CN106043711A - Flight method and aircraft - Google Patents
Flight method and aircraft Download PDFInfo
- Publication number
- CN106043711A CN106043711A CN201610301893.2A CN201610301893A CN106043711A CN 106043711 A CN106043711 A CN 106043711A CN 201610301893 A CN201610301893 A CN 201610301893A CN 106043711 A CN106043711 A CN 106043711A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- air force
- energy
- air
- container
- 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
- 238000000034 method Methods 0.000 title claims abstract description 14
- 230000005484 gravity Effects 0.000 claims description 11
- 238000013461 design Methods 0.000 claims description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 6
- 238000006073 displacement reaction Methods 0.000 claims description 6
- 238000001514 detection method Methods 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 3
- 239000013536 elastomeric material Substances 0.000 claims description 3
- 239000001307 helium Substances 0.000 claims description 3
- 229910052734 helium Inorganic materials 0.000 claims description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 3
- 238000005381 potential energy Methods 0.000 claims description 3
- 230000001133 acceleration Effects 0.000 claims description 2
- 230000004907 flux Effects 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000002245 particle Substances 0.000 claims description 2
- 230000026676 system process Effects 0.000 claims description 2
- 230000007704 transition Effects 0.000 claims 1
- 239000003570 air Substances 0.000 description 70
- 230000033001 locomotion Effects 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 6
- 230000004888 barrier function Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 230000009194 climbing Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000010006 flight Effects 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 238000002604 ultrasonography Methods 0.000 description 2
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 1
- 235000017491 Bambusa tulda Nutrition 0.000 description 1
- 241001330002 Bambuseae Species 0.000 description 1
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 239000011425 bamboo Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 210000000744 eyelid Anatomy 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000000178 monomer Substances 0.000 description 1
- 238000011112 process operation Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
The invention provides a flight method and an aircraft. The aircraft is composed of a container, an aerodynamic forming device fixedly connected with the container and an intelligent control system connected with the aerodynamic forming device. The container is a volumetric container and can form certain buoyancy. The aerodynamic forming device is designed according to the aerodynamic principle and can form certain aerodynamic force. Furthermore, the intelligent control system is arranged on the aircraft in order to achieve intelligent driving of the aircraft. By the adoption of the flight method, the aircraft does not fly by being pushed through a single force of the buoyancy formed by the aircraft or the aerodynamic force formed by the aerodynamic forming device of the aircraft. The method is characterized in that two forces of the buoyancy formed by the aircraft and the aerodynamic force generated by the aerodynamic forming device of the aircraft jointly act on the aircraft to achieve flight, and through control over the aerodynamic force, the aircraft takes off, flies and lands.
Description
Technical field
The present invention relates to technical field of aerospace, be specifically related to a kind of flying method and aircraft.
Background technology
The most artificial flying method mainly has three kinds,
The first is that the law of buoyancy according to Archimedes manufactures, and such as balloon, hot balloon etc., only considers spheroid or lamp during design
Body forms this factor of size of buoyancy, so needing the material of weight to be able to mention, the spheroid of balloon makes very
Huge, the fire balloon volume of seven grades is 2000-2400M3, the balloon volume of ten grades reach 6000M3；Hot balloon is due to its small volume
Limited being little to of buoyancy formed mentions any weight, so not having what use value, this simple dependence buoyancy realizes
The method of flight, owing to not having autonomous dynamic, is difficulty with controllable flight.
The second manufactures according to aerodynamic principle, such as aircraft, rocket, guided missile, unmanned plane etc., mainly by machine
The air force that tool motion or warm-up movement are formed promotes, and realizes when thrust upwards is more than gravity rising and flight, buoyancy pair
The impact of this kind of aircraft is almost negligible, so this flying method is difficulty with steadily hovering.
The third is that the law of buoyancy according to Archimedes realizes flight, and plane motion is realized by air force, as
Dirigible, although he also achieves hovering and motion, but its lifting is the most only by one controlling factors of buoyancy, it is difficult to realize freely
Lifting.
The weight that fire balloon is bulky, hot balloon is mentioned is limited；And the smooth flights such as aircraft, rocket, guided missile, unmanned plane
Difficulty；Dirigible lifting can not freely realize.
Summary of the invention
For the problems referred to above, the present invention proposes a kind of flying method, including by container with fix the sky being connected with container
Aerodynamic force forms device and forms the aircraft of the intelligence control system composition that device is connected with air force；
Described container is positive displacement container, and he can form certain buoyancy, and the buoyancy that he is formed is not more than this aircraft
Gravity；Helium/air/hydrogen gas/be vacuum it is filled with in described container；Further, it is a list that described container does not limit
Body, can be two or the assembly of several difformity monomer；
Described air force formation device is according to aerodynamic principle design system, and he can form certain air and move
The buoyancy sum of power, the air force that it is formed and this aircraft is not less than the gravity of this aircraft；
Further, described air force forms device and is not intended to the form of energy, kind and quantity, can be mechanical energy and/
Or heat energy and/or luminous energy and/or electric energy and/or the air force such as acoustic energy and/or particle flux form device；
Further, the purpose left a blank for a long time to make this aircraft reach, the air force of this aircraft forms device at least
Having one is that solar energy provides power, takes
Daytime is formed air force by the air in solar energy heating container, or
Air force is formed by solar energy blower fan, or
Blower fan is driven to form air force by solaode,
Realize driving the machine flight, to reduce the consumption of the energy entrained by self, originally fly when the energy of solar energy is not enough to support
Self energy feed system is started, when when being supplied with remaining of solar energy, by unnecessary solar energy by heat energy during row device normal flight
Type air compressor is changed into air force energy, heat energy type vacuum machine is transformed into vacuum power energy, heat energy type electromotor is transformed into
Electric energy or heat engine are transformed into the potential energy of elastomeric material and store；
Further, in order to make this aircraft realize free flight aloft, air force forms the air force of device and can export
Do not limit the side, ground only to the earth；The most do not limit and only set an outlet；
Further, in order to make this aircraft realize intelligent driving, the machine is provided with intelligence control system, described Based Intelligent Control
System includes:
Attitude and state control system include electronic gyroscope and speed and acceleration transducer；
Obstacle detection and avoidance system include the ADS-B module actively prevented, and the ultrasonic module of emergent avoidance, infrared sense
Answer module and image information collecting module；
Global positioning system；
Informix processing system,
Described attitude and state control system, obstacle detection and avoidance system, global positioning system process with informix
System is connected, and informix processing system and air force can form on off controller/and the air force energy delivery outlet of device
Starting controller is connected.
The air force that the flying method of the present invention is not the buoyancy formed by this aircraft or this aircraft is formed is formed
Try hard to recommend this aircraft dynamic realization flight for one that the air force of device formation is single, it is characterised in that be by this aircraft shape
The buoyancy become and the air force of this aircraft form two power of air force of device generation and jointly act on this aircraft in fact
Now fly, by controlling aerodynamic size, make this aircraft realize lift-off, fly and land, thus make balloon, hole
Bright lamp, dirigible isometric(al) type aircraft, mainly limited by buoyancy parameter control, can only be made sufficiently bulky epoch and aircraft not
The controlled epoch that drift with the wind termination, makes displacement type aircraft enter into controlled independently circling in the air the epoch.
In order to reduce the thermal loss that solar energy and burner produce, the eyelid covering of positive displacement container at least one layer be with adopting
Make of the heat conductivity transparent adiabator less than 0.003w/m.k.
Concrete grammar is such that
Started air force when this aircraft is to be gone up to the air and form device so that it is produce and be perpendicular to ground thrust upwards, when floating
When power and thrust sum upwards are more than the gravity of this aircraft, this aircraft goes up to the air, and controls thrust and buoyancy sum and gravity
Keeping balance, this aircraft can the most steadily stop, when needing to advance by intelligence control system by the sky of this aircraft
Aerodynamic force can after export and open, delivery air kinetic force realizes advancing, when needs retreat by intelligence control system by this flight
The air force of device can before outlet open, delivery air kinetic force realizes back leg, and it is same to move to left and move to right principle, works as needs
During landing, reduce air force and form the air force that device produces, make air force and buoyancy sum less than this aircraft
Gravity, makes this aircraft realize slowly and declines.
When state of flight and flight attitude sensor senses are to self state of flight exception, carry out manually or controlled by intelligence
System automatic-posture-adjustment processed, when the ADS-B module real-time reception of active obstacle is to the flight letter of other aircraft in neighbouring spatial domain
Breath, cooks up the optimal route of the machine in real time, when the emergent obstacle of needs, and spatial domain object near the machine that the machine is collected
Ultrasound information, the infrared information sensed and image information are comprehensively analyzed, and determine character and the trend of barrier, with this
Compare in the course line of aircraft, it may be judged whether the flight of this aircraft of image, as impact is taked by intelligence control system accordingly
Measures to keep clear；The course line that the ownship position information that the machine collects according to global positioning system and the machine are planned at the beginning of taking off is entered
Optimal route is planned in the real-time comparison of row again, it is achieved autonomous flight.
The present invention has the advantage that compared with existing aircraft
Compared with fire balloon: owing to this aircraft improves the ratio that air force is shared in fire balloon climbing power, unlike existing
Fire balloon limited by buoyancy parameter, it is necessary to being made to very big, it is the least that it can design as required, can make steam
This sports events of ball realizes popular, and its application also will expand further, as being applied to take photo by plane, monitoring, communication,
The fields such as air transport.
Compared with hot balloon: do not limited by the lightweight materials such as thin bamboo strips used for weaving, paper, cloth originally can only be used to make, draw materials more
Add extensively, and become the aircraft with extensive application.
Compared with the aircraft such as aircraft, rocket, guided missile: aircraft, rocket, guided missile, unmanned plane etc. rely on merely air force
Promote object, suitably increase buoyancy proportion in climbing power, the VTOL of aircraft and unmanned plane can be realized, steadily fly
OK, militarily can accomplish to monitor the purpose hit of selecting a time in real time.
Compared with dirigible: achieve and can be freely lifted.Ground anchoring, mooring process operation difficulty when the lift-off of dirigible, landing
Degree is big, it is desirable to have substantial amounts of ground crew is matched could be realized, because the flying method of this aircraft is different, is not
Tried hard to recommend dynamic the machine by single one of buoyancy and realize flight, it is characterised in that jointly acted on by buoyancy and two power of air force
In this aircraft, this aircraft only need to be by controlling aerodynamic size, it is achieved freely goes up to the air, fly and lands.
Accompanying drawing explanation
Fig. 1 is a fire balloon with the technology path design of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing, the design concept of the present invention is described further.
It is understood that the making of fire balloon and hot balloon only considers this parameter of buoyancy, due to air formed buoyancy relatively
Little, need the material of weight to be able to mention, it is the hugest that the spheroid of fire balloon makes；Hot balloon is due to small volume, shape
The buoyancy become is limited, so being unable to lift what weight, over more than 2,000 year, hot balloon never changes.
It is understood that aircraft, rocket, guided missile, unmanned plane etc., the air force mainly formed by mechanical movement or warm-up movement
Promoting, realize when thrust upwards is more than gravity rising and flight, the impact of this kind of aircraft almost can be ignored by buoyancy
Disregard, but it is extremely difficult to achieve steadily hovering.
And this aircraft strength proportioning, the technology path that he changes fire balloon and hot balloon relies on merely buoyancy to fly,
Making hot balloon and fire balloon be unlikely to be limited by the constraint of a parameter, can design more freely, fire balloon can do very
Little, it is more conducive to the universal of this motion, the most a miniature fire balloon mixes relevant instrument, will have widely at Military and civil fields
Application；Can become a low flyer truly after the elevated air force of hot balloon, it has again it steady simultaneously
Qualitative good advantage, can make hot balloon not only be applied to pray for blessings；When the buoyancy changing the aircraft such as aircraft, rocket, guided missile
After the strength proportioning of climbing power, them can be made more to save the energy, it is possible to achieve steadily hover, supervision real-time to target,
Select a time strike.
Fig. 1 is a aircraft with the technology path design of the present invention, and this aircraft includes container 1 and air force shape
Become device heat engine type blower fan 2；Described container is positive displacement container, and he can form certain buoyancy, and the size of buoyancy is not more than
The gravity of this aircraft, take due to this example is that air force is formed the layout that device heat energy type blower fan is placed in container,
Gas in container 1 be floating life gas be also air force can execution gas, so needing to set air intake 3 and air moves
Power can export, and when container 1 forms, with air force, the layout that device takes other forms, container can be designed to vacuum,
Or it being filled with helium, hydrogen or air, top is located at by the air intake 3 of described container, is connected with getter device 5, during such air-breathing
Also forming certain lifting force, described getter device 5 is connected with control pressurer system, control pressurer system and pressure transducer
Being connected, the pressure parameter that pressure transducer collects feeds back to control system, according to opening of the Stress control getter device set
Stop, make container maintain in the pressure limit of setting；1 body sidewall of described container is provided with at least 4 air forces and can export
4.1, i.e. each side, four sides, the front, rear, left and right of this container can export 4.1 at least provided with 1 air force, and bottom is extremely
Being provided with 1 air force less and can export 4.2, more steady in order to make the machine fly, the machine bottom is provided with 3 air forces and can go out
Mouth 4.2；The energy outlet that described air force can export with air force formation device communicates, and described air force can go out
Mouth is provided with starting controller, starting controller realize the open and close that air force can export, starting controller and intelligence
Control system, barrier are evaded control system and are connected with autonomous cruise control system, can go out when needs rise air force at present
Mouth is opened under control of the control system, sprays from end opening with high-octane gas, drives this aircraft to go up to the air, when before needs
After when entering, air force can export and open, when needs retreat before air force can export and open, when needs move to right, left air
Kinetic force outlet is opened, and when needs move to left, right air force can export and open；Avoiding barrier is also so；
Described air force can be formed on the supporting surface of the lower plane formation that device is placed in positive displacement container；After the machine outbound
Starting heat energy type blower fan 2, when the buoyancy sum that thrust upwards and this container are formed is more than the gravity of the machine, the machine realizes flying
OK, during flight, solar energy constantly adds the air in heat container, and the power formed when solar energy be enough to promote the machine to fly
During row, close heat engine, to save the energy entrained by the machine, when when being supplied with remaining of solar energy, by unnecessary solar energy by heat
Type air compressor is changed into air force energy to energy, heat energy type vacuum machine is transformed into vacuum power energy, heat energy type electromotor changes
The potential energy becoming electric energy or heat engine to be transformed into elastomeric material is stored；When the sundowners solar energy be enough to drive this aircraft flight
Time, start the energy of storage on daytime, when storing energy and can not maintain the machine normal flight, start heat energy type blower fan and drive the machine
Flight, when needs land, reduces air force and forms the power that device produces, make air force and buoyancy sum less than originally flying
The weight of row device, makes this aircraft realize slowly and declines.
In flight course, when state of flight and flight attitude sensor senses are to self state of flight exception, carry out
Manually or automatically posture adjustment, with other flights in the ADS-B module real-time reception of active obstacle during flight to neighbouring spatial domain before flight
The flight information of device, cooks up the optimal route of the machine in real time, when the emergent obstacle of needs, near the machine the machine collected
The ultrasound information of spatial domain object, infrared information and image information are comprehensively analyzed, and determine character and the trend of barrier, with
The course line of this aircraft contrasts, if the flight of this aircraft of image, takes to dodge accordingly as affected the flight of the machine
Measure；The course line that the ownship position information that the machine collects according to global positioning system and the machine are planned at the beginning of taking off is carried out in real time
Optimal route is planned in contrast in real time.
The description that above embodiment specific illustrative to the present invention is presented is in order at the purpose of illustration and description, not
It is intended to limit the invention to disclosed precise forms, it is clear that much changing according to above-mentioned technology path and changing is all can
Can.Select fire balloon exemplary and to be described be the particular technology route in order to explain the present invention, so that
Others skilled in the art are capable of, and utilize the exemplary of the present invention and different choice form thereof and
Modification.The scope of the present invention is intended to be limited by appended claims and the equivalent form of value thereof.
Claims (6)
1. a flying method, including by container and fix with container the air force being connected formed device and with air force shape
The aircraft that the intelligence control system becoming device to be connected is constituted；
The flying method of the present invention is not the buoyancy only formed by container or is only formed, by air force, the air that device formed and move
One that power is single tries hard to recommend dynamic the machine and realizes flight, it is characterised in that be the buoyancy and this aircraft formed by this aircraft
Air force forms two power of air force of device formation and jointly acts on what this aircraft realized, by controlling this aircraft
Air force formed device formed aerodynamic size, make this aircraft realize lift-off, fly and land.
2. can realize an aircraft for purpose described in claim 1, including container with fix the air force being connected with container
Form device and form, with air force, the intelligence control system that device is connected；
Described container is positive displacement container, and he can form certain buoyancy, and the buoyancy that he is formed is not more than this aircraft
Gravity；
Described air force formation device is according to aerodynamic principle design system, and he can form certain air and move
The buoyancy sum of power, the air force that it is formed and this aircraft is not less than the gravity of this aircraft；
Described intelligence control system includes:
Attitude and state control system include electronic gyroscope and speed and acceleration transducer；
Obstacle detection and avoidance system include the ADS-B module actively prevented, and the ultrasonic module of emergent avoidance, infrared sense
Answer module and image information collecting module；
Global positioning system；
Informix processing system,
Described attitude and state control system, obstacle detection and avoidance system, global positioning system process with informix
System is connected, and informix processing system and air force can form on off controller/and the air force energy delivery outlet of device
Starting controller is connected.
3. in the container of as claimed in claim 2 aircraft, it is filled with helium/air/hydrogen gas or vacuum.
4. the air force of aircraft forms device as claimed in claim 2, does not limit the form of energy, kind and quantity, can
To be mechanical energy and/or heat energy and/or luminous energy and/or electric energy and/or acoustic energy and/or particle flux air force forms device, but
At least an air force forms device is provided energy by solar energy.
5. solar air power as claimed in claim 4 forms device, takes
Daytime is formed air force by the air in solar energy heating container, or
Air force is formed by solar energy blower fan, or
Blower fan is driven to form air force by solaode,
Realize driving the machine flight, to reduce the consumption of the energy entrained by self, originally fly when the energy of solar energy is not enough to support
Self energy feed system is started, when when being supplied with remaining of solar energy, by unnecessary solar energy by heat energy during row device normal flight
Type air compressor is changed into air force energy/and heat energy type vacuum machine is transformed into vacuum power energy/and heat energy type electromotor turns
Become electric energy or heat engine engine transitions becomes the potential energy of elastomeric material to store.
6. aircraft as claimed in claim 2, freely-movable aloft in order to make this aircraft realize, air force forms device
Air force can export and not limit only to side, ground；The most do not limit and only set an outlet；Each aircraft does not limit with one
Set air force forms device；The most do not limit and provided air force by a kind of energy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610301893.2A CN106043711A (en) | 2016-05-09 | 2016-05-09 | Flight method and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610301893.2A CN106043711A (en) | 2016-05-09 | 2016-05-09 | Flight method and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106043711A true CN106043711A (en) | 2016-10-26 |
Family
ID=57176237
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610301893.2A Pending CN106043711A (en) | 2016-05-09 | 2016-05-09 | Flight method and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106043711A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107745814A (en) * | 2017-11-15 | 2018-03-02 | 航宇救生装备有限公司 | A kind of active landed for aerial delivery system is anti-to turn over controlling organization |
| CN108475065A (en) * | 2017-06-30 | 2018-08-31 | 深圳市大疆创新科技有限公司 | Method of controlling security, equipment and the machine readable storage medium of unmanned plane during flying |
-
2016
- 2016-05-09 CN CN201610301893.2A patent/CN106043711A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108475065A (en) * | 2017-06-30 | 2018-08-31 | 深圳市大疆创新科技有限公司 | Method of controlling security, equipment and the machine readable storage medium of unmanned plane during flying |
| CN107745814A (en) * | 2017-11-15 | 2018-03-02 | 航宇救生装备有限公司 | A kind of active landed for aerial delivery system is anti-to turn over controlling organization |
| CN107745814B (en) * | 2017-11-15 | 2023-12-22 | 航宇救生装备有限公司 | Active anti-overturning control mechanism for landing of air drop system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10810894B2 (en) | Deep stall aircraft landing | |
| US10112694B2 (en) | Self-righting aeronautical vehicle and method of use | |
| De Croon et al. | The delfly | |
| US9725158B2 (en) | Self-righting frame and aeronautical vehicle and method of use | |
| US20200182613A1 (en) | Inverted-Landing Aircraft | |
| US10144509B2 (en) | High performance VTOL aircraft | |
| CN106114853B (en) | A kind of push-button aircraft | |
| CN106114854B (en) | A kind of push-button aircraft | |
| US7980510B2 (en) | Small unmanned aircraft | |
| US10577097B2 (en) | Glider for airborne wind energy productions | |
| US20100051755A1 (en) | Tail-less boxed biplane air vehicle | |
| US11117657B2 (en) | Aeronautical apparatus | |
| US20140014767A1 (en) | Self-Righting Frame And Aeronautical Vehicle | |
| CN108058802A (en) | A kind of variable density unmanned airship based on solar energy | |
| CN107499513A (en) | Microminiature can hover Fixed Wing AirVehicle | |
| CN106672231A (en) | Unmanned aerial vehicle | |
| Krashanitsa et al. | Flight dynamics of a flapping-wing air vehicle | |
| US10246185B2 (en) | Aircraft system and method for vertical takeoff and landing | |
| CN102167160A (en) | Miniature flapping wing aircraft launching in jumping mode | |
| CN204056287U (en) | A kind of autonomous flight is without active force unmanned plane | |
| CN108425541A (en) | A kind of unmanned plane sunshade flies paulin and its implementation | |
| CN106043711A (en) | Flight method and aircraft | |
| CN106005371B (en) | Difference directly drives dynamic three rudder face unmanned planes entirely | |
| WO2019042238A1 (en) | Flapping-wing flying blimp | |
| Robertson et al. | Design and perching experiments of bird-like remote controlled planes |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161026 |