CN207809782U - A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device - Google Patents
A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device Download PDFInfo
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- CN207809782U CN207809782U CN201721830687.7U CN201721830687U CN207809782U CN 207809782 U CN207809782 U CN 207809782U CN 201721830687 U CN201721830687 U CN 201721830687U CN 207809782 U CN207809782 U CN 207809782U
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- aerial vehicle
- unmanned aerial
- instrumentation device
- formula protection
- vehicle ejecting
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Abstract
A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device of the utility model, includes the body of unmanned plane, it is characterised in that：The body upper is provided with instrument container, and the instrument upper box part is provided with parachute, and lower part is provided with air bag；It is provided with separator between the instrument container and body, guard screen is provided between the separator and instrument container.The utility model can allow detection instrument safe landing after unmanned plane is out of control, protect the safety of detection instrument.
Description
Technical field
The utility model belongs to meteorological unmanned plane field more particularly to a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device.
Background technology
Meteorological unmanned plane is mainly used for long-range weather monitoring and scouts purpose, is to aim at ocean, outlying district, region of war and not
Meteorological and environment is scouted and is developed under sharp weather condition.Originally, meteorological unmanned plane is mostly converted by general unmanned machine.
With the continuous development of the technologies such as computer, microelectronics, communication, information, material, recent domestic also develop dedicated for
The meteorological unmanned plane that meteorological and environment is scouted.Meteorological unmanned plane has the characteristics that economical, motor-driven, flexible, and use scope is wide, can be right
Tropical cyclone and other hazardous weathers carry out systemic monitoring.
Unmanned plane meteorological detection system is made of aircraft system, payload, ground installation.Aircraft system includes aircraft
Platform, propulsion system, navigation system, flight control system, take off/landing system airborne portion, data link airborne portion etc..
Take off/airborne portion of landing system coordinates with above ground portion, complete the transmitting and recycling of unmanned plane.Propulsion system provides nobody
The power of machine.Navigation system can be guided by satellite navigation, early warning plane, ground guides and the target detection of unmanned plane itself
Tactical mission is completed for UAV system navigation and the guarantee of target information are provided with ability of tracking.Flight control system is for nobody
The core of part on machine machine, it monitors, controls and command other On-Board Subsystems, receives the instruction that earth station sends out, and coordinates machine
The work of each subsystem is carried, and the state of unmanned plane and other desired information are sent to earth station by data link,
Under the monitoring and commander of earth station, control unmanned plane completes preplanned mission.
Payload includes the meteorologic parameters measuring apparatus such as temperature, humidity, air pressure, wind speed, wind direction, particulate matter, completes to fly
The meteorologic parameter in row region measures.
Ground installation includes ground-support equipment, ground monitoring subsystem, take off/landing system above ground portion, data-link
Road floor portion is graded.Take off/above ground portion of landing system is the important guarantee for completing unmanned plane transmitting, recycling.Data link
Above ground portion and airborne portion cooperate, the communication of earth station and unmanned plane is provided, the monitoring to unmanned plane is realized, refers to
It waves, completes scheduled combat duty.The monitoring of ground monitoring subsystem controls and other subsystems is commanded to work, and is carried to operator
For comprehensive environmental information and drone status information, subsystems are arranged to complete scheduled according to the order of operator
Business.Rational reaction is made to the event of burst, and is notified to operator in time.
Meteorological unmanned plane is as a kind of new and effective Atmospheric Survey type machinery, when carrying detection instrument, safeguard measure
It is simple and crude, and meteorological detection instrument price is expensive, falls once unmanned plane is out of control, detection instrument is caused to damage, and will bring a large amount of
Economic loss, and delay detection affairs.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of unmanned aerial vehicle ejecting for the deficiency of background technology
Formula protection of instrumentation device, can allow detection instrument safe landing after unmanned plane is out of control, protect the safety of detection instrument.
The utility model uses following technical scheme to solve above-mentioned technical problem：
A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device, includes the body of unmanned plane, and the body upper is provided with instrument
Case, the instrument upper box part are provided with parachute, and lower part is provided with air bag；It is provided between the instrument container and body point
From device, guard screen is provided between the separator and instrument container.
Further, it is provided with PLC controller in the instrument container, obliquity sensor is connected in PLC controller.
Further, the separator includes seal box, and propellant is filled in the seal box, is set on the propellant
It is equipped with electronic lighter, electronic lighter and PLC controller electrical connection.
Further, the limit bolt of several Contraband types, the both ends difference of the limit bolt are provided with outside the seal box
With seal box and instrument container grafting.
Further, it is provided with radome fairing outside the body.
Further, radome fairing top is arc.
Further, the radome fairing top is provided with opening, the opening and instrument container side wall snug fit.
Further, bracket is provided with by holder above the instrument container.
Further, the material of the holder and bracket is carbon fiber.
Further, ultrasonic sensor and stroboscopic lamp, buzzer are connected in the PLC controller.
The utility model has the following technical effects using above technical scheme is compared with the prior art：
1, electronic lighter is allowed to light propellant by way of remote control or condition triggering, to pop up instrument container, so
The safety of detection instrument is protected in landing safe with the help of parachute afterwards；
2, when ultrasonic sensor is detected according to ground 3m, the air bag of bottom is opened.Carry out buffering of contacting to earth.And it is directed to
The case where drop in water surface, can be such that babinet floats on the water surface.After landing, buzzer and stroboscopic lamp are opened, and are carried to reseaching staff
For message；
3, radome fairing is provided with outside body, radome fairing top is arc, is used for smooth air so that unmanned plane during flying is more
Steadily, the effect of dust from land surface and waterproof when preventing from taking off is also functioned to；
4, holder is provided above instrument container and be provided with bracket, for placing some open instruments.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present embodiment；
Fig. 2 is the enlarged drawing at A in Fig. 1.
1, body；2, instrument container；21, parachute；22, air bag；3, separator；31, seal box；32, propellant；
33, limit bolt；34, guard screen；4, radome fairing；41, it is open；5, bracket；51, holder；6, battery supporting plate.
Specific implementation mode
The technical solution of the utility model is described in further detail below in conjunction with the accompanying drawings：
A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device includes the body 1 of unmanned plane, the body 1 as illustrated in fig. 1 and 2
Top is provided with instrument container 2, and 2 top of the instrument container is provided with parachute 21, and lower part is provided with air bag 22；The instrument
Separator 3 is provided between case 2 and body 1.
It is provided with PLC controller in instrument container 2, raspberry pi controllers can be selected, the PLC controller is with wireless
Remote controler is connected with obliquity sensor in PLC controller.Ultrasonic sensor and stroboscopic lamp, buzzing are connected in PLC controller
Device.
Separator 3 includes seal box 31, is filled with propellant 32 in seal box 31, which can be selected unmanned aircraft parachute descent
System propellant.Electronic lighter, electronic lighter and PLC controller electrical connection are provided on the propellant 32.Seal box
The limit bolt 33 of several Contraband types is provided with outside 31, the both ends of the limit bolt 33 are inserted with seal box 31 and instrument container 2 respectively
It connects.Guard screen 34 is provided between separator 3 and instrument container 2, guard screen 34 can avoid the burning of propellant 32 to instrument
Damage caused by case 2.
Radome fairing 4 is provided with outside body 1,4 top of radome fairing is arc, is used for smooth air so that unmanned plane during flying is more
Add steadily, also functions to the effect of dust from land surface and waterproof when preventing from taking off.4 top of radome fairing is provided with opening 41, the opening
41 and 2 side wall snug fit of instrument container.2 top of instrument container is provided with bracket 5 by holder 51, open for placing some
Instrument.The material of holder 51 and bracket 5 is carbon fiber, can mitigate whole weight.The lower section of body 1 is additionally provided with battery
Supporting plate 6, for storing battery.
Explanation is embodied：
When aircraft encountered during flight high wind or it is out of control so that body 1 inclination angle be more than 70 degree after, inclination angle sense
This signal is transferred to PLC controller by device, and PLC controller automatic decision unmanned plane is out of control, and control electronic lighter igniting is lighted
Propellant 32, generates a large amount of gas, and bulk gas generates high pressure, and limit bolt 33 is popped up seal box 31, while by instrument
Case 2 pops up so that instrument container 2 is far from unmanned plane.Parachute 21 carries parachute opening device, can according to highly automated parachute-opening,
To allow instrument container 2 to land safely.Certainly, electronic lighter can also remote control trigger.When unmanned plane is out of control, pass through remote controler
Instruction directly is sent out to PLC controller, electronic lighter is allowed to light a fire.
When ultrasonic sensor is detected according to ground 3m, the air bag 22 of bottom is opened.Carry out buffering of contacting to earth.And it is directed to
The case where drop in water surface, can be such that babinet floats on the water surface.After landing, buzzer and stroboscopic lamp are opened, and are carried to reseaching staff
For message.
Those skilled in the art of the present technique are it is understood that unless otherwise defined, all terms used herein（Including skill
Art term and scientific terminology）With meaning identical with the general understanding of the those of ordinary skill in the utility model fields
Justice.It should also be understood that those terms such as defined in the general dictionary should be understood that with upper with the prior art
The consistent meaning of meaning hereinafter, and unless defined as here, will not with the meaning of idealization or too formal come
It explains.
Above example is only to illustrate the technological thought of the utility model, and the protection model of the utility model cannot be limited with this
Enclose, it is every according to the utility model proposes technological thought, any change done on the basis of technical solution each falls within this reality
Within the scope of novel protected.The embodiment of the utility model is explained in detail above, but the utility model is not
It is limited to the above embodiment, within the knowledge of a person skilled in the art, can also be or else detached from this practicality
It is made a variety of changes under the premise of novel objective.
Claims (10)
1. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device, includes the body of unmanned plane, it is characterised in that：The body upper is set
It is equipped with instrument container, the instrument upper box part is provided with parachute, and lower part is provided with air bag；Between the instrument container and body
It is provided with separator, guard screen is provided between the separator and instrument container.
2. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 1, it is characterised in that：In the instrument container
It is provided with PLC controller, obliquity sensor is connected in PLC controller.
3. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 1, it is characterised in that：The separator packet
Include seal box, propellant be filled in the seal box, be provided with electronic lighter on the propellant, electronic lighter and
PLC controller is electrically connected.
4. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 3, it is characterised in that：Outside the seal box
Be provided with the limit bolt of several Contraband types, the both ends of the limit bolt respectively with seal box and instrument container grafting.
5. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 1, it is characterised in that：The body peripheral hardware
It is equipped with radome fairing.
6. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 5, it is characterised in that：Radome fairing top is
Arc.
7. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 5, it is characterised in that：On the radome fairing
Portion is provided with opening, the opening and instrument container side wall snug fit.
8. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 1, it is characterised in that：On the instrument container
Side is provided with bracket by holder.
9. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 8, it is characterised in that：The holder and support
The material of frame is carbon fiber.
10. a kind of unmanned aerial vehicle ejecting formula protection of instrumentation device according to claim 2, it is characterised in that：The PLC controls
Ultrasonic sensor and stroboscopic lamp, buzzer are connected on device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721830687.7U CN207809782U (en) | 2017-12-22 | 2017-12-22 | A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721830687.7U CN207809782U (en) | 2017-12-22 | 2017-12-22 | A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device |
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| Publication Number | Publication Date |
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| CN207809782U true CN207809782U (en) | 2018-09-04 |
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| CN201721830687.7U Active CN207809782U (en) | 2017-12-22 | 2017-12-22 | A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163197A (en) * | 2017-12-22 | 2018-06-15 | 南京俊全科技有限公司 | A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device and method |
-
2017
- 2017-12-22 CN CN201721830687.7U patent/CN207809782U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163197A (en) * | 2017-12-22 | 2018-06-15 | 南京俊全科技有限公司 | A kind of unmanned aerial vehicle ejecting formula protection of instrumentation device and method |
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