CN205638734U - A survey and drawing unmanned aerial vehicle for highlands - Google Patents
A survey and drawing unmanned aerial vehicle for highlands Download PDFInfo
- Publication number
- CN205638734U CN205638734U CN201620521069.3U CN201620521069U CN205638734U CN 205638734 U CN205638734 U CN 205638734U CN 201620521069 U CN201620521069 U CN 201620521069U CN 205638734 U CN205638734 U CN 205638734U
- Authority
- CN
- China
- Prior art keywords
- carburetor
- air inlet
- highlands
- controller
- temperature
- 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.)
- Expired - Fee Related
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Road Paving Machines (AREA)
Abstract
The utility model relates to a survey and drawing unmanned aerial vehicle for highlands belongs to the unmanned aerial vehicle field. The utility model aims to provide an unmanned aerial vehicle who is used for highlands survey and drawing that can adapt to the temperature on plateau. Including the organism, set up in the engine of organism, the outer camera that carrys by the organism that is located the organism, connect the carburetor on the engine, the carburetor is linked together with the engine, is equipped with the air inlet on the carburetor, is equipped with the blast pipe on the engine, including pipe, temperature sensor and controller, pipe one end and waste pipe intercommunication, the other end is close to the air inlet of carburetor, temperature sensor installs in the air inlet of carburetor, the controller is installed in the organism, be equipped with control flap on the pipe, temperature sensor is connected with the controller communication, the controller is connected with the control flap electricity. The temperature of the air inlet department of this a survey and drawing unmanned aerial vehicle for highlands ability automatically regulated carburetor makes its highlands in that the difference in temperature is big normally work.
Description
Technical field
This utility model belongs to unmanned plane field, particularly a kind of mapping unmanned plane.
Background technology
High altitude localities, the temperature difference is big, and maximum temperature reaches, and minimum temperature is the most subzero；MAV is due to lightweight, body
Long-pending little, length in cruising time, low cost and flexible operation etc. are widely used in low latitude photogrammetry.Highlands, owing to environment is disliked
Bad, unmanned plane mapping substitutes artificial mapping, it is to avoid mapping worker relates to body high-risk environment, gets a good review.But, highlands,
Height above sea level, the temperature difference are big.Unmanned plane, during flight mapping, can experience different temperature, at low ambient temperatures unmanned plane
The air inlet of oil device easily freezes, and causes engine speed to reduce, the most flame-out, affects the normal of unmanned plane and works, therefore,
Need to heat up at air inlet, prevent from freezing；But, when ambient temperature is too high, if continuing air inlet is heated up, meeting
Accelerate the aging of carburetor.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of mapping unmanned plane for highlands, and it adapts to plateau
Temperature, normally work under the different temperatures on plateau.
The technical solution adopted in the utility model is: a kind of mapping unmanned plane for highlands, including body, is arranged at machine
The electromotor of body, be positioned at the outer video camera delivered by body of body, the carburetor being connected on electromotor, described carburetor with send out
Motivation is connected, and carburetor is provided with air inlet, and electromotor is provided with exhaustor；Including conduit, temperature sensor and controller,
Described tube at one end connects with waste pipe, and the other end is near the air inlet of carburetor；Described temperature sensor is installed on
The air inlet of carburetor；Described controller is installed on body；Conduit is provided with control valve；Described temperature sensor and control
Device communication connects, and described controller electrically connects with controlling valve.
Further, described conduit is flexible pipe.
Further, carburetor is provided with and buckles, described in buckle and be positioned at air inlet side；Described conduit entering near carburetor
One end of QI KOU is provided with hook, described hook with buckle suitable.
The beneficial effects of the utility model are: a kind of mapping unmanned plane for highlands, gather carburetion by temperature sensor
The temperature of the air inlet of device is transferred to controller, and the closedown of the temperature control valve that controller gathers according to temperature sensor is opened,
Conduit is selected whether to turn on.This kind of unmanned function of surveying and drawing for highlands is automatically adjusted the temperature at the air inlet of carburetor,
It is made can normally to work in the highlands that the temperature difference is big.
Accompanying drawing explanation
Fig. 1 is this utility model schematic diagram.
In figure, electromotor 1, carburetor 2, air inlet 3, exhaustor 4, conduit 5, temperature sensor 6, controller 7, control
Valve 8 processed, buckle 9, hook 10.
Detailed description of the invention
With embodiment, this utility model is described further below in conjunction with the accompanying drawings.
A kind of mapping unmanned plane for highlands, as it is shown in figure 1, include body, be arranged at the electromotor 1 of body, position
In the outer video camera delivered by body of body, the carburetor 2 being connected on electromotor 1, described carburetor 2 and electromotor 1 phase
Connection, carburetor 2 is provided with air inlet 3, and electromotor 1 is provided with exhaustor 4；Including conduit 5, temperature sensor 6 and control
Device 7 processed, described conduit 5 one end connects with the exhaustor 4 of electromotor 1, and the other end is near the air inlet 3 of carburetor 2；Described
Temperature sensor 6 is installed on the air inlet 3 of carburetor 2；Described controller 7 is installed on body；Conduit 5 is provided with control
Valve 8；Described temperature sensor 6 is connected with controller 7 communication, and described controller 7 electrically connects with controlling valve 8.
A kind of mapping unmanned plane for highlands, the temperature of the air inlet 3 being gathered carburetor 2 by temperature sensor 6 is passed
Being defeated by controller 7, controller 7 controls the cut out of valve 8 and opens, thus selects conduit 5 whether to turn on.Temperature sensor 6
When air inlet 3 temperature of the carburetor 2 collected is less than design temperature, controller 7 controls valve 8 and opens, electromotor 1
Tail gas is transported to the air inlet 3 of carburetor 2 by conduit 5, heats at air inlet 3, prevents the air inlet 3 of carburetor 2
Freeze.When air inlet 3 temperature of the carburetor 2 that temperature sensor 6 collects is higher than design temperature, controller 7 control valve
Door 8 is closed, and stops the tail gas of electromotor 1 to be transported to the air inlet 3 of carburetor 2 by conduit 5, stops to air inlet 3
Heating, the temperature preventing air inlet 3 is too high.Design temperature is configured according to actual needs, for the air inlet 3 of carburetor 2
The critical point that place freezes.This kind of unmanned function of surveying and drawing for highlands is automatically adjusted the temperature at the air inlet 3 of carburetor 2
Degree so that it is the highlands big in the temperature difference can normally work.
Preferably, described conduit 5 is flexible pipe.Flexible pipe is lightweight, it is simple to bending.
Preferably, carburetor 2 is provided with and buckles 9, described in buckle 9 and be positioned at air inlet 3 side；Described conduit 5 closeization
One end of air inlet 3 of oil device 2 is provided with hook 10, and described hook 10 is with to buckle 9 suitable.By hook 10 with buckle 9
Mounting, it is simple to the air inlet 3 of conduit 5 centering carburetor 2, and mounting is convenient.
Claims (3)
1., for the mapping unmanned plane of highlands, the electromotor (1) including body, being arranged at body, it is positioned at outside body
The video camera delivered by body, the carburetor (2) being connected on electromotor (1), described carburetor (2) and electromotor (1)
Being connected, carburetor (2) is provided with air inlet (3), and electromotor (1) is provided with exhaustor (4)；It is characterized in that: bag
Include the exhaustor (4) of conduit (5), temperature sensor (6) and controller (7), described conduit (5) one end and electromotor (1)
Connection, the other end is near the air inlet (3) of carburetor (2)；Described temperature sensor (6) is installed on entering of carburetor (2)
QI KOU (3)；Described controller (7) is installed on body；Conduit (5) is provided with control valve (8)；Described temperature sensing
Device (6) is connected with controller (7) communication, and described controller (7) electrically connects with controlling valve (8).
A kind of mapping unmanned plane for highlands, it is characterised in that: described conduit (5)
For flexible pipe.
A kind of mapping unmanned plane for highlands, it is characterised in that: in carburetor (2)
Be provided with and buckle (9), described in buckle (9) and be positioned at air inlet (3) side；Described conduit (5) is near carburetor (2)
One end of air inlet (3) is provided with hook (10), and described hook (10) is with to buckle (9) suitable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620521069.3U CN205638734U (en) | 2016-05-31 | 2016-05-31 | A survey and drawing unmanned aerial vehicle for highlands |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620521069.3U CN205638734U (en) | 2016-05-31 | 2016-05-31 | A survey and drawing unmanned aerial vehicle for highlands |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205638734U true CN205638734U (en) | 2016-10-12 |
Family
ID=57051208
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620521069.3U Expired - Fee Related CN205638734U (en) | 2016-05-31 | 2016-05-31 | A survey and drawing unmanned aerial vehicle for highlands |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205638734U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105840360A (en) * | 2016-05-31 | 2016-08-10 | 四川鸿鑫空间测绘有限公司 | Surveying and mapping unmanned aerial vehicle for plateau region |
-
2016
- 2016-05-31 CN CN201620521069.3U patent/CN205638734U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105840360A (en) * | 2016-05-31 | 2016-08-10 | 四川鸿鑫空间测绘有限公司 | Surveying and mapping unmanned aerial vehicle for plateau region |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9328650B2 (en) | Engine cooling system | |
| CN108306079B (en) | Unmanned aerial vehicle battery heat preservation device and heat preservation method | |
| CN105270134B (en) | System and method for controlling the air-flow in vehicle | |
| CN109538384B (en) | Air intake system and vehicle | |
| EP2868579B1 (en) | Aircraft air conditioning system and method of operating an aircraft air conditioning system | |
| CN205277471U (en) | High and cold construction ventilation of tunnel system in plateau | |
| CN205638734U (en) | A survey and drawing unmanned aerial vehicle for highlands | |
| CN105840360A (en) | Surveying and mapping unmanned aerial vehicle for plateau region | |
| SE1300194A1 (en) | Air conditioning for aircraft | |
| CN107745828A (en) | A kind of anti-deicing experiment air entraining device of hot gas | |
| US20150040577A1 (en) | System and method for preventing ice crystal accretion in gas turbine engines | |
| CN104329171B (en) | Aircraft and electromotor thereof | |
| CN110685793A (en) | Intercooling bypass device, diesel engine air intake system, control method and vehicle | |
| CN203996904U (en) | A kind of bourdon's tube structure of the angle adjustable for hot air anti-icing | |
| CN202954873U (en) | Urea box used for diesel engine tail gas post-processing silicon controlled rectifier (SCR) system | |
| CN105863845B (en) | Icing instruction system | |
| US10883466B2 (en) | High altitude air start equipment for aircraft reciprocating engine | |
| RU140978U1 (en) | ANTI-ICE SYSTEM OF UNMANNED AIRCRAFT | |
| EP3248823A1 (en) | Motor-vehicle powertrain unit with a system for cooling a clutch device | |
| CN114658574A (en) | Engine air inlet system, control method thereof and vehicle | |
| CN205981615U (en) | Realize set out supporting mechanism of match test of small -size advancing device in intermittent wind tunnel | |
| CN211692670U (en) | Intake manifold icing prevention system, engine and automobile | |
| CN209208893U (en) | A kind of all-terrain vehicle CVT button for rubber strap thermal | |
| CN111017198B (en) | Nacelle for high-altitude flight aircraft wing mixed laminar flow control | |
| CN207847819U (en) | Punching type vehicular engine gas handling system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161012 Termination date: 20170531 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |