CN105947169A - Solar saucer-shaped floating aircraft provided with shrinkable airbag - Google Patents
Solar saucer-shaped floating aircraft provided with shrinkable airbag Download PDFInfo
- Publication number
- CN105947169A CN105947169A CN201610396799.XA CN201610396799A CN105947169A CN 105947169 A CN105947169 A CN 105947169A CN 201610396799 A CN201610396799 A CN 201610396799A CN 105947169 A CN105947169 A CN 105947169A
- Authority
- CN
- China
- Prior art keywords
- air
- aircraft
- flight device
- lighter
- solar energy
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/30—Lighter-than-air aircraft, e.g. aerostatic aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Abstract
The invention discloses a solar saucer-shaped floating aircraft provided with a shrinkable airbag. The solar saucer-shaped floating aircraft provided with the shrinkable airbag comprises a saucer-shaped aircraft body which is transformed from a saucer-shaped motor, and a propeller is arranged in the middle of a rotor of the saucer-shaped aircraft body. The shrinkage airbag is installed on the edge of the saucer-shaped aircraft body, and a solar power generation device is installed on the skin of the upper portion of the airbag. The lifting force of the aircraft body can be provided by air in the airbag and the propeller in the middle of the aircraft body independently or jointly, and power, in the horizontal direction, of the aircraft body is provided by a steering engine. The shrinkage airbag is mainly composed of airbag skin, a pull pressing rod system in the airbag and a telescopic system supporting the skin. The solar power generation device is in a fan shape, is circularly distributed on the skin in an attached mode, and moves along with the stretching or retracting of the skin.
Description
Technical field
The invention belongs to flight equipment technical field, the solar energy dish floating relating to a kind of collapsible air bag flies
Row device, can rise to higher spatial, it is possible to remains unchanged in a certain fixed position for a long time, can resist stronger
Beam wind, during landing, occupied ground is less, can be widely applied to may be used for navigation, signal of communication, monitoring,
Each field such as transportation.
Background technology
Lighter-than-air flight device is in recent years by the biggest concern, the progress that industry acquirement is certain, but existing dirigible
Etc. yet suffering from that flight speed is low, flight stability is poor, climate impact is big and safety is the most high many asks
Topic.Needing more operator when taking off landing, airborne period is limited.Lighter-than-air flight device still can not at present
Enough large-scale application are in each field.
Summary of the invention
It is an object of the invention to the weakness overcoming lighter-than-air flight device presently, there are, a kind of simple in construction of design,
Good stability, occupied ground are few compared with little, airborne period length, operator, and intelligence degree is high, it is possible to wide
The lighter-than-air flight device of general application.
The solar energy dish lighter-than-air flight device of a kind of collapsible air bag, it is characterised in that lighter-than-air flight device is by dish
Shape aircraft and the air bag composition being looped around on disc-shaped flying craft；The main body of disc-shaped flying craft is for installing propeller additional
Rotor-support-foundation system, middle part have stator system and the central compartment of duct, disc type electric machine is for having brush or brushless disk-type
Motor.Contractile air bag is installed in the marginal portion of aircraft ring-shaped shell, air bag top eyelid covering is pacified
Equipped with device of solar generating, the lift of aircraft can be by the gas in air bag and the spiral in the middle part of aircraft
Oar separately or cooperatively provides, the servos control on aircraft water square power stator system upwards.Described
Contractile air bag mainly by air bag eyelid covering, the strut and tie system of inside air bag, supports the telescopic system of eyelid covering
Composition；Described device of solar generating is fan-shaped, is close to be distributed on eyelid covering, along with illiteracy in circular
The opening or shrink and move of skin.
The telescopic system of utricule inner support eyelid covering is to be hinged and connected between rod member, the skeletal support of similar umbrella
Structure, one end is fixed on disc-shaped flying craft, and the other end is fixed on strut and tie.Telescopic system is exactly one end
It is fixed on aircraft skin, the set of outwardly directed a series of radial type rod member.
The internal strut and tie system of utricule is exactly that one end is fixed on aircraft skin, and the other end is connected to telescoping rod
On end, the set of the outwardly directed rod member that can stretch.
Utricule is looped around outside aircraft, and utricule can be with aircraft profile in the profile of aircraft section
Good transition, utricule meets aerodynamic demands.
Device of solar generating outside utricule is close to airbag shape annular distribution, each annular distribution
All being made up of the generator unit of one piece of block independence on layer, annular distribution number of plies amount determines as required, along
Radius directional spreding from small to large, is layered on air bag jointly.
Two ring-type device of solar generating at least it are distributed between two pin joints that telescopic system top is nearest,
When, after air bag deflation, device of solar generating internally folds, as Folding umbrella, reduce its landing
Shi Tiji, is so easier to find the landing place of suitable size, also solves the landing that volume causes greatly
Cheng Zhongyi is by the problem of interference in air flow.
Liquified helium storage device and steam vent is had in utricule, can be according to the air bag automatic aerofluxus of internal gas pressure situation
Regulation system with inflation；In descent, if there is propeller fault, then can supplement rapidly helium
Gas, regulation gas flow ensures its safe falling.
Lighter-than-air flight device carries accumulator, backs up oil-fired power generating equipment；Air bag liter is relied primarily on during floating
Power remains floating, and the power supply that solar energy equipment provides is mainly used to promote aircraft to maintain position, fly and carry
For the electric power needed for charging appliance, excrescent electric power accumulator preserves in case night uses；When special circumstances occur
Time can enable oil-fired power generating equipment provide the energy.
What preferably airbag shape can be complete with aircraft combines, and the entirety of composition can accord with well
Close aerodynamic demands, reduce flight resistance.After utricule folds, the most firmly it is fitted in flight
On device, now aircraft profile remains to meet aerodynamic demands.
The available lift of propeller is greater than the weight without lighter-than-air flight device whole during air bag, in order at gas
In the case of time condition is very severe also can autonomous flight, safe falling.
Rotor-support-foundation system is outwards followed successively by central compartment, bearing, propeller, permanent magnet or coil windings by center.
The upper and lower part at rotor-support-foundation system propeller edge is the cylinder being arranged on stator, propeller and cylinder group
Become ducted fan system；In bottom, cylinder is provided with flow deflector, and its inclination angle can change, when fan rotates
Flow deflector produces counter-force and makes stationary part keep stable, does not rotates.
Stator system and central compartment all use intensity material high, lightweight such as carbon fiber etc., stator system
Rigidly connected with central compartment, stator system wraps in outside rotor-support-foundation system, installs at rotor-support-foundation system outer ledge
Resilient material (rubber and spring etc.), to reduce the collision impact of aircraft and other object.
The devices such as radar, supersonic sounding and video camera are installed, it is possible to detect or see on lighter-than-air flight device
Barrier, realizes intelligent barrier avoiding or the nearest early warning of obstacle distance under the effect of control system.
Lighter-than-air flight device is provided with intelligent identifying system, ability after needing fingerprint, iris or password authentification to pass through
Enter aircraft.
On lighter-than-air flight device, each parts are mounted on the sensor of monitoring component operating condition, and sensor information is real
Time transmission, for decision-making.
Be provided with on aircraft on lighter-than-air flight device during record-setting flight is installed each parts operation information and in
The black box of heart cabin details, the most all of flight information all can be uploaded by high in the clouds automatically, with
Exempt from information dropout when aircraft damages.
Lighter-than-air flight device is provided with automatic status monitoring system, it is possible to analyzes guilty culprit, and can assess
Whether fault affects flight；If aircraft fault, nearest repair location can be pointed out, and fault message
Being sent to maintenance department, maintenance department can prepare to keep in repair required parts in advance.
Regular maintenance aid system is installed on lighter-than-air flight device, it is possible in the operating of record-setting flight device, each parts are gone through
History status data, when exceeding the standard value that parts allow operation time or access component to need repairing or change
After, system gives early warning the most in advance, it is desirable to go before personnel to safeguard, if safeguarded the most on request, stops starting,
Until unlocking after maintainer maintenance.
On lighter-than-air flight device, automated driving system is installed, after setting terminal, aircraft takeoff, wait to fly to
Terminal near above time confirm level point whether meet drop conditions, then precision approach is in the position specified,
Intervene without personnel.
Sensor and monitoring arrangement can be installed, it is possible to monitoring plant gas discharge, danger on lighter-than-air flight device
The flowing of goods transportation vehicle, carry personnel's trend etc. of dangerous goods.
Can install active or passive type air cleaner on lighter-than-air flight device, it is tighter in air pollution
The region of weight, height at pollutant place carry out operation, it is achieved the pollutant in air are adsorbed or
Sedimentation, alleviates air pollution.
Lighter-than-air flight device control system internal memory be placed with do not allow flight spatial domain coordinate, either manual operation,
Automatic Pilot or remote control all can not make aircraft pass through this no-fly region.
Propeller in lighter-than-air flight device duct both can be one group, it is also possible to is several groups；Rotor and stator system
System both can be one group, it is possibility to have several groups, bearing can undertake xial feed.
I.e. can there is one group of bearing can also nested several groups of bearings on lighter-than-air flight device between propeller and cabin.
On lighter-than-air flight device, the permanent magnet on stator or rotor can replace with coil, permanent magnet or coil
The satisfactory shape such as generally circular in shape, trapezoidal and fan-shaped.
Lighter-than-air flight device cabin interior can install aircraft, guided missile, rocket, space shuttle and spacecraft etc.
Aerial vehicle launcher, by buoyancy and the Stabilization of lighter-than-air flight device self of dirigible, brings it to sky
In, reduce its launch cost.
Lighter-than-air flight device cabin interior can be the place that hotel, hotel and dining room etc. are used for going sightseeing to board and lodge.
Accompanying drawing explanation
Fig. 1 is the solar energy dish lighter-than-air flight device structural representation of the collapsible air bag shown in the present invention；
Fig. 2 is dish lighter-than-air flight device top view；
Fig. 3 is dish lighter-than-air flight device brace rod detail drawing；
Fig. 4 is schematic diagram before and after dish lighter-than-air flight device utricule shrinks；
In accompanying drawing, the labelling of each parts is as follows: 1, device of solar generating；2, stator system；3, bearing system
System；4, expansion link system；5, strut and tie system；6, steering wheel；7, propeller system；8, rotor system
Permanent magnet on system or coil；9, corresponding on stator system coil or permanent magnet；10, brace rod system；
11, central compartment；12, flow deflector.
Detailed description of the invention
In order to make problem to be solved by this invention, technical scheme and beneficial effect clearer, below
By example with reference, the invention will be further described.Should be appreciated that concrete reality described herein
Executing example is only with explaining the present invention, being not intended to limit the present invention.
When lighter-than-air flight device on the ground time, air bag is to fold and be firmly fitted in the shell of ring-type aircraft
Around.After aircraft starts, under the effect of propeller 7, aircraft goes up to the air, required when rising to
Time highly, airbag deployment is also inflated to suitable volumes, and now the buoyancy of lighter-than-air flight device will hold up whole flight
The amount of thinking highly of, the power that the propeller of aircraft produces is mainly used in horizontal flight and the position of stabilized flight device；With
This simultaneously, the device of solar generating 1 on air bag is started working, it is provided that an electric power part for aircraft
Propeller rotary power, a part is stored in energy storage device, in case using during night flying.
When lighter-than-air flight device is when the air-flow that flight runs into is excessive, can first the steam vent in air bag be opened,
Gas is discharged, then by pinch system, air bag is packed up folding, and the power using aircraft propeller to produce comes
Flight.
When lighter-than-air flight device is to be landed, first being opened by the steam vent in air bag, gas is discharged, then by receiving
Air bag is packed up folding by compression system, and under the effect of aircraft propeller, floating aircraft drop to place size
Suitably region.
These are only the embodiment of patent of the present invention, not thereby limit the scope of the claims of the present invention, every profit
The equivalent structure made with description of the invention and diagramatic content or equivalence flow process conversion, or directly or indirectly
It is used in other relevant technical fields, is the most in like manner included in the scope of patent protection of the present invention.
Claims (26)
1. the solar energy dish lighter-than-air flight device of a collapsible air bag, it is characterised in that lighter-than-air flight device by
Disc-shaped flying craft (being formed by 2,3,6,7,8,9,11 and 12) and being looped around on disc-shaped flying craft
Gas-bag system (being formed by 1,4,5 and 10) forms；The main body of disc-shaped flying craft is to install turning of propeller additional
Subsystem 8, middle part have stator system 2 and the central compartment 11 of duct, and disc type electric machine is for having brush or without brush
Formula motor.Contractile air bag is installed, on the eyelid covering of air bag top in the marginal portion of aircraft ring-shaped shell
Being provided with device of solar generating 1, the lift of aircraft can be by the gas in air bag and the spiral shell in the middle part of aircraft
Rotation oar 7 separately or cooperatively provides, and the steering wheel 6 on aircraft water square power stator system upwards controls.
Described contractile air bag mainly by air bag eyelid covering, the strut and tie system 4 of inside air bag, supports stretching of eyelid covering
Compression system composition 5；Described device of solar generating 1 is fan-shaped, is close to be distributed on eyelid covering in circular,
Move along with opening or shrinking of eyelid covering.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
Telescopic system 4 in support eyelid covering is can be to be hinged and connected between rod member, the skeletal support knot of similar umbrella
Structure, one end is fixed on disc-shaped flying craft, and the other end is fixed on strut and tie, and exists by aircraft skin
Supporting to the longitudinal rib 10 of utricule edge direction, longitudinal rib is distributed in the top and the bottom of utricule, is looped around flight
On device, when it shrinks, longitudinal rib Shang You mechanism can ensure that it is collapsible.Telescopic system 4 is exactly that one end is solid
It is scheduled on aircraft skin, the set of outwardly directed a series of radial type rod member.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
Being exactly that one end is fixed on aircraft skin in strut and tie system 5, the other end is connected on telescoping rod end,
The set of the outwardly directed rod member that can stretch.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
In, the propeller in duct both can be one group, it is also possible to is several groups；Rotor and stator system both can be
One group, it is possibility to have several groups.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
Be close to airbag shape annular distribution in device of solar generating 1, each annular distribution layer is by
One piece of block independence generator unit composition, annular distribution number of plies amount determines as required, along radius from little to
Big directional spreding, is layered on air bag jointly.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
In, i.e. can have between propeller and cabin one group of bearing can also nested several groups of bearings, bearing can undertake
Xial feed.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
In, the permanent magnet on stator or rotor can replace with coil, permanent magnet or coil generally circular in shape,
The satisfactory shape such as trapezoidal and fan-shaped.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
In, between two pin joints that telescopic system 4 top is nearest, at least it is distributed two ring-type solar electrical energy generation dresses
Put, when, after air bag deflation, device of solar generating internally folds, as Folding umbrella, reduce it
Volume during landing, is so easier to find the landing place of suitable size, also solves the fall that volume causes greatly
Easily by the problem of interference in air flow during falling.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature exists
In, there are liquified helium storage device and steam vent in air bag, can be according to the air bag automatic aerofluxus of internal gas pressure situation
Regulation system with inflation；In descent, if there is propeller fault, then can supplement rapidly helium
Gas, regulation gas flow ensures its safe falling.
The solar energy dish lighter-than-air flight device of collapsible air bag the most according to claim 1, its feature
Being, lighter-than-air flight device carries accumulator, and accumulator can aloft be replaced, and backs up oil-fired power generating equipment；
Relying primarily on air bag lift during floating and remain floating, the power supply that solar energy equipment provides is mainly used to promote
Aircraft maintains position, flies and provide the electric power needed for charging appliance, excrescent electric power accumulator preserve in case
Night uses；Oil-fired power generating equipment can be enabled when there are special circumstances the energy is provided.
The solar energy dish lighter-than-air flight device of 11. collapsible air bags according to claim 1, its feature
Being, utricule is looped around outside aircraft, and what utricule profile can be complete with aircraft combines,
The entirety of composition can meet aerodynamic demands well, reduces flight resistance.After utricule folds,
On board the aircraft, now aircraft profile remains to meet aerodynamic demands in the most firm laminating.
The solar energy dish lighter-than-air flight device of 12. collapsible air bags according to claim 1, its feature
Being, the available lift of propeller system is greater than the weight without lighter-than-air flight device whole during air bag, with
Just in the case of weather conditions are very severe also can autonomous flight, safe falling.
The solar energy dish lighter-than-air flight device of 13. collapsible air bags according to claim 1, its feature
Be, rotor-support-foundation system be outwards followed successively by by center central compartment, bearing, propeller, permanent magnet or coil around
Group.
The solar energy dish lighter-than-air flight device of 14. collapsible air bags according to claim 1, its feature
Being, the upper and lower part at rotor-support-foundation system propeller edge is the cylinder being arranged on stator, propeller and cylinder
Composition ducted fan system；In bottom, cylinder is provided with flow deflector, and its inclination angle can change, when fan rotates
Time flow deflector produce counter-force and make stationary part keep stable, do not rotate.
The solar energy dish lighter-than-air flight device of 15. collapsible air bags according to claim 1, its feature
Being, stator system and central compartment all use intensity material high, lightweight such as carbon fiber etc., stator system
System and central compartment are rigidly connected, and stator system wraps in outside rotor-support-foundation system, pacify at rotor-support-foundation system outer ledge
Equipped with elastomeric material (rubber and spring etc.), to reduce the collision impact of aircraft and other object.
The solar energy dish lighter-than-air flight device of 16. collapsible air bags according to claim 1, its feature
It is, aircraft is provided with the devices such as radar, supersonic sounding and video camera, it is possible to detect or see barrier
Hinder thing, under the effect of control system, realize intelligent barrier avoiding or the nearest early warning of obstacle distance.
The solar energy dish lighter-than-air flight device of 17. collapsible air bags according to claim 1, its feature
It is, aircraft is provided with intelligent identifying system, ability after needing fingerprint, iris or password authentification to pass through
Enter aircraft.
The solar energy dish lighter-than-air flight device of 18. collapsible air bags according to claim 1, its feature
It is, aircraft is provided with on aircraft each parts operation information and center during record-setting flight is installed
The black box of cabin details, the most all of flight information all can be uploaded by high in the clouds automatically, in order to avoid
Information dropout when aircraft damages.
The solar energy dish lighter-than-air flight device of 19. collapsible air bags according to claim 1, its feature
Being, aircraft is provided with automatic trouble diagnosis system, it is possible to analyzes guilty culprit, and can assess event
Whether barrier affects flight；If aircraft fault, nearest repair location can be pointed out, and fault message is sent out
Giving maintenance department, maintenance department can prepare to keep in repair required parts in advance.
The solar energy dish lighter-than-air flight device of 20. collapsible air bags according to claim 1, its feature
It is, aircraft is provided with regular maintenance aid system, it is possible to each part history in the operating of record-setting flight device
Status data, allows operation time or access component to need repairing or after the standard value changed when exceeding parts,
System gives early warning the most in advance, it is desirable to go before personnel to safeguard, if safeguarded the most on request, stops starting, directly
Unlock after keeping in repair to maintainer.
The solar energy dish lighter-than-air flight device of 21. collapsible air bags according to claim 1, its feature
It is, aircraft is provided with automated driving system, after setting terminal, aircraft takeoff, wait to fly to end
Confirm when putting near above whether level point meets drop conditions, and then precision approach is in the position specified, nothing
Personnel are needed to intervene.
The solar energy dish lighter-than-air flight device of 22. collapsible air bags according to claim 1, its feature
It is, aircraft can be installed sensor and monitoring arrangement, it is possible to monitoring plant gas discharge, danger
The flowing of product haulage vehicle, carry personnel's trend etc. of dangerous goods.
The solar energy dish lighter-than-air flight device of 23. collapsible air bags according to claim 1, its feature
Being, aircraft can be installed active or passive type air cleaner, and aircraft is in air pollution relatively
Serious region, the height at pollutant place carry out operation, it is achieved adsorb the pollutant in air
Or sedimentation, alleviate air pollution.
The solar energy dish lighter-than-air flight device of 24. collapsible air bags according to claim 1, its feature
Be, flight control system internal memory be placed with do not allow flight spatial domain coordinate, either manual operation, from
Dynamic driving still remote control all can not make aircraft pass through this no-fly region.
The solar energy dish lighter-than-air flight device of 25. collapsible air bags according to claim 1, its feature
Being, lighter-than-air flight device cabin interior can install aircraft, guided missile, rocket, space shuttle and spacecraft
Deng aerial vehicle launcher, by buoyancy and the Stabilization of lighter-than-air flight device self of dirigible, bring it to
In the air, its launch cost is reduced.
The solar energy dish lighter-than-air flight device of 26. collapsible air bags according to claim 1, its feature
Being, lighter-than-air flight device cabin interior can be the place that hotel, hotel and dining room etc. are used for going sightseeing to board and lodge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610396799.XA CN105947169A (en) | 2016-06-07 | 2016-06-07 | Solar saucer-shaped floating aircraft provided with shrinkable airbag |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610396799.XA CN105947169A (en) | 2016-06-07 | 2016-06-07 | Solar saucer-shaped floating aircraft provided with shrinkable airbag |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105947169A true CN105947169A (en) | 2016-09-21 |
Family
ID=56907825
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610396799.XA Pending CN105947169A (en) | 2016-06-07 | 2016-06-07 | Solar saucer-shaped floating aircraft provided with shrinkable airbag |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105947169A (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364658A (en) * | 2016-10-09 | 2017-02-01 | 华北水利水电大学 | Information collecting and monitoring device capable of staying in air for long time |
| CN106364656A (en) * | 2016-10-09 | 2017-02-01 | 华北水利水电大学 | Information collecting and monitoring device capable of staying in air for long time |
| CN106364659A (en) * | 2016-10-09 | 2017-02-01 | 华北水利水电大学 | Information collecting and monitoring device capable of staying in air for long time |
| CN106379508A (en) * | 2016-10-09 | 2017-02-08 | 华北水利水电大学 | Information collection and monitoring device with long-time blanking function |
| CN107284640A (en) * | 2017-07-11 | 2017-10-24 | 中国电子科技集团公司第三十八研究所 | A kind of integral vertically taking off and landing flyer of deformable buoyance lift and flying method |
| CN109941435A (en) * | 2019-04-08 | 2019-06-28 | 华南农业大学 | A kind of wide cut spray boom self-balancing aircraft and its control method |
| CN110466780A (en) * | 2019-08-19 | 2019-11-19 | 西安长峰机电研究所 | A kind of Helios |
| CN111776195A (en) * | 2020-07-17 | 2020-10-16 | 河北柒壹壹玖工业自动化技术有限公司 | Solar unmanned aerial vehicle capable of replacing satellite communication |
| CN111776229A (en) * | 2020-07-15 | 2020-10-16 | 河北柒壹壹玖工业自动化技术有限公司 | Gliding type solar unmanned aerial vehicle device replacing satellite communication |
| CN113525632A (en) * | 2021-07-09 | 2021-10-22 | 北京工商大学 | Underwater intelligent robot capable of floating upwards quickly |
| WO2021258444A1 (en) * | 2020-06-24 | 2021-12-30 | 深圳市巨鼎医疗股份有限公司 | Ventilation apparatus |
| RU2769036C1 (en) * | 2021-12-03 | 2022-03-28 | Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" | Unmanned aerial vehicle with electric power generation |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2327922A1 (en) * | 1975-10-15 | 1977-05-13 | Lorraines Elect Meca Entrepris | Propeller-driven passenger airship - has concentric toroidal inner tubes with aerodynamic canvas sheath |
| US5071383A (en) * | 1990-05-17 | 1991-12-10 | Jal Data Communications & Systems Co., Ltd. | Radio-controlled flying apparatus |
| WO2005032939A1 (en) * | 2003-10-03 | 2005-04-14 | Franz Autherith | Toroidal flying object |
| CN102205875A (en) * | 2010-12-29 | 2011-10-05 | 中国特种飞行器研究所 | Umbrella unfolding type airship air bag |
| CN103587674A (en) * | 2012-08-13 | 2014-02-19 | 中国空间技术研究院 | Airship airbag with shape-control frames |
| CN206087259U (en) * | 2016-06-07 | 2017-04-12 | 王庆方 | Solar energy dish of collapsible gasbag floats empty aircraft |
-
2016
- 2016-06-07 CN CN201610396799.XA patent/CN105947169A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2327922A1 (en) * | 1975-10-15 | 1977-05-13 | Lorraines Elect Meca Entrepris | Propeller-driven passenger airship - has concentric toroidal inner tubes with aerodynamic canvas sheath |
| US5071383A (en) * | 1990-05-17 | 1991-12-10 | Jal Data Communications & Systems Co., Ltd. | Radio-controlled flying apparatus |
| WO2005032939A1 (en) * | 2003-10-03 | 2005-04-14 | Franz Autherith | Toroidal flying object |
| CN102205875A (en) * | 2010-12-29 | 2011-10-05 | 中国特种飞行器研究所 | Umbrella unfolding type airship air bag |
| CN103587674A (en) * | 2012-08-13 | 2014-02-19 | 中国空间技术研究院 | Airship airbag with shape-control frames |
| CN206087259U (en) * | 2016-06-07 | 2017-04-12 | 王庆方 | Solar energy dish of collapsible gasbag floats empty aircraft |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364658B (en) * | 2016-10-09 | 2018-10-09 | 华北水利水电大学 | A kind of information collection that can be emptied for a long time and monitoring device |
| CN106364656A (en) * | 2016-10-09 | 2017-02-01 | 华北水利水电大学 | Information collecting and monitoring device capable of staying in air for long time |
| CN106364659A (en) * | 2016-10-09 | 2017-02-01 | 华北水利水电大学 | Information collecting and monitoring device capable of staying in air for long time |
| CN106379508A (en) * | 2016-10-09 | 2017-02-08 | 华北水利水电大学 | Information collection and monitoring device with long-time blanking function |
| CN106364658A (en) * | 2016-10-09 | 2017-02-01 | 华北水利水电大学 | Information collecting and monitoring device capable of staying in air for long time |
| CN106364656B (en) * | 2016-10-09 | 2018-06-08 | 华北水利水电大学 | A kind of information collection that can be emptied for a long time and monitoring device |
| CN106364659B (en) * | 2016-10-09 | 2018-10-09 | 华北水利水电大学 | A kind of information collection that can be emptied for a long time and monitoring device |
| CN106379508B (en) * | 2016-10-09 | 2018-10-09 | 华北水利水电大学 | A kind of information collection that can be emptied for a long time and monitoring device |
| CN107284640A (en) * | 2017-07-11 | 2017-10-24 | 中国电子科技集团公司第三十八研究所 | A kind of integral vertically taking off and landing flyer of deformable buoyance lift and flying method |
| CN109941435A (en) * | 2019-04-08 | 2019-06-28 | 华南农业大学 | A kind of wide cut spray boom self-balancing aircraft and its control method |
| CN110466780A (en) * | 2019-08-19 | 2019-11-19 | 西安长峰机电研究所 | A kind of Helios |
| WO2021258444A1 (en) * | 2020-06-24 | 2021-12-30 | 深圳市巨鼎医疗股份有限公司 | Ventilation apparatus |
| CN111776229A (en) * | 2020-07-15 | 2020-10-16 | 河北柒壹壹玖工业自动化技术有限公司 | Gliding type solar unmanned aerial vehicle device replacing satellite communication |
| CN111776195A (en) * | 2020-07-17 | 2020-10-16 | 河北柒壹壹玖工业自动化技术有限公司 | Solar unmanned aerial vehicle capable of replacing satellite communication |
| CN113525632A (en) * | 2021-07-09 | 2021-10-22 | 北京工商大学 | Underwater intelligent robot capable of floating upwards quickly |
| CN113525632B (en) * | 2021-07-09 | 2024-01-12 | 北京工商大学 | Underwater intelligent robot capable of quickly floating upwards |
| RU2769036C1 (en) * | 2021-12-03 | 2022-03-28 | Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" | Unmanned aerial vehicle with electric power generation |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105947169A (en) | Solar saucer-shaped floating aircraft provided with shrinkable airbag | |
| US11530036B2 (en) | Fixed-wing aerial underwater vehicle and control method thereof | |
| US7306187B2 (en) | Inflatable endurance unmanned aerial vehicle | |
| KR101883896B1 (en) | Buoyant aerial vehicle | |
| CA2872028C (en) | Unmanned aerial vehicle | |
| CN108146169B (en) | Wing rear-folding type air-ground dual-purpose carrier | |
| US10081424B2 (en) | Flying car or drone | |
| US9487286B2 (en) | Lift and propulsion device, and heavier-than-air aircraft provided with such a device | |
| US20160207626A1 (en) | Airborne Surveillance Kite | |
| CN104139845B (en) | Unmanned aerostat system | |
| US20170253325A1 (en) | Unmanned aerial vehicle (uav) and a method of improving the performance thereof | |
| CN104925243B (en) | A kind of variable inflated type buoyance lift integration stratospheric airship of span | |
| CN109515674B (en) | Hybrid vertical take-off and landing vehicle | |
| CN109606605B (en) | Many rotors of dirigible combined type aircraft | |
| CN105730170B (en) | Four culvert vertical take-off and landing hovercars | |
| CN108116668A (en) | The land and air double-used more rotor manned aircraft of full electricity | |
| US10933975B2 (en) | Variable geometry airframe for vertical and horizontal flight | |
| CN108995802B (en) | Modular propulsion system and aircraft capable of vertical takeoff and landing | |
| CN206968327U (en) | A kind of hovercar | |
| US10689105B2 (en) | Passenger-carrying rotorcraft with fixed-wings for generating lift | |
| US11179989B2 (en) | Triphibian vehicle | |
| CN105966605A (en) | Delta parallel mechanism-based six-rotor aircraft | |
| CN101857087A (en) | Dual-rotor dish-shaped aircraft | |
| CN105730168B (en) | Three culvert vertical take-off and landing hovercars | |
| CN206087259U (en) | Solar energy dish of collapsible gasbag floats empty 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 | ||
| AD01 | Patent right deemed abandoned | ||
| AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20190409 |