CN206218244U - Aircraft and flight system - Google Patents
Aircraft and flight system Download PDFInfo
- Publication number
- CN206218244U CN206218244U CN201621313416.XU CN201621313416U CN206218244U CN 206218244 U CN206218244 U CN 206218244U CN 201621313416 U CN201621313416 U CN 201621313416U CN 206218244 U CN206218244 U CN 206218244U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- flight
- harvester
- environment
- data
- 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.)
- Active
Links
Abstract
The utility model discloses a kind of aircraft and flight system.Wherein, the aircraft includes：Harvester, the environmental data for gathering aircraft flight environment；Whether processor, is connected with the harvester, the flight for detecting the suitable aircraft of the flight environment of vehicle based on the environmental data；Protection device, is connected with the processor, during for the flight for being not suitable for the aircraft in the flight environment of vehicle, protection act is performed, to protect the aircraft.The utility model solves the technical problem that cannot effectively protect aircraft.
Description
Technical field
The utility model is related to space industry, in particular to a kind of aircraft and flight system.
Background technology
Traditional environmental detection set is typically to be only used for the environment measuring on ground, it is impossible to really detect aerial ring
The high costs such as the concrete condition in border, aircraft sampling, aerostat, it is impossible to popularize.
Detection means is carried according to aircraft, due to there is no environmental protection link in the middle of current aerocraft system,
And aircraft interior avionics safeguard measure is limited, when environmental catastrophe (bust heavy rain, dash forward and carry out strong wind) is run into, often price is held high
Expensive aircraft can be lost by different degrees of, meeting directly born destruction when serious, lose huge.
When receiving such environmental effects for aircraft at present, mainly there are two approach to protect：First is to pass through
Weather forecast or other approach predicting means obtain environmental information to take safeguard measure in advance, and second is that aircraft is flying
During row, operator is by the environmental information of earth station or artificially judges that whether current environment has infringement to aircraft, and right
Safeguard measure is taken in flight.
Conventionally, anticipation weather has certain inaccuracy, and passes through earth station or artificial judge
Protected mode, due to aircraft and earth station and operator relatively far away from, when there are environmental catastrophe (bust heavy rain etc) feelings
During condition, operator cannot take efficient safeguard measure to aircraft in-flight in time, so as to cause aircraft to be subjected to necessarily
Loss.
For the above-mentioned problem that cannot effectively protect aircraft, effective solution is not yet proposed at present.
Utility model content
The utility model embodiment provides a kind of aircraft and flight system, at least to solve effectively protect flight
The technical problem of device.
According to the one side of the utility model embodiment, there is provided a kind of aircraft, it is characterised in that including：Collection
Device, the environmental data for gathering aircraft flight environment；Processor, is connected, for based on described with the harvester
Whether environmental data detects the flight of the suitable aircraft of the flight environment of vehicle；Protection device, is connected with the processor, uses
When the flight of the aircraft is not suitable in the flight environment of vehicle, protection act is performed, to protect the aircraft.
Further, the harvester is arranged on sampling plate, and the sampling plate is arranged on the frame of the aircraft
Lower section.
Further, the aircraft is dirigible, and the harvester is arranged in the nacelle of gondola, and the gondola is installed
On the dirigible.
Further, the harvester includes at least one following：Temperature sensor, humidity sensor, PM2.5 detections
Device.
Further, aircraft also includes data storage transmitting device, is connected with harvester, for storage environment number
According to, and environmental data is sent to control terminal.
Further, harvester includes：Information input interface, information input interface is used to receive meteorological equipment transmission
Environmental data.
Further, meteorological equipment includes at least one following：Meteorological satellite, weather information record terminal and air detection
Device, wherein, weather information record terminal is used for the environmental data in record-setting flight device flight location；Air detecting device is set
On board the aircraft or on building, the distance of building and aircraft is without departing from preset distance.
Further, data storage transmitting device is arranged in the frame of aircraft, or, it is the feelings of dirigible in aircraft
Under condition, the data storage transmitting device is arranged in the nacelle of the gondola of the dirigible.
Further, the aircraft also includes：Locator, the position for positioning the aircraft, wherein, institute's rheme
Put the flight original position including the aircraft；The processor, is connected with the locator, in the flight environment of vehicle
When being not suitable for the flight of the aircraft, generation protection instruction；The protection device is performed under the triggering of the protection instruction
The protection act.
Further, the locator includes at least one following：GPS positioning unit, remote sensor and light spread
Sensor.
According to the another aspect of the utility model embodiment, a kind of flight system is additionally provided, including：In above-described embodiment
Any one aircraft；Control terminal, with the aircraft wireless connection, for controlling the aircraft, and receives described flying
The data that row device is returned.
Further, the control terminal includes at least one following：Remote control, mobile terminal and earth station.
In the utility model embodiment, by setting harvester, processor and protection device etc. on board the aircraft
Equipment, the information of Real-time Collection aircraft flight environment, and judged according to the information for collecting, judge current flight ring
The whether suitable aircraft flight in border.It is under flyable state in aircraft, aircraft normally runs.It is in aircraft
It is not suitable in the state of flight, aircraft performs protection act.So as to, aircraft can according to the real-time status of flight environment of vehicle,
Corresponding countermeasures are taken, aircraft is reduced in the environment of mutation by being influenceed, reduction is given because of the mutation of environment
The loss that aircraft brings.Also, because the aircraft can reduce the losing for bringing by flight environment of vehicle mutation, so making
Air environment monitoring is carried out with the flight, the loss of air environment monitoring device can be reduced, so that reduces cost.And then solve
The technical problem of aircraft cannot effectively be protected.
Brief description of the drawings
Accompanying drawing described herein is used for providing being further understood to of the present utility model, constitutes the part of the application,
Schematic description and description of the present utility model is used to explain the utility model, does not constitute to of the present utility model improper
Limit.In the accompanying drawings：
Fig. 1 is a kind of aircraft schematic diagram according to the utility model embodiment；
Fig. 2 is a kind of flight system schematic diagram according to the utility model embodiment；
Fig. 3 is a kind of optional aircraft schematic diagram according to the utility model embodiment.
Specific embodiment
In order that those skilled in the art more fully understand the utility model scheme, below in conjunction with the utility model reality
The accompanying drawing in example is applied, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described
Embodiment is only the embodiment of the utility model part, rather than whole embodiments.Based on the reality in the utility model
Example is applied, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made all should
When the scope for belonging to the utility model protection.
It should be noted that term " first " in specification and claims of the present utility model and above-mentioned accompanying drawing,
" second " etc. is for distinguishing similar object, without for describing specific order or precedence.It should be appreciated that so
The data for using can be exchanged in the appropriate case, so that embodiment of the present utility model described herein can be with except at this
In diagram or description those beyond order implement.Additionally, term " comprising " and " having " and their any deformation, meaning
Figure is that covering is non-exclusive to be included, for example, contain a series of system of units, product or equipment to be not necessarily limited to clearly arrange
Those units for going out, but may include other units do not list clearly or intrinsic for these products or equipment.
Fig. 1 is a kind of aircraft schematic diagram according to the utility model embodiment, as shown in figure 1, the aircraft includes：Adopt
Acquisition means 10, the environmental data for gathering aircraft flight environment；Processor 12, is connected with harvester, for based on ring
The flight of the border whether suitable aircraft of Data Detection flight environment of vehicle；Protection device 14, is connected with processor, in flight environment of vehicle
When being not suitable for the flight of aircraft, protection act is performed, to protect aircraft.
According to the utility model above-described embodiment, by carry-on harvester, collection aircraft flight environment
Environmental data, then the environmental data of collection is transmitted to processor.Within a processor, according to the environmental data for collecting, detection
The whether suitable aircraft flight of current environment, and testing result is transmitted to protection device.Protection device according to testing result, certainly
Determine whether aircraft performs protection act.The program, by setting harvester, processor and protection device on board the aircraft
Etc. equipment, the information of Real-time Collection aircraft flight environment, and judged according to the information for collecting, judged current flight
The whether suitable aircraft flight of environment.In the case where environment is not suitable for aircraft flight, it is protected, such that it is able to have
Effect protection aircraft, solves the technical problem that cannot effectively protect aircraft in the prior art.
In the above-described embodiments, detecting in the case that current flight environment is not suitable for aircraft flight, control flight
Device performs protection act.Detecting in the case that current flight environment is not suitable for aircraft flight, do not taking protection act, flying
Row device normally runs.
By above-described embodiment, in aircraft in the state of being not suitable for flying, aircraft performs protection act.From
And, aircraft can take corresponding countermeasures according to the real-time status of flight environment of vehicle, reduce ring of the aircraft in mutation
By being influenceed under border, the loss that reduction brings by the mutation of environment to aircraft.Also, because the aircraft can be reduced
What is be mutated by flight environment of vehicle and brought loses, so carrying out air environment monitoring using the flight, can reduce air environment prison
The loss of device is surveyed, so that reduces cost.And then solve the technical problem that cannot effectively protect aircraft.
Further, harvester can be with the environmental information of Real-time Collection aircraft local environment, it is also possible to receive meteorological
The weather information of office's collection.
Alternatively, harvester can include：Information input interface, information input interface is used to receive meteorological equipment transmission
Environmental data.Wherein, meteorological equipment includes at least one following：Meteorological satellite, weather information record terminal and air detection
Device, wherein, weather information record terminal is used for the environmental data in record-setting flight device flight location；Air detecting device is set
On board the aircraft or on building, the distance of building and aircraft is without departing from preset distance.
According to above-described embodiment, the harvester can include the information input for receiving aircraft flight environmental information
Interface, the information input interface can receive the ring for being sent that aircraft flight location weather bureau or meteorological satellite are sent
Border data；And/or, information input interface can receive the environmental data sent by air detecting device.
Further, air detecting device can be the device for real-time detection environmental information, it is possible to will detect
Environmental information transmit to harvester.
Alternatively, air detecting device, may be mounted in flight, the data of real-time detection aircraft flight environment.
Alternatively, air detecting device, may be mounted on the building of aircraft flight contextual vicinity, for example, be arranged on
On the high tower of aircraft flight contextual vicinity, on tree, on high building etc., the data of sense aircraft flight environment of vehicle, and by the ring
Border data send, and are received by the reception device (information input interface described above) of aircraft.
Further, by processor, the flight environment of vehicle information that harvester is collected is detected.Its detection process
Can be that flight environment of vehicle data are compared with environmental data set in advance.Do not met in current flight environmental data predetermined
In the case of environmental data, the result of detection is to be not suitable for flight；Meet specific environment data in current flight environmental data
In the case of, the result of detection is suitable flight.
Alternatively, environmental data set in advance can include multiple environmental datas, and Arbitrary Term does not meet pre- wherein
In the case of determining environmental data, processor just can draw the testing result for being not suitable for flight.For example, environmental data set in advance
Can include：Multiple data item such as limitation flight temperature, humidity and wind speed, in current flight environmental data wherein at least one
In the case that data item does not meet specific environment data, processor just can draw the testing result for being not suitable for flight.
Alternatively, specific environment data can be obtained by from aircraft manufacturer, and the manufacturer of aircraft is in order to allow
Aircraft is preferably protected, and can all indicate aircraft storage condition condition and flight environment of vehicle condition, and these information are in explanation
Mark is had in book, user can be set according to the conditional information.Can also be previously written for the data predetermined by other manufacturer
Environmental data, so as to be set without user.
Alternatively, specific environment data, can be as obtained by the experience of aircraft user.User is by using aircraft
Experience, obtain aircraft can with the flight environment of vehicle parameter of safe flight so that artificially be input into specific environment data.
Further, protection device, in the case where the testing result for being not suitable for flight that processor draws is received, holds
Row protection act.
Alternatively, the operation for performing protection act can be, flight control system sends control aircraft, and to do protection dynamic
A series of flare maneuvers instruction made, and using the instruction as being the first preferential operation for performing, user is to aircraft for cut-out
Control operation.
In another optional embodiment, harvester is arranged on sampling plate, and sampling plate is arranged on the machine of aircraft
Frame lower section.Specifically, sampling apparatus is arranged on sampling plate, and sampling plate and sampling apparatus is arranged on aircraft frame
Lower section.During aircraft flight, the air sample of flight environment of vehicle is gathered by the sampling plate below aircraft, and
Air sample according to collecting draws the environmental information of current flight environment.Sampling plate is arranged under the frame of aircraft
Side, frame is the framework material of aircraft, and its intensity is high, and weight is big.Sampling plate and frame are installed, the peace of sampling plate can be made
Dress is more firm.And sampling plate weight is small, sampling plate and frame are installed, can make aircraft after sampling plate is installed to flying
The influence of row device is smaller.Sampling plate is arranged on frame lower section, aircraft flight unit can not be influenceed.
Alternatively, sampling plate includes power supply module, Temperature and Humidity module, PM2.5 detection modules, ARM control modules,
Sampling plate is arranged on frame lower section, and flight control system is electrically connected with sampling plate.According to the air sample for collecting, by adopting
The Temperature and Humidity module of model, PM2.5 detection modules draw the flight environment of vehicle information representated by air sample, and this is flown
Row environmental information is processed flight environment of vehicle information by arm processor control module, generates data mode, is easy to follow-up
The application of transmission.Wherein, the power supply module can be lithium battery power supply module, the Temperature and Humidity mould set on sampling plate
Block, PM2.5 detection modules and ARM processing and control modules are operated by the electric power that power supply module is provided.And the sampling plate
With flight control system electrical connection, it is easy to for flight environment of vehicle information and flight control system to do data transfer.
According to the utility model above-described embodiment, aircraft is dirigible, and harvester is arranged in the nacelle of gondola, gondola
On dirigible.The top of dirigible is typically to be lighter than the floatage air bag of air for filling, and propulsion and direction controlling dress
Put；In the bottom of dirigible, gondola is set.Driving cabin is set in gondola, and engine and personnel compartment are (if manned fly
Ship).It is not influence airship flight according to the structure of dirigible in the case where aircraft is dirigible, can will be used for collection flight
The harvester of environmental information is arranged in the gondola of dirigible.So as to protect collecting device by gondola, and also will can answer
All it is arranged in gondola with the module of the flight environment of vehicle information for collecting, is easy to the biography of flight environment of vehicle information for collecting mutually,
Also as it is wrapped in gondola, effect attractive in appearance is played.
According to the utility model above-described embodiment, harvester includes at least one following：Temperature sensor, humidity sensor
Device, PM2.5 detectors.Harvester is used to detect that air is believed including temperature sensor, humidity sensor, PM2.5 detectors etc.
At least one of equipment of breath equipment.According to the equipment of different detection air informations, the type of its detection is also different, Ke Yishe
The equipment for putting multiple detection air informations, by detecting different air informations, it is ensured that the flight environment of vehicle information accuracy of detection.
According to the utility model above-described embodiment, aircraft also includes data storage transmitting device, is connected with harvester,
For storage environment data, and environmental data is sent to control terminal.The flight environment of vehicle information that harvester is collected, will be logical
Cross data storage transmitting device carries out calculation system to the information, then is stored, and sends to control terminal, makes control end
End is controlled according to the environmental data to the state of flight of aircraft.
Alternatively, data storage transmitting device includes d GPS locating module, wireless communication module, arm processor treatment mould
Block, storage module, for being positioned to aerial detection means, and the signal that individual sensor is exported is amplified, is filtered,
The treatment such as analog-to-digital conversion, numeral isolation and storage.
Alternatively, d GPS locating module, can position to the position of aircraft.Wherein, the content of positioning can include
The original position of aircraft, and flight path.
Alternatively, wireless module, can be 433MHz/915MHz wireless modules.
Alternatively, harvester can send air environment information to earth station by wireless module, the ground station reception
The environmental information that environment monitoring device is sended over, is analyzed, using or in real time display.
Alternatively, harvester can send air environment information to control terminal by wireless module, be control terminal
Aircraft is controlled according to the environmental data.
Alternatively, wireless module, the aircraft original position that d GPS locating module can be positioned, and flight path, hair
Deliver in the reception devices such as control terminal.
Alternatively, the location information that arm processor module can obtain d GPS locating module, and harvester collection
To environmental information carry out calculation system, and the data after treatment sent to control terminal etc. by wireless module receive dress
In putting.
According to the utility model above-described embodiment, data storage transmitting device is arranged in the frame of aircraft, or,
In the case that aircraft is dirigible, data storage transmitting device is arranged in the nacelle of the gondola of dirigible.It is aircraft by frame
Framework material, its intensity is high, and data storage transmitting device is arranged in the frame of aircraft, and it can be made more firm,
It is hardly damaged.In the case where aircraft is dirigible, data storage transmitting device is arranged in the nacelle of the gondola of dirigible, can
In order to carry out information transfer, and data storage transmission dress with the harvester being similarly installed in the nacelle of the gondola of dirigible
Put and also protected by airship gondola, the risk of its loss is reduced, while may also operate as effect attractive in appearance.
According to the utility model above-described embodiment, aircraft also includes：Locator, for the position of positioning aircraft, its
In, position includes the flight original position of aircraft；Processor, is connected with locator, for being not suitable for flight in flight environment of vehicle
During the flight of device, generation protection instruction；Protection device performs protection act under the triggering of protection instruction, wherein, including protection
Action includes：Control aircraft flies to flight original position, drop to after aircraft reaches original position original position and
Power supply is closed after landing in aircraft.Specifically, in the original position and flight course by locator to aircraft
Position is positioned, then the processor by being connected with locator, and the positional information of Aerial vehicle position can be stored, with
And when flight environment of vehicle is not suitable for the flight of aircraft, generation protection instruction.Instructed according to protection, trigger protection device starts,
Aircraft is set to perform protection act.Wherein, protection act can be that control aircraft stable landing is in original position, Yi Ji
Power supply is closed after aircraft landing.And then, when flight environment of vehicle is not suitable for aircraft flight, aircraft can be forced to have drop to
Beginning position, be easy to the recovery of aircraft.
According to the utility model above-described embodiment, locator includes at least one following：GPS positioning unit, remote sensing sensing
Device and light flow sensor.Collector is used for aerial including GPS positioning unit, remote sensor and light flow sensor etc.
At least one equipment that detection means is positioned.According to different location equipments, the mode of its positioning is also different, can set many
Individual location equipment, by different positioning methods, positions, it is ensured that the accuracy of positioning to aerial detection means.
Fig. 2 is a kind of flight system schematic diagram according to the utility model embodiment, as shown in Fig. 2 the flight system bag
Include：Any one aircraft 21 in above-described embodiment；Control terminal 23, and aircraft wireless connection, for controlling aircraft,
And receive the data of aircraft return.Aircraft in above-described embodiment, by being wirelessly connected with control terminal.Control terminal leads to
Transmission wireless signal is crossed, the flight of aircraft is controlled, and by wireless signal, receives the data that aircraft is returned.
According to the utility model above-described embodiment, control terminal includes at least one following：Remote control, mobile terminal, with
And earth station.Control including remote control, mobile terminal and earth station etc. for controlling at least one of the equipment of aircraft
Equipment.Same aircraft is controlled by an equipment or multiple equipment of the control terminal, it is ensured that the control to aircraft, it is to avoid
Control terminal causes the loss of aircraft with the connection failure of aircraft.
Fig. 3 is a kind of optional aircraft schematic diagram according to the utility model embodiment, as shown in figure 3, the aircraft
Including：Frame 1, the support 2 that rises and falls, brushless electric machine 3, propeller 4, electron speed regulator 5, flight control system 6, Digiplex 7,
Wireless receiver 8, lithium battery 9 and harvester 10, the support that rises and falls are fixedly mounted on frame lower end, the brushless electricity
Mechanical, electrical sub- debugger, flight control system, wireless receiver and lithium battery are installed in frame, and propeller is arranged on brushless
On motor, wireless receiver matches with Digiplex, and lithium battery is electrically connected with flight control system, flight control system
It is electrically connected with wireless receiver and electron speed regulator respectively, electron speed regulator is electrically connected with brushless electric machine.And fly at this
The frame lower section of row device is provided with harvester.Harvester includes：The power supply module of lithium battery power supply, Temperature and Humidity mould
Block, PM2.5 detection modules, ARM control modules, the sampling plate are arranged on frame lower section, flight control system and sampling plate electricity
Gas is connected.The controlled system control flight of aircraft, and in flight course, aircraft can be collected by harvester
The information of current flight environment.
Further, data storage transmitting device is also equipped with the frame of aircraft, including：D GPS locating module, wirelessly
Communication module, arm processor processing module, storage module can be positioned to aerial detection means, and to individual sensor
The signal of output is amplified, filters, analog-to-digital conversion, numeral isolation and storage etc. treatment.Data storage transmitting device, with collection
Device is connected, and for storage environment data, and environmental data is sent to control terminal.The flying ring that harvester is collected
Environment information is detected.Wherein, d GPS locating module, can position to the position of aircraft.Wherein, the content of positioning can
With the original position including aircraft, and flight path.Wherein, wireless module, the flight that d GPS locating module can be positioned
Device original position, and flight path, send to the reception devices such as control terminal.Also, wireless module will can also be gathered
The environmental information that device is collected is sent to arm processor.Wherein, arm processor module can obtain d GPS locating module
Location information, and the environmental information that harvester is collected carries out calculation system, and harvester is collected fly
Row environmental information is detected.Its detection process can be that flight environment of vehicle data are compared with environmental data set in advance.
In the case where current flight environmental data does not meet specific environment data, the result of detection is to be not suitable for flight；Current
In the case of flight environment of vehicle data fit specific environment data, the result of detection is suitable flight.It is suitable to be in aircraft
In the state of flight, aircraft normally runs；In aircraft in the state of being not suitable for flying, it is dynamic that aircraft performs protection
Make.Startup is preset in the protection module in arm processor, sends a series of flare maneuvers for controlling aircraft to make protection act and refers to
Order, and the instruction is cut off into control operation of the user to aircraft as being the first preferential operation for performing.So as to current
Flight environment of vehicle is not suitable in the state of aircraft flight, and protection act is made by controlling aircraft, reduces the damage of aircraft
Risk, reduces the loss of aircraft.
Alternatively, the frame of aircraft includes：Upper cover plate, lower shoe and transverse arm, lower shoe are fixedly connected with undercarriage, on
Cover plate, transverse arm, lower shoe be fixedly connected sequentially it is integral, the transverse arm be 4, in cross shape be distributed, four brushless electric machines
It is separately mounted to the end of each bar transverse arm.By the structure design and connected mode, the structure of aircraft, Yi Jiti can be strengthened
Bonding strength between each part high, makes aircraft firmer, so as to reduce the damage risk of aircraft.
According to the utility model above-described embodiment, can be in aircraft when unexpected environmental change is run into, can be to flight
Device is protected.During the use of aircraft, operator's hand-hold wireless remote control goes up to the air to the sky to be detected the present apparatus
Between, aircraft passes earth station's computer back by above-mentioned each device and module, the flight environment of vehicle information that will be collected, be analyzed,
Using and display.Also, by harvester, the environment to the periphery of aircraft carries out real-time monitoring, can be to aircraft
State of flight carry out anticipation in advance and assessment, it is ensured that the safe flight of aircraft, it is to avoid because high altitude environment causes aircraft thing
Therefore.Aircraft interior add said apparatus and system, can aircraft automatically detect environment occur or will dash forward
In the state of change, safeguard measure will be automatically taken, the loss of aircraft is preferably minimized.
Alternatively, before aircraft is started, data are limited the environment that aircraft is set, its environment limitation data can lead to
Cross and obtained over there from aircraft production firm, general manufacturer can all indicate aircraft to allow aircraft to obtain preferably protecting
Storage environment condition and flying condition (for example, it is adapted to -10 DEG C -80 DEG C of flight environment of vehicle temperature, humidity 0% -85%), if exceeded
Those conditions, manufacturer can all advise taking certain safeguard measure, and these all can have mark in aircraft specification.May be used also
With the flight condition parameter obtained by the experience by using person, by being artificially input in Environmental Protection System, limited as environment
Data processed.Start aircraft during the use of aircraft, the d GPS locating module in aircraft is started working, obtain starting
When positional information, origin position etc. that these information contain the coordinate position that obtains by GPS, light flow sensor is obtained
Deng different according to the instrument for obtaining positional information, its information content is also without identical, but purpose is provided to acquisition when taking off
That position, be that safeguard measure below is prepared.During aircraft flight, by sensor, current environment is obtained
Data, wherein the most basic is also it is important that several parameters such as temperature, humidity, air pressure and wind speed, if needing to exist
The aircraft of particular surroundings work, it is also desirable to install corresponding sensor (for example：Remote sensing aircraft is, it is necessary to install remote sensing sensing
Device, to obtain remote sensing signal), it is stored in system after data acquisition, taken out again during judgement.Its judgment mode
It is to be compared with current environment data by starting the preceding environment limitation data for setting, at least one current environmental data not
In the case of meeting environment limitation data, safeguard measure is taken immediately.For example, when we artificially set environment limitation data middle ring
Border humidity data be 0% -80% in the state of, if current environment humidity be 80% or more, judge to damage aircraft
Evil, performs alarm and safeguard measure, protects aircraft.If it is determined that arrive without departing from limitation, then normal vehicle operation, and follow
Ring performs aforesaid operations.Until there is situation of the current environment beyond limitation, then corresponding safeguard measure is taken：It is switched to environment
Protected mode, earth station and remote control cannot be operated to aircraft, and aircraft is set to mesh by by start position information
Cursor position, original position is flown to the speed of unmanned plane maximum throttle, after arriving at location, original position ground is dropped to automatically
On, power supply is then shut off, when preventing from being parked in original position, the short circuit phenomenon for contacting water or other conducting liquids and triggering, with
Aircraft is protected to greatest extent.For example, in the case of the rainfall that happens suddenly, aircraft closes power supply after returning, and can reduce rainwater
Into in aircraft, trigger the risk of short circuit.Performed it is above-mentioned after, operator can outburst surroundings change after, with most
The fast time tidies up aircraft, prevents it by environmental nuisance.Under normal circumstances, Environmental Protection System can only be performed and work as front ring
Border data acquisition and limitation is seen if fall out, there is no any interference to the flight control system of script.
Above-mentioned the utility model embodiment sequence number is for illustration only, and the quality of embodiment is not represented.
In above-described embodiment of the present utility model, the description to each embodiment all emphasizes particularly on different fields, in certain embodiment
Without the part described in detail, the associated description of other embodiment is may refer to.
In several embodiments provided herein, it should be understood that disclosed technology contents, can be by other
Mode is realized.Wherein, device embodiment described above is only schematical, such as division of described unit, Ke Yiwei
A kind of division of logic function, can there is other dividing mode when actually realizing, such as multiple units or component can combine or
Person is desirably integrated into another system, or some features can be ignored, or does not perform.Another, shown or discussed is mutual
Between coupling or direct-coupling or communication connection can be the INDIRECT COUPLING or communication link of unit or module by some interfaces
Connect, can be electrical or other forms.
The unit that is illustrated as separating component can be or may not be it is physically separate, it is aobvious as unit
The part for showing can be or may not be physical location, you can with positioned at a place, or can also be distributed to multiple
On unit.Some or all of unit therein can be according to the actual needs selected to realize the purpose of this embodiment scheme.
In addition, during each functional unit in the utility model each embodiment can be integrated in a processing unit,
Can be that unit is individually physically present, it is also possible to which two or more units are integrated in a unit.It is above-mentioned integrated
Unit can both be realized in the form of hardware, it would however also be possible to employ the form of SFU software functional unit is realized.
The above is only preferred embodiment of the present utility model, it is noted that for the common skill of the art
For art personnel, on the premise of the utility model principle is not departed from, some improvements and modifications can also be made, these improve and
Retouching also should be regarded as protection domain of the present utility model.
Claims (11)
1. a kind of aircraft, it is characterised in that including：
Harvester, the environmental data for gathering aircraft flight environment；
Whether processor, is connected with the harvester, for detecting the suitable institute of flight environment of vehicle based on the environmental data
State the flight of aircraft；
Protection device, is connected with the processor, during for the flight for being not suitable for the aircraft in the flight environment of vehicle, performs
Protection act, to protect the aircraft.
2. aircraft according to claim 1, it is characterised in that the harvester is arranged on sampling plate, described to adopt
Model is arranged on the frame lower section of the aircraft.
3. aircraft according to claim 1, it is characterised in that the aircraft is dirigible, the harvester is set
In the nacelle of gondola, the gondola is arranged on the dirigible.
4. aircraft as claimed in any of claims 1 to 3, it is characterised in that the harvester includes following
At least one：Temperature sensor, humidity sensor, PM2.5 detectors.
5. aircraft as claimed in any of claims 1 to 3, it is characterised in that the harvester includes：Information
Input interface, described information input interface is used to receive the environmental data of meteorological equipment transmission.
6. aircraft according to claim 5, it is characterised in that the meteorological equipment includes at least one following：It is meteorological
Satellite, weather information record terminal and air detecting device,
Wherein, the weather information record terminal is used to record the environmental data in the aircraft flight location；Air detection
Device is set on board the aircraft or on building, and the distance of building and aircraft is without departing from preset distance.
7. aircraft according to claim 1, it is characterised in that the aircraft also includes data storage transmitting device,
It is connected with the harvester, for storing the environmental data, and the environmental data is sent to control terminal.
8. aircraft according to claim 7, it is characterised in that the data storage transmitting device is arranged on the flight
In the frame of device, or, in the case where the aircraft is dirigible, the data storage transmitting device is arranged on the dirigible
Gondola nacelle in.
9. aircraft according to claim 1, it is characterised in that the aircraft also includes：
Locator, the position for positioning the aircraft, wherein, the position includes the flight start bit of the aircraft
Put；
The processor, is connected with the locator, raw during for the flight for being not suitable for the aircraft in the flight environment of vehicle
Instructed into protection；
The protection device performs the protection act under the triggering of the protection instruction.
10. a kind of flight system, it is characterised in that including：
Aircraft in claim 1 to 9 described in any one；
Control terminal, with the aircraft wireless connection, for controlling the aircraft, and receives the number that the aircraft is returned
According to.
11. flight systems according to claim 10, it is characterised in that the control terminal includes at least one following：
Remote control, mobile terminal and earth station.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621313416.XU CN206218244U (en) | 2016-12-01 | 2016-12-01 | Aircraft and flight system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621313416.XU CN206218244U (en) | 2016-12-01 | 2016-12-01 | Aircraft and flight system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206218244U true CN206218244U (en) | 2017-06-06 |
Family
ID=58784349
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621313416.XU Active CN206218244U (en) | 2016-12-01 | 2016-12-01 | Aircraft and flight system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206218244U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107329491A (en) * | 2017-08-16 | 2017-11-07 | 广东容祺智能科技有限公司 | A kind of unmanned plane high/low temperature protects system and method |
| CN108492531A (en) * | 2018-03-21 | 2018-09-04 | 遵义师范学院 | A kind of disaster early warning system and installation method based on wireless sensor network |
| CN112068601A (en) * | 2020-10-20 | 2020-12-11 | 北京卫通新科测控技术有限公司 | Navigation control system for fixed-wing unmanned aerial vehicle |
| CN115132020A (en) * | 2022-07-26 | 2022-09-30 | 中国人民解放军海军航空大学 | Freely settable system for aircraft training |
-
2016
- 2016-12-01 CN CN201621313416.XU patent/CN206218244U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107329491A (en) * | 2017-08-16 | 2017-11-07 | 广东容祺智能科技有限公司 | A kind of unmanned plane high/low temperature protects system and method |
| CN108492531A (en) * | 2018-03-21 | 2018-09-04 | 遵义师范学院 | A kind of disaster early warning system and installation method based on wireless sensor network |
| CN108492531B (en) * | 2018-03-21 | 2019-09-06 | 遵义师范学院 | A kind of disaster early warning system and installation method based on wireless sensor network |
| CN112068601A (en) * | 2020-10-20 | 2020-12-11 | 北京卫通新科测控技术有限公司 | Navigation control system for fixed-wing unmanned aerial vehicle |
| CN115132020A (en) * | 2022-07-26 | 2022-09-30 | 中国人民解放军海军航空大学 | Freely settable system for aircraft training |
| CN115132020B (en) * | 2022-07-26 | 2023-10-31 | 中国人民解放军海军航空大学 | System capable of being freely set for training aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206218244U (en) | Aircraft and flight system | |
| CN206171828U (en) | Unmanned aerial vehicle safety arrangement that falls | |
| Polo et al. | Design of a low-cost Wireless Sensor Network with UAV mobile node for agricultural applications | |
| CN104820429B (en) | Ultrasonic distance detection-based unmanned aerial vehicle obstacle avoidance system and control method thereof | |
| JP6968911B2 (en) | Information processing equipment and information processing method | |
| CN103078673B (en) | A kind of dedicated unmanned Helicopter System being applicable to mountain area electrical network and patrolling and examining | |
| CN203876988U (en) | Protection and control system of aircraft and aircraft | |
| CN202533754U (en) | Ground monitoring system for unmanned vehicle physical simulated test platform | |
| CN106909169A (en) | A kind of full automatic power patrol UAV system | |
| CN207133659U (en) | A kind of unmanned vehicle tele-control system | |
| CN106919184A (en) | Double unmanned plane coordinated operation systems and double unmanned plane work compound methods | |
| CN203219298U (en) | Unmanned helicopter system special for inspecting electric grid in mountain area | |
| CN107992029A (en) | Unmanned plane device for detecting performance based on status monitoring | |
| CN105334861A (en) | Unmanned plane flight control module, unmanned plane flight control system and unmanned plane | |
| CN107917988A (en) | A kind of toxic and harmful gas detecting system and method based on multi-rotor unmanned aerial vehicle | |
| CN104881042A (en) | Multi-dimension aviation remote sensing test platform | |
| CN205581576U (en) | Unmanned aerial vehicle farmland soil information monitoring system | |
| CN103558653A (en) | Weather detection airplane based on platform with multiple rotor wings | |
| CN107590878A (en) | A kind of unmanned plane during flying safe prediction apparatus for evaluating and method | |
| CN110832195A (en) | Monitoring system for wind farms and related method | |
| CN104316901B (en) | For the aerial intelligent robot of radio monitoring | |
| CN107069859A (en) | A kind of wireless charging system and method based on unmanned plane base station | |
| CN106741899A (en) | Kite aircraft and its implementation | |
| CN209103156U (en) | A kind of emergency parachuting of unmanned plane and impact location system, MILS | |
| CN109696920B (en) | Work device, and control method and device thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |