dress lower density light weight gas with can charge into the hot air distortion and expand to become big or discharge and discharge the hot gas capsule that dwindles the hull volume in the hot air income ship and cooperate, lift is provided taking off to hover when landing; When converting cruising flight into, discharge gradually and discharge hot air distortion reducing volume reduction flight resistance, the lift when conversion cruising flight being provided by the ship wing.Cheap and the hot air that is easy to make can with the gas such as the helium of lower density light weight, and the lift that provides of propulsion system etc. provides the lift that takes off when hovering landing.Reduce volume and reduce flight resistance and convert aircraft cruising flight pattern into through discharge discharging hot air, the stage that flies before cruising provides lift by the aerodynamic lift hull and the ship wing of wing shapes.This dirigible is made up of the top hull that can upwards open and bottom hull two parts hull or a plurality of hull; Top and the bottom hull fore-end connects; Leading section through the top hull that can upwards open and bottom hull links to each other and controls the top and the bottom hull and upwards open and close up the drag rope system and device that resets to front opening from afterbody.Open to open or close up through the separation of hull up and down and reset, can discharge and open or reclaims the interior hot gas capsule cyst wall capsule skin that is used to load hot air of retraction hull.Hull up and down through being similar to the clam shell configuration opens under the help of drag rope device gradually, and the hull of the lift that the low density gas that is lighter than outside air weight that the high temperature that is charged into by injection in the high-temperature hot air manufacturing installation while thermotropism air bag expands produces and the hull of the constant lift of geostationary generation and wing shapes provides the lift needs when taking off landing.Whether the aerodynamic lift hull and the inner ship wing that charges into helium with similar wing shapes, the ship wing charge into the structure decision of helium by the ship wing.When taking off landing, the sub-fraction buoyancy lift is provided, mainly is provided at the lift that cruises when advancing.According to concrete design demand can be in the bottom gondola or the ship wing is installed with the hull both sides.The ship wing can adopt folding or flexible design.What be provided for controlling the hull attitude up and down in the both sides of hull has an adjustable valve design-calculated exhaust duct aperture, the hull attitude of the exhaust duct aperture control dirigible through the control correct position.
The propulsion system device adopted and to be similar to the AH-56 summer that the U.S. developed and to prolong the rotor of high-speed vertical-lifting machine and the propulsion system device of propelling screws switch operating when hull was suitable.Promptly have and be used to the major diameter rotor than lift is provided, when taking off and land, switch to the lifting airscrew lift mode and improve take-off weight and speed.In aircraft cruising flight pattern, then switch to screw propeller gradually and advance pattern, can adopt shrouded propeller with yaw rudder, better attitude control effort is provided, with dirigible take off weight and speed when cooperating that improving takes off hovers landing when hovering landing.Its major diameter rotor can adopt fixing fixed-wing or the cyclogyro pattern that lift is provided of not changeing to improve lift in the cruising flight pattern.
This novel airship take off reach a certain height after; The power that the propulsion system device flies before strengthening; Open the propelling exhaust duct aperture of hull tail end; Hot air in the rejected heat air bag gradually; Take in the ship automatically shrinking under the convergent force of the elastic rope on the capsule skin under the Pneumatic pressure that advancing by drag rope device and hull up and down to twine to shrink that closing up gradually synchronously resets and cooperate with top and the bottom hull bonded assembly hot gas capsule, under the forward thrust effect of the propelling exhaust duct aperture jet thrust of hull tail end and propulsion system device, convert the ship wing gradually by the come-up lift mode that is lighter than atmosphere into the aircraft cruising flight pattern that flies resistance before lift less is provided by Abseiling device.The landing pattern flies thrust before reducing gradually in contrast, opens gradually to open and sprays the low density gas that is lighter than outside air weight that the high temperature that charges into expands in the synchronous thermotropism air bag of hull up and down and produce the vertical or wide-angle low speed that facings the wind of buoyancy lift and do not have the landing of sliding.It will be safer that there is landing drag rope device in certain landing zone..The top hull can move up under the buoyancy lift effect, and the bottom hull moves down under the action of gravity of gondola and opens the hot gas capsule.
Description of drawings
Accompanying drawing 1 closes up the state of flight scheme drawing for hull about the present invention
Accompanying drawing 2 opens the side schematic view that launches the hot gas capsule for hull about the present invention
Accompanying drawing 3 is overlooked schematical top view for the present invention
Accompanying drawing 4 merges lift hull design-calculated schematical top view for the present invention adopts wing body
Accompanying drawing 5 merges the anterior front schematic view of aerodynamic lift body design-calculated for the present invention adopts wing body
Accompanying drawing 6 adopts the belly scheme drawing of lifting rotor and the combination of duct propelling unit for the present invention
The schematical top view of accompanying drawing 7 full wing shapes hull for the present invention adopts
The side schematic view of accompanying drawing 8 full wing shapes hull for the present invention adopts
Accompanying drawing 9 adopts high range hot gas balloonet hull schematic cross-section for the present invention
Because I graduate from primary school, the junior middle school does not run through the graphic capability extreme difference, and the vice proper of the software of computer and use causes the discontinuous sawtoothization of the pattern line of accompanying drawing, please be interpreted as normal pattern line.
Below in conjunction with accompanying drawing practical implementation method of the present invention is described
In concrete enforcement design, be not limited to the design of accompanying drawing, accompanying drawing only supplies to be used to understand the design-calculated implementation method.
In Fig. 1, be denoted as top hull 1, bottom hull 2, the ship wing 3, gondola 4..Adopt the indent design at concrete enforcement middle and lower part hull, the bottom nested of top hull is in the groove of bottom hull
In Fig. 2, be denoted as open top hull 5, bottom hull 6; The ship wing 7; Gondola 8 gondola rear portions are the shrouded propeller propelling unit, and traction control Abseiling device 9 charges into the hot gas capsule utricule 10 of hot air with top and the bottom hull expansion molding synchronously with the hull bonded assembly.The capsule skin of open top and the bottom hull and expansion forms the compound lift hull of semi-hard type.When specifically manufacturing and designing, be not limited to aspect ratio LD Ratio shown in the drawings, the upper and lower hull relative position population size area shape relative size ratio can adjust according to design demand.Can be in taking off of reality hovered landing control through the open ratio control buoyancy lift of hull in-to-in drag rope control hot gas capsule.
In Fig. 3, hull 11, the ship wing 12, the position of the ship wing can be adjusted and be installed in around the gondola of bottom, vertical fin and tail vane 13, horizontal tail and tail vane 14 are used for the exhaust duct aperture position 15 that attitude is controlled, and connect the zone 16 that is flexible coupling of hull up and down.The exhaust duct aperture that is used for attitude control is provided with the number of locations length scale according to design demand, carries out the control of hull attitude through discharging hot air.The aerodynamic force transfer device can be set in the tailpipe hole in concrete design plan to be provided a part or whole being used to shrink to reclaim the hot gas capsule and close up the power of the rope wind of hull up and down that resets; Design is laid complicated, adopts electrically operated rope wind more suitable.Manufacture and design concrete; The hatch door that can open and close that can be employed in release aperture or the certain-length width of hull upper design hot gas capsule is used to discharge and reclaim the hull design of hot gas capsule, through launching and reclaim the hot air that charges into or emit that the hot gas capsule cooperates and come the conversion offline mode with discharging gradually.At the conformal hull that the anterior design of hull can modify tone, hull also can be designed as oval ring, and the middle part is used in discharging and recovery hot gas capsule.At least the aerodynamic lift hull and the ship wing that have the similar wing shapes of a part or whole part; Be used to provide buoyancy lift can charge into hot air become big with emit the hot air income hull design-calculated hot gas capsule that diminishes; The hull optimum configuration is semihard or fully hard formula structure; Also can adopt the rigid ship wing of soft hull, influence flying speed.The hot gas capsule volume of dirigible needs very big, and the dirigible back can be designed as expansible covering, and this covering has good toughness and air-tightness, and the time spent is not folded in the ship body.Be not limited to above ship type design, also can adopt other hull shape structure according to actual needs.Ship alar part or all can adopt the design of wing.The pore that charges into hot air is unidirectional aperture, also can be designed as other the mode of closing, and after it is closed, is taken over job with the pressurized air of air compressor input by dirigible in-to-in hot air manufacturing installation.
Fig. 4 has adopted the wing body that is similar to all-wing aircraft to merge lift hull design schematical top view, has increased the capacity and the blade area of low density gas, can be with extremely low speed flight.Top is used for upwards opening the roudnel type hull 41 of hot gas capsule, can adjust shape and area and position that top is used to open the hull of hot gas capsule as required.Vertical tail tail vane 42, the aerodynamic lift hull 43 of wing shapes.
In Fig. 5, adopted the front elevation of blended wing-body design-calculated technical scheme of the present invention, top is used for upwards opening the roudnel type hull 51 of hot gas capsule, can adjust shape and area and position that top is used to open the hull of hot gas capsule as required.Vertical tail tail vane 52, the aerodynamic lift hull 53 of wing shapes.Vector propulsion device 54.
Fig. 6 is similar to the propulsion system device of rotor that AH-56 summer that the U.S. develop prolongs the high-speed vertical-lifting machine and propelling screws switch operating for the present invention uses in force, adopt the belly layout scheme drawing of the power system that can carry out the offline mode switching that lifting rotor and shrouded propeller propelling unit make up.Promptly have and be used to the major diameter rotor than lift is provided, when taking off and land, switch to the lifting airscrew lift mode and improve take-off weight and speed.In aircraft cruising flight pattern, then switch to screw propeller gradually and advance pattern, can adopt shrouded propeller with yaw rudder, better attitude control effort is provided, with dirigible take off weight and speed when cooperating that improving takes off hovers landing when hovering landing.Its major diameter rotor can adopt fixing fixed-wing or the cyclogyro pattern that lift is provided of not changeing to improve lift in the cruising flight pattern.Wing body merges hull 61, the position 62 of anterior gondola and alighting gear, duct propelling unit 63, rotor 64, engine mission 65.
Fig. 7 implements the design-calculated schematical top view for the present invention adopts wing shapes aerodynamic lift hull; Be used for upwards opening promptly open hot gas capsule cyst wall capsule skin be positioned at wing shapes lift hull top rectangular hull 71; Be positioned at the vertical tail tail vane 72 on the wing shapes lift hull; The lift hull 73 of wing shapes, duct formula vector propulsion device and control rudder 74.The horizontal tail wing and tail vane 75 connect the join domain 76 of openable top hull and wing shapes aerodynamic lift hull.
Under different enforcement design goals; According to different design implementation target needs, can adjust hull and the shape of the hull that is used for upwards opening hot gas capsule cyst wall capsule skin and the size of shared whole hull, ratio; Shape and area and position and quantity form different hull layout configurations.For example only design is positioned at a part of zone at hull top or the different design goal of realization that Zone Full is used for upwards opening hot gas capsule capsule skin.Also can be designed as a plurality of being used for upwards opens, and the enforcement design plan of varying number and layout is formed on the hull top of the hot gas capsule capsule skin that links to each other with the captain boat body.
Fig. 8 implements design-calculated lateral plan, the aerodynamic lift hull 81 of wing shapes, vertical tail tail vane 82, the duct formula vector propulsion device 83 that deflects down, horizontal tail wing tail vane 84 for adopt wing shapes aerodynamic lift hull for the present invention.
When different design objectives needs, can install the ship wing additional, use the tilting rotor design that is similar to the V22 osprey in the hull both sides.
Used 4% to 90% the balloonet design that when taking off, charges into hot air of dress low density gas air bag relative scale in accounting in the enforcement design diagram shown in Figure 9; Promptly can when taking off, charge into hot air and cold air discharged the lift coefficient that keeps enough; Along with the helium that descends gradually of the pressurized energy of climbing to cruising altitude expands gradually; Hot air cools off reduced volume is gradually discharged outside the ship by the valve pipe system, keeps ship shape, prevents the hull spalling.Be used to open the top hull 91 of hot gas capsule capsule skin, the bottom capsule skin 91A of top hull; Be used to support the skeleton 92 of hull, account for the hot gas balloonet 93 of the larger proportion of top bag volume, the hull 94 that wing body merges; The hot gas balloonet 95 of hull side, bottom; The rope wind 96 that is used for traction control hot gas capsule capsule skin is for balloonet charges into hot air or discharges the plumbing system 97 of hot air, in concrete design; Pipeline is connected with the balloonet of top hull through the hull front end; The gondola 98 at driving engine place, the folding hot gas capsule capsule skin 99 of the segmentation that can upwards open expansion with the top hull that is used to open the hot gas capsule links to each other with the bottom hull is used for the hot air filtration hybrid cooling with hot air manufacturing installation or driving engine discharge; Through the valve pipe system is the hot air control setup 90 of balloonet inflation exhaust, charges into the volume size and the lift coefficient of discharging hot air or cold air adjusting balloonet through valve pipe control.The relative size of control hot air hot gas balloonet and air bag in concrete design is determined by the maximum ceiling altitude of design-calculated.The big or small width decision of the size of balloonet and the concrete design-calculated hull of quantity basis.Be used to charge into the space 90A of hot air.
The gas of lower density light weight also can adopt hot air to substitute a part or whole in the dirigible hull in concrete enforcement and design; Reduce the manufacturing cost of dirigible; Air heating apparatus is set in the hull of top or provides by the hot air manufacturing installation of bottom; Be used for will be heavier air bag and the hull that cold air that the top hull is pressed onto the bottom by hot air is discharged to the bottom that be positioned at, accomplish same process by the bottom hull again.Discharge outside the hull by the exhaust duct aperture of tailpipe hole or other position, also can pass through internal insulation capsule skin cancellation top hull or bottom hull, or the isolation capsule skin cost-cutting and the weight of cancel all upper and lower hull.Through with portion less the hot air of part substitute invariable relatively gas such as helium and can save a part or whole adjusting balloonets in the air bag; The hot air of being discharged by the hot air manufacturing installation or the driving engine of bottom provides adjusting through the valve pipe system, when low-latitude flying needs, hot air is charged into the top air bag and keeps the ship type and improve lift coefficient.
Bottom capsule skin in the hull of top is provided with suitable quantity correct position such as forward position controlledly opens that close and uncontrollable unidirectional pore; Bottom hull covering also can be adjusted the ratio of two types of gases of top hull as required; Corresponding independently air bag is set; The hot gas capsule that is used to charge into the filling hot air can charge into invariable relatively lower density light weight gas for example helium and hydrogen when needed, the ratio that can such gas of air bag regulation and control independently be provided for such gas as required with avoid damage.Speed when influencing the aircraft cruise mode, the consumption of when landing fuel of hovering but reserve buoyance has reduced greatly to take off.
In-flight concrete, can according to circumstances select as aircraft running take off landing, also can the running take off vertical landing or process opposite.The wind speed in landing zone change during greater than the wind speed that can allow VTOL fall near the airport slide landing.Behind the vertical comparatively safe height that climbs down with the wind at a certain angle after liftoff; Open the tailpipe hole; The hull hot air of under the Pneumatic pressure that causes that advances, discharging in the hot gas capsule closes up locking gradually up and down; And the generation propulsive force, cooperate with propulsion system dirigible is accelerated to the speed that the ship wing produces enough aerodynamic lifts.The landing process is slowed down for the forward thrust that reduces propulsion system; The power conversion of propulsion system is arrived the lifting rotor system, and release is hull up and down, through the ballonet raising lift of control lift in the hull of top; Reduce the lift of bottom hull synchronously; Hull opens air bag about opening, and in air bag, charges into hot air generation buoyancy lift by the hot air manufacturing installation synchronously, realizes landing or hovering.Can be when the design of concrete ship type on top hull the flying tail wing is installed or is adopted the X-shaped empennage to realize opening of counter motion control upper and lower hull up and down and close up.Under taking off and landing regional different weather situation, the hot gas capsule provides 0% to 50 lift.
In concrete enforcement design, if be used to provide the structure of the ship wing of offline mode conversion to adopt structure such as semihard formula or the rigid design that is similar to hull, can charge into the low-density gas of light weight for example helium a fraction of lift is provided.
In concrete enforcement design; The unfolding mode of top hull and bottom can be employed in locking front portion when taking off; The design of opening by afterbody, the ship type design that the locking afterbody is opened by the front portion when fall-retarding, the problem of hot gas capsule is opened and launched to top and the bottom hull when reducing fall-retarding because pneumatic pressure resistance is difficult; This design is unsatisfactory, manufactures and designs complicated hot gas capsule and is difficult in the income ship.
In concrete enforcement design, be not limited to single hull design shown in the drawings; Can adopt horizontal up and down many hulls and top and the bottom many hulls combined design according to the design demand hull when too roomy, add the hull design of one or more hulls between top hull and the bottom hull.
In concrete design implementation according to the difference of selecting propulsion system; As required the waste gas after burning of the discharge of propulsion system or the high temperature gas flow of ejection are imported in the hot gas capsule through valve and pipeline, are used for providing part or all of buoyancy lift. when for example using fanjet through valve and pipeline with part high-temperature injection air-flow importing hot gas capsule.Taking off after the high-temp waste gas of when using turboshaft engine/piston engine and other driving engine, through valve pipe driving engine being discharged filters to charge into when hovering landing provides buoyancy lift to save part or all of hot air manufacturing installation in the hot gas capsule.
Claims (10)
1. a NEW TYPE OF COMPOSITE lift is out of shape dirigible; Its major technique is characterized as; By the hull of interior dress lower density light weight gas with can control charge into hot air open become big expand or discharge hot gas utricule that hot air dwindles hull be engaged in taking off lift be provided when hovering landing; When converting cruising flight into, discharge the distortion of discharge hot air gradually and reduce hull volume reduction flight resistance, the lift when cruising flight being provided by the aerodynamic lift hull and the ship wing.The major technique of the type dirigible hull is characterized as the hull design that main employing has hull fore-end bonded assembly openable top hull and bottom hull two parts or is divided into a plurality of parts; The hull of upper and lower can open to be opened or closes up the design that resets; Can discharge to open and shrink and reclaim hot gas capsule capsule skin, through open or close up that resetting matches and spray in the thermotropism air bag buoyancy lift that the high-temperature low-density hot air that charges into provides and the low-density light weight gas in the hull of the top and the bottom for example mode converting of the constant relatively buoyancy lift that provides of helium and propulsion system and the lift that power that the propulsive force vector produces is compound when providing taking off landing to hover with opening of hull upper and lower.Or discharge hot air gradually and convert aircraft cruising flight pattern into.Have all or part of the aerodynamic lift hull that is similar to wing shapes and the ship wing, the lift that cruises when advancing is provided.
2. the technical characterictic of NEW TYPE OF COMPOSITE lift distortion dirigible as claimed in claim 1 is for have the hull and the ship wing of the interior dress low density gas of a part or whole part wing shapes at least; The hull optimum configuration is semihard or fully hard formula structure, also can adopt the rigid ship wing of soft hull.
3. the major technique like the described NEW TYPE OF COMPOSITE lift distortion of claim one dirigible is characterized as the fore-end connection that hull adopts best shell clam shell configuration, can open hull bottom, the top hull that closes up by the rear portion afterbody.Be not limited to this hull configuration; Being used to open the open hull of hull instant heating air bag that promptly opens hot gas capsule capsule skin can be for occupying the design of hull part zone, top to Zone Full; Also can adopt other hull configurations as required; When the practical implementation design plan, be not limited to configuration shown in the accompanying drawing, can adjust area and shape and the position and the quantity of hull and the hull and the hot gas capsule that are used for upwards opening the hot gas capsule as required, form different layouts and hull shape configurations.
4. as claimed in claim 1 can release opened and reclaimed that the release that is useful on the control air bag on the hot gas capsule utricule cyst wall of retraction is opened and the elastic rope of the bonded assembly up and down device and the rope wind that is used for air bag is recovered into hull of the lateral arrangement that resets.
5. the both sides design distribution like the top and the bottom hull of the described dirigible of claim one has several can be used to control the discharging air pipe aperture apparatus of hull attitude.
6. its technical characterictic of the power system of compound lift dirigible as claimed in claim 1 is the propulsion system device with rotor and propelling screws switch operating.When taking off and land, switch to the rotor lift pattern and improve take-off weight and speed.
7. provide the gas of the lower density light weight of buoyancy lift also can adopt the alternative part of hot air or all buoyancy lift is provided in the dirigible hull by hot air; Air heating apparatus is set in the hull of top or provides by the hot air manufacturing installation of bottom; The bottom of top hull is provided with controlled and uncontrollable pore of suitable quantity correct position; Be used for will be heavier air bag and the hull that cold air that the top hull is pressed onto the bottom by hot air is discharged to the bottom that be positioned at; Accomplish same process by the bottom hull again, when design demand, can cancel the isolation capsule skin of top hull or bottom, or the capsule skin is all isolated in cancellation.
8. the hot gas capsule that charges into hot air as claimed in claim 1 can charge into invariable relatively lower density light weight gas for example helium and hydrogen when needed, the ratio that can such gas of the regulation and control of air bag independently be provided for such gas as required with avoid damage.
9. the difference of the driving engine of the propulsion system that compound lift distortion dirigible as claimed in claim 1 uses according to concrete design imports the hot gas capsule through pipeline and valve with a part of driving engine ejection or the high-temp waste gas hot air of discharging and is used to save part or all of hot air manufacturing process units.
10. compound lift distortion dirigible as claimed in claim 1 can design according to the different designs flying height and use and 4% to 90% the hot air balloonet that accounts for the air bag relative scale, improves the cruising flight height.
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|---|---|---|---|
| CN2011100907462A CN102730179A (en) | 2011-04-02 | 2011-04-02 | Combined lifting force deformation airship |
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| CN2011100907462A CN102730179A (en) | 2011-04-02 | 2011-04-02 | Combined lifting force deformation airship |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218853A (en) * | 2016-09-30 | 2016-12-14 | 德保县实验小学 | A kind of hot air balloon device |
| CN106394895A (en) * | 2016-09-23 | 2017-02-15 | 广东天米教育科技有限公司 | Multi-form unmanned aerial vehicle and flight control method thereof |
| CN106516074A (en) * | 2016-10-24 | 2017-03-22 | 北京航空航天大学 | Deformable lift and buoyancy integrated aircraft aerodynamic configuration |
| CN109050866A (en) * | 2018-06-29 | 2018-12-21 | 范超然 | A kind of dirigible |
| CN109436283A (en) * | 2018-09-30 | 2019-03-08 | 中国特种飞行器研究所 | A kind of flying wing type variant dirigible |
| CN109606605A (en) * | 2018-12-25 | 2019-04-12 | 北京航空航天大学 | An airship multi-rotor composite aircraft |
| CN113148139A (en) * | 2021-05-18 | 2021-07-23 | 西华大学 | Utilize engine waste gas to carry out unmanned aerial vehicle of VTOL |
-
2011
- 2011-04-02 CN CN2011100907462A patent/CN102730179A/en active Pending
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106394895A (en) * | 2016-09-23 | 2017-02-15 | 广东天米教育科技有限公司 | Multi-form unmanned aerial vehicle and flight control method thereof |
| CN106394895B (en) * | 2016-09-23 | 2019-05-03 | 广东天米教育科技有限公司 | A kind of polymorphic unmanned plane and its flight control method |
| CN106218853A (en) * | 2016-09-30 | 2016-12-14 | 德保县实验小学 | A kind of hot air balloon device |
| CN106516074A (en) * | 2016-10-24 | 2017-03-22 | 北京航空航天大学 | Deformable lift and buoyancy integrated aircraft aerodynamic configuration |
| CN106516074B (en) * | 2016-10-24 | 2019-01-22 | 北京航空航天大学 | Aerodynamic shape of a deformable lift-floating integrated aircraft |
| CN109050866A (en) * | 2018-06-29 | 2018-12-21 | 范超然 | A kind of dirigible |
| CN109050866B (en) * | 2018-06-29 | 2021-02-09 | 范超然 | Airship |
| CN109436283A (en) * | 2018-09-30 | 2019-03-08 | 中国特种飞行器研究所 | A kind of flying wing type variant dirigible |
| CN109606605A (en) * | 2018-12-25 | 2019-04-12 | 北京航空航天大学 | An airship multi-rotor composite aircraft |
| CN109606605B (en) * | 2018-12-25 | 2021-10-29 | 北京航空航天大学 | An airship multi-rotor composite aircraft |
| CN113148139A (en) * | 2021-05-18 | 2021-07-23 | 西华大学 | Utilize engine waste gas to carry out unmanned aerial vehicle of VTOL |
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Addressee: Fan Tianming Document name: Notification of Publication of the Application for Invention |
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Application publication date: 20121017 |