CN105840360A - Surveying and mapping unmanned aerial vehicle for plateau region - Google Patents

Surveying and mapping unmanned aerial vehicle for plateau region Download PDF

Info

Publication number
CN105840360A
CN105840360A CN201610380587.2A CN201610380587A CN105840360A CN 105840360 A CN105840360 A CN 105840360A CN 201610380587 A CN201610380587 A CN 201610380587A CN 105840360 A CN105840360 A CN 105840360A
Authority
CN
China
Prior art keywords
carburetor
air inlet
controller
unmanned aerial
surveying
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
Application number
CN201610380587.2A
Other languages
Chinese (zh)
Inventor
段亚会
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sichuan Hongxin Space Plotting Co Ltd
Original Assignee
Sichuan Hongxin Space Plotting Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sichuan Hongxin Space Plotting Co Ltd filed Critical Sichuan Hongxin Space Plotting Co Ltd
Priority to CN201610380587.2A priority Critical patent/CN105840360A/en
Publication of CN105840360A publication Critical patent/CN105840360A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M31/00Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
    • F02M31/02Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating
    • F02M31/04Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture
    • F02M31/06Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture by hot gases, e.g. by mixing cold and hot air
    • F02M31/08Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture by hot gases, e.g. by mixing cold and hot air the gases being exhaust gases
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N5/00Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy
    • F01N5/02Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy the devices using heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Road Paving Machines (AREA)

Abstract

The invention discloses a surveying and mapping unmanned aerial vehicle for a plateau region, belongs to the field of unmanned aerial vehicles, and aims at providing an unmanned aerial vehicle suitable for the temperature of the plateau and used for surveying and mapping of the plateau region. The surveying and mapping unmanned aerial vehicle comprises a vehicle body, an engine arranged on the vehicle body, a camera located outside the vehicle body and conveyed by the vehicle body and a carburetor connected to the engine; the carburetor is communicated with the engine, an air inlet is formed in the carburetor, and an air exhausting pipe is arranged on the engine; the surveying and mapping unmanned aerial vehicle further comprises a guide pipe, a temperature sensor and a controller; one end of the guide pipe is communicated with the air exhausting pipe of the engine, and the other end of the guide pipe is close to an air inlet of the carburetor; the temperature sensor is mounted on the air inlet of the carburetor; the controller is mounted on the vehicle body; a control valve is arranged on the guide pipe; and the temperature sensor is in communication connection with the controller, and the controller is electrically connected with the control valve. The surveying and mapping unmanned aerial vehicle for the plateau region can automatically adjust the temperature of the air inlet of the carburetor and can normally work on the plateau region with the large temperature difference.

Description

A kind of mapping unmanned plane for highlands
Technical field
The invention 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.
Summary of the invention
The technical problem to be solved is to provide a kind of mapping unmanned plane for highlands, and it adapts to the temperature on plateau Degree, normally works under the different temperatures on plateau.
The technical solution used in the present invention is: a kind of mapping unmanned plane for highlands, including body, is arranged at body Electromotor, it is positioned at the outer video camera delivered by body of body, the carburetor being connected on electromotor, described carburetor and electromotor Being connected, carburetor is provided with air inlet, and electromotor is provided with exhaustor;Including conduit, temperature sensor and controller, institute Stating tube at one end to connect with waste pipe, the other end is near the air inlet of carburetor;Described being installed on of temperature sensor The air inlet of oil device;Described controller is installed on body;Conduit is provided with control valve;Described temperature sensor and controller 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 invention has the beneficial effects as follows: a kind of mapping unmanned plane for highlands, gather carburetor by temperature sensor The temperature of air inlet is transferred to controller, and the closedown of the temperature control valve that controller gathers according to temperature sensor is opened, and selects Whether conduit turns on.This kind of unmanned function of surveying and drawing for highlands is automatically adjusted the temperature at the air inlet of carburetor, makes It can normally work in the highlands that the temperature difference is big.
Accompanying drawing explanation
Fig. 1 is schematic diagram of the present invention.
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
The present invention is described further with embodiment 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.
CN201610380587.2A 2016-05-31 2016-05-31 Surveying and mapping unmanned aerial vehicle for plateau region Pending CN105840360A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610380587.2A CN105840360A (en) 2016-05-31 2016-05-31 Surveying and mapping unmanned aerial vehicle for plateau region

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610380587.2A CN105840360A (en) 2016-05-31 2016-05-31 Surveying and mapping unmanned aerial vehicle for plateau region

Publications (1)

Publication Number Publication Date
CN105840360A true CN105840360A (en) 2016-08-10

Family

ID=56595465

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610380587.2A Pending CN105840360A (en) 2016-05-31 2016-05-31 Surveying and mapping unmanned aerial vehicle for plateau region

Country Status (1)

Country Link
CN (1) CN105840360A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110594046A (en) * 2019-09-19 2019-12-20 浙江瑞星化油器制造有限公司 Electric control carburetor for unmanned aerial vehicle
CN110594045A (en) * 2019-09-19 2019-12-20 浙江瑞星化油器制造有限公司 Control method for fuel injection quantity of carburetor for unmanned aerial vehicle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4005693A (en) * 1973-01-29 1977-02-01 Nissan Motor Co., Ltd. Warming-up system for internal combustion engines
CN1242472A (en) * 1998-07-17 2000-01-26 成汝峰 Gasoline vaporization jet type carburetor
JP2007127095A (en) * 2005-11-07 2007-05-24 Nikki Co Ltd Icing preventing device for carburetor
CN103912418A (en) * 2014-04-24 2014-07-09 四川测绘地理信息局测绘技术服务中心 Extended-range unmanned aerial vehicle with novel air cleaner
CN103925118A (en) * 2014-04-24 2014-07-16 四川测绘地理信息局测绘技术服务中心 Unmanned aerial vehicle suitable for emergency surveying and mapping protection in plateau area
CN205638734U (en) * 2016-05-31 2016-10-12 四川鸿鑫空间测绘有限公司 A survey and drawing unmanned aerial vehicle for highlands

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4005693A (en) * 1973-01-29 1977-02-01 Nissan Motor Co., Ltd. Warming-up system for internal combustion engines
CN1242472A (en) * 1998-07-17 2000-01-26 成汝峰 Gasoline vaporization jet type carburetor
JP2007127095A (en) * 2005-11-07 2007-05-24 Nikki Co Ltd Icing preventing device for carburetor
CN103912418A (en) * 2014-04-24 2014-07-09 四川测绘地理信息局测绘技术服务中心 Extended-range unmanned aerial vehicle with novel air cleaner
CN103925118A (en) * 2014-04-24 2014-07-16 四川测绘地理信息局测绘技术服务中心 Unmanned aerial vehicle suitable for emergency surveying and mapping protection in plateau area
CN205638734U (en) * 2016-05-31 2016-10-12 四川鸿鑫空间测绘有限公司 A survey and drawing unmanned aerial vehicle for highlands

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110594046A (en) * 2019-09-19 2019-12-20 浙江瑞星化油器制造有限公司 Electric control carburetor for unmanned aerial vehicle
CN110594045A (en) * 2019-09-19 2019-12-20 浙江瑞星化油器制造有限公司 Control method for fuel injection quantity of carburetor for unmanned aerial vehicle

Similar Documents

Publication Publication Date Title
US10457399B2 (en) Aircraft air conditioning system and method of operating an aircraft air conditioning system
US10633098B2 (en) Environmental control system
EP2868579B1 (en) Aircraft air conditioning system and method of operating an aircraft air conditioning system
GB2512442A8 (en) Regulated oil cooling system for a turbine engine with deicing of the nacelle
EP2250090B1 (en) Icing protection for aircraft air inlet scoops
EP2909086B1 (en) Aircraft fuel system with fuel return from engine
CN105775134B (en) A kind of environmental protection sampling aircraft
EP3127813A1 (en) Electric compressor for use with a wing anti-ice system
CN105840360A (en) Surveying and mapping unmanned aerial vehicle for plateau region
CN109538384B (en) Air intake system and vehicle
EP2697119B1 (en) System for delivering pre-conditioned air to an aircraft on the ground
CN205277471U (en) High and cold construction ventilation of tunnel system in plateau
CN104129504A (en) Flute-shaped tube structure with adjustable angle for hot air anti-icing
CN205638734U (en) A survey and drawing unmanned aerial vehicle for highlands
EP3335993B1 (en) Aircraft nacelle anti-ice systems and methods
CN107745828A (en) A kind of anti-deicing experiment air entraining device of hot gas
FR3005440A1 (en) SELF-COOLING LOOP WITH DYNAMIC ELECTRIC VENTILATOR FOR MOTOR COMPRESSOR.
KR101685853B1 (en) Dual fuel internal combustion engine impelling apparatus
CN203996904U (en) A kind of bourdon's tube structure of the angle adjustable for hot air anti-icing
CN110803277A (en) Variable pitch propeller control system
CN113044224A (en) Aircraft anti-icing method and system
US10883466B2 (en) High altitude air start equipment for aircraft reciprocating engine
US8899009B2 (en) Fuel anti-icing and APU compartment drain combination
WO2020121301A1 (en) Method and system for autonomous cloud seeding
CN110963045A (en) Automatic anti-icing and deicing device for fuel wing of aircraft and working method of automatic anti-icing and deicing device

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20160810