CN207860442U - Fire-fighting fire extinguishing unmanned helicopter system - Google Patents

Fire-fighting fire extinguishing unmanned helicopter system Download PDF

Info

Publication number
CN207860442U
CN207860442U CN201721789981.8U CN201721789981U CN207860442U CN 207860442 U CN207860442 U CN 207860442U CN 201721789981 U CN201721789981 U CN 201721789981U CN 207860442 U CN207860442 U CN 207860442U
Authority
CN
China
Prior art keywords
fire
shell
rotor
tail
fire extinguishing
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
Application number
CN201721789981.8U
Other languages
Chinese (zh)
Inventor
章晨光
管建伟
马玉涛
葛贤坤
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.)
Jiangsu Tianyu Aviation Technology Group Ltd By Share Ltd
Original Assignee
Jiangsu Tianyu Aviation Technology Group Ltd By Share 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 Jiangsu Tianyu Aviation Technology Group Ltd By Share Ltd filed Critical Jiangsu Tianyu Aviation Technology Group Ltd By Share Ltd
Priority to CN201721789981.8U priority Critical patent/CN207860442U/en
Application granted granted Critical
Publication of CN207860442U publication Critical patent/CN207860442U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model patent is related to a kind of fire-fighting fire extinguishing unmanned helicopter system, including housing construction, dynamical system, flight control system, fire-fighting fire extinguishing gondola and Extinguishing bomb, the housing construction is made of main rotor, shell, tail-rotor and undercarriage, the undercarriage is arranged in the bottom of shell, the main rotor is mounted on the top of shell, and the tail-rotor is mounted on the side wall of shell tail end;The dynamical system is engine, and the engine is mounted in shell, and the engine is connected with main rotor and tail-rotor;The fire-fighting fire extinguishing gondola is mounted on the bottom of shell, and the fire-fighting fire extinguishing gondola is located in undercarriage, and the Extinguishing bomb is seated in inside fire-fighting fire extinguishing gondola;By using appeal structure, the utility model has the advantages of of low cost, efficiency-cost ratio is high, is used convenient for a large amount of equipments.

Description

Fire-fighting fire extinguishing unmanned helicopter system
Technical field
The utility model belongs to unmanned helicopter technical field, and in particular to a kind of unmanned plane for fire-fighting fire extinguishing is gone straight up to Machine system.
Background technology
Medium-and-large-sized unmanned helicopter is generally using the dynamic engine of oil as power, with load is big, cruise duration is long, energy is empty Middle hovering, the advantages that stability is good, easily controllable.Various industrial UAV system based on unmanned helicopter exploitation is It rapidly develops.
Since the high level of each big and medium-sized cities, high-rise building are increasing, fire-fighting fire extinguishing problem is always world-famous puzzle, Using unmanned plane carry out fire attack be a kind of effective solution approach, due to fixed-wing unmanned plane cannot hover, flexibility not It is enough, rotor wing unmanned aerial vehicle exploitation consumption unmanned plane and fire-extinguishing system can only be used.Currently without related ripe technology and auxiliary products.
Invention content
The utility model is directed to the demand, and fire-fighting fire extinguishing gondola, maximum load can be carried up to 30kg, continuous by having developed one kind ETS estimated time of sailing can effectively put out tetra- class primary fire of A, B, C, D up to 2 hours fire-fighting fire extinguishing unmanned helicopter systems.
In order to solve the above technical problems, the utility model provides a kind of fire-fighting fire extinguishing unmanned helicopter system, including Housing construction, dynamical system, flight control system, fire-fighting fire extinguishing gondola and Extinguishing bomb,
The housing construction is made of main rotor, shell, tail-rotor and undercarriage, and the undercarriage is arranged in shell The bottom of body, the main rotor are mounted on the top of shell, and the tail-rotor is mounted on the side wall of shell tail end;
Dynamical system is engine, and the engine is mounted in shell, the engine and main rotor and tail-rotor It is connected;
Row control system forms nobody together by battery, sensing system, integrated flight control system, differential global positioning system Helicopter is formed, and the battery, sensing system and integrated flight control system are mounted in shell, the differential GPS System is mounted on the top of shell, and the battery, sensing system, differential global positioning system and engine fly with integrated respectively Control system is electrically connected;
Fire-fighting fire extinguishing gondola is mounted on the bottom of shell, and the fire-fighting fire extinguishing gondola is located in undercarriage, and described disappears Fire extinguishing bullet is seated in inside fire-fighting fire extinguishing gondola.
Further:The shell is made of glass fiber material, 2.7 meters of the shell overall length, 1.11 meters of height.
Further:The main rotor is made of aluminum alloy materials, is made of two panels blade, 3.2 meters of diameter, paddle disk Area 8.04m2, the tail-rotor is also made of two panels blade, 0.55 meter of diameter, rotor disk area 0.238m2,The main rotor 1.8 meters of propeller hub center and tail-rotor distance.
Further:The engine be two-stroke water cooled engine, discharge capacity 350cc, mainly by engine body, Water pump, radiator, water pipe, thermostat composition, main paddle and tail-rotor, main biography are transmitted power to after engine work by driver Dynamic ratio 7.67, tail transmission ratio 1.14.
Further:The sensing system selects attitude measurement system, including 3 accelerometers and 3 angular speed Meter, described 3 accelerometers and 3 angular speed meters are electrically connected with integrated flight control system respectively.
Further:The fire-fighting fire extinguishing gondola includes 4 launching tubes, 1 double light gunsight and 1 emission control Box, described 4 launching tubes are connected with emission control box respectively, described 1 double light gunsight and 1 emission control box and one Body flight control system is electrically connected.
Further:The Extinguishing bomb is provided with 4 pieces, and described 4 pieces of Extinguishing bombs are filled in 4 hairs respectively In shooting cylinder.
Further:The Extinguishing bomb long 680mm, outer diameter 120mm.Head is made of Al-alloy metal, intermediate Body is made of brittleness friable material, and interior to fill 4kg high-efficiency water-base extinguishing chemicals, tail portion is driver, using propellant actuated.
With the above structure the utility model have the advantage that for:
(1) unmanned helicopter maximum ceiling is up to 1000 meters or more, and holds fire fighting truck maximum water spray height high and there was only 100 Rice, solves the problems, such as high-rise building fire attack.
(2) use unmanned helicopter to carry out fire attack, it is fast to set out speed, solve hold high fire fighting truck development rate it is slow, The problem high to site requirements.
(3) principle is advanced, and accuracy at target is high.Double light gunsight interior designs that system is specially equipped with have special trajectory control Algorithm processed can accurately calculate the point of impact, and the accuracy at target of fire extinguisher bomb can control to be less than 0.5 meter.
(4) of low cost, efficiency-cost ratio is high, used convenient for a large amount of equipments.
Description of the drawings
Utility model will be further described in detail below with reference to the attached drawings and specific embodiments.
Fig. 1 is the structural schematic diagram of the utility model.
Specific implementation mode
The utility model as shown in Figure 1 provides a kind of fire-fighting fire extinguishing unmanned helicopter system, including housing construction, power System, flight control system, fire-fighting fire extinguishing gondola and Extinguishing bomb, the housing construction are by main rotor 1, shell 2, tail Paddle 3 and undercarriage 4 are formed, and the undercarriage 4 is arranged in the bottom of shell 2, and the main rotor 1 is mounted on shell 2 Top, the tail-rotor 3 are mounted on the side wall of 2 tail end of shell;The dynamical system is engine 5, the engine 5 In shell 2, the engine 5 is connected with main rotor 1 and tail-rotor 3;The row control system is by battery 6, sensing Device system 7, integrated flight control system 8, differential global positioning system 9 form unmanned helicopter and are formed together, the battery 6, sensing Device system 7 and integrated flight control system 8 are mounted in shell 2, and the differential global positioning system 9 is mounted on the top of shell 2, institute Battery 6, sensing system 7, differential global positioning system 9 and the engine 5 stated are electrically connected with integrated flight control system 8 respectively;It is described to disappear Fire extinguishing gondola 10 is mounted on the bottom of shell 2, and the fire-fighting fire extinguishing gondola 10 is located in undercarriage 4, and the fire-fighting is gone out Fiery bullet 11 is seated in inside fire-fighting fire extinguishing gondola.
Shell 2 as shown in Figure 1 is made of glass fiber material, 2.7 meters of 2 overall length of shell, 1.11 meters of height; Configuration design is carried out according to internal body equipment, emphasis considers the small requirement of flight resistance, carries out whole die sinking design processing.
Main rotor 1 as shown in Figure 1 is made of aluminum alloy materials, is made of two panels blade, 3.2 meters of diameter, paddle disk Product 8.04m2, the tail-rotor 2 is also made of two panels blade, 0.55 meter of diameter, rotor disk area 0.238m2,The main rotor 1 1.8 meters of propeller hub center and tail-rotor distance;Turn left when work, in structure design, is designed using anticreep paddle, blade revolves in the air Turning can self-tightening.
Engine 5 as shown in Figure 1 is two-stroke water cooled engine, discharge capacity 350cc, mainly by engine body, water Pump, radiator, water pipe, thermostat composition, main paddle and tail-rotor, main transmission are transmitted power to after engine work by driver Than 7.67, tail transmission ratio 1.14;For the engine using the machine oil of common 92 ﹟ gasoline addition 5% as fuel, delivery efficiency is high, Good reliability, single stream time are not less than 4 hours, and the total working service life is not less than 1000 hours.
The sensing system 7 as shown in Figure 1 selects attitude measurement system, including 3 accelerometers and 3 angle speed Degree meter, described 3 accelerometers and 3 angular speed meters are electrically connected with integrated flight control system 8 respectively;Pass through 3 acceleration Meter and 3 angular speed meters can measure flight attitude in real time, and measurement result is sent into integrated flight control system 8, flight control system Unmanned plane stability analysis is controlled according to sensor measurement, and receives remote signal, control aircraft makes various flare maneuvers.
Fire-fighting fire extinguishing gondola 10 as shown in Figure 1 includes 4 launching tubes, 1 double light gunsight and 1 emission control box, 4 launching tubes are connected with emission control box respectively, described 1 double light gunsight and 1 emission control box and one Change flight control system 8 to be electrically connected;Target burning things which may cause a fire disaster can be accurately indicated by using above structure, and is being closed by the video pictures of passback When opportunity tip ground manipulation hand emit fire extinguisher bomb, gondola can receive ground hair control instruction, fire extinguisher bomb is reliably launched And accurately hit fire's point of origin.
Extinguishing bomb 11 as shown in Figure 1 is provided with 4 pieces, and described 4 pieces of Extinguishing bombs 11 are filled in 4 hairs respectively In shooting cylinder;The Extinguishing bomb 11 long 680mm, outer diameter 120mm;Head is made of Al-alloy metal, can penetrate and be not less than The glass of 20mm thickness, intermediate are made of brittleness friable material, and interior to fill 4kg high-efficiency water-base extinguishing chemicals, tail portion is driver, Using propellant actuated;Fire extinguishing resilience energy, which enters at interior of building burning things which may cause a fire disaster, to be acted on, and tetra- class primary fire of A, B, C, D is effectively put out.
Embodiment described above is only described preferred embodiments of the present invention, not to this reality It is defined with novel range, under the premise of not departing from the spirit of the design of the utility model, this field ordinary engineering and technical personnel The various modifications made to technical solutions of the utility model and improvement should all fall into claims determination of the utility model In protection domain.

Claims (8)

1. a kind of fire-fighting fire extinguishing unmanned helicopter system, it is characterised in that:Including housing construction, dynamical system, flight control system System, fire-fighting fire extinguishing gondola and Extinguishing bomb,
The housing construction is made of main rotor (1), shell (2), tail-rotor (3) and undercarriage (4), the undercarriage (4) setting is mounted on the top of shell (2) in the bottom of shell (2), the main rotor (1), and the tail-rotor (3) is mounted on On the side wall of shell (2) tail end;
The dynamical system is engine (5), and the engine (5) is mounted in shell (2), the engine (5) with Main rotor (1) is connected with tail-rotor (3);
The row control system is by battery (6), sensing system (7), integrated flight control system (8), differential global positioning system (9) Composition unmanned helicopter is formed together, and the battery (6), sensing system (7) and integrated flight control system (8) are mounted on In shell (2), the differential global positioning system (9) is mounted on the top of shell (2), the battery (6), sensing system (7), differential global positioning system (9) and engine (5) are electrically connected with integrated flight control system (8) respectively;
The fire-fighting fire extinguishing gondola (10) is mounted on the bottom of shell (2), and the fire-fighting fire extinguishing gondola (10) is located at undercarriage (4) in, the Extinguishing bomb (11) is seated in inside fire-fighting fire extinguishing gondola.
2. fire-fighting fire extinguishing unmanned helicopter system according to claim 1, it is characterised in that:The shell (2) uses Glass fiber material is made, 2.7 meters of the shell (2) overall length, 1.11 meters of height.
3. fire-fighting fire extinguishing unmanned helicopter system according to claim 1, it is characterised in that:The main rotor (1) is adopted It is made of aluminum alloy materials, is made of two panels blade, 3.2 meters of diameter, rotor disk area 8.04m2, the tail-rotor (3) is also by two Piece blade forms, 0.55 meter of diameter, rotor disk area 0.238m2,The propeller hub center of the main rotor (1) and tail-rotor distance 1.8 Rice.
4. fire-fighting fire extinguishing unmanned helicopter system according to claim 1, it is characterised in that:The engine (5) is Two-stroke water cooled engine, discharge capacity 350cc are mainly made of engine body, water pump, radiator, water pipe, thermostat, hair Main paddle and tail-rotor, final ratio 7.67, tail transmission ratio 1.14 are transmitted power to by driver after motivation work.
5. fire-fighting fire extinguishing unmanned helicopter system according to claim 1, it is characterised in that:The sensing system (7) attitude measurement system, including 3 accelerometers and 3 angular speed meters, described 3 accelerometers and 3 angular speed are selected Meter is electrically connected with integrated flight control system (8) respectively.
6. fire-fighting fire extinguishing unmanned helicopter system according to claim 1, it is characterised in that:The fire-fighting fire extinguishing gondola (10) include 4 launching tubes, 1 double light gunsight and 1 emission control box, described 4 launching tubes respectively with emission control Box is connected, and described 1 double light gunsights and 1 emission control box are electrically connected with integrated flight control system (8).
7. fire-fighting fire extinguishing unmanned helicopter system according to claim 6, it is characterised in that:The Extinguishing bomb (11) 4 pieces are provided with, described 4 pieces of Extinguishing bombs (11) are filled in respectively in 4 launching tubes.
8. the fire-fighting fire extinguishing unmanned helicopter system according to any one of claim 1 or 6, it is characterised in that:Described Extinguishing bomb (11) long 680mm, outer diameter 120mm, head are made of Al-alloy metal, and intermediate is brittleness friable material system At interior to fill 4kg high-efficiency water-base extinguishing chemicals, tail portion is driver, using propellant actuated.
CN201721789981.8U 2017-12-20 2017-12-20 Fire-fighting fire extinguishing unmanned helicopter system Active CN207860442U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721789981.8U CN207860442U (en) 2017-12-20 2017-12-20 Fire-fighting fire extinguishing unmanned helicopter system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721789981.8U CN207860442U (en) 2017-12-20 2017-12-20 Fire-fighting fire extinguishing unmanned helicopter system

Publications (1)

Publication Number Publication Date
CN207860442U true CN207860442U (en) 2018-09-14

Family

ID=63465611

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721789981.8U Active CN207860442U (en) 2017-12-20 2017-12-20 Fire-fighting fire extinguishing unmanned helicopter system

Country Status (1)

Country Link
CN (1) CN207860442U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108248838A (en) * 2017-12-20 2018-07-06 江苏天域航空科技集团股份有限公司 Fire-fighting fire extinguishing unmanned helicopter system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108248838A (en) * 2017-12-20 2018-07-06 江苏天域航空科技集团股份有限公司 Fire-fighting fire extinguishing unmanned helicopter system

Similar Documents

Publication Publication Date Title
US5549259A (en) Innovative airtankers and innovative methods for aerial fire fighting
CN102785778A (en) Tubular transmitting fire-extinguishing unmanned plane and fire-extinguishing control methods
WO2023070787A1 (en) Airdrop forest fire extinguishing bomb
CN204822083U (en) For military use alert unmanned aerial vehicle system that uses of multipurpose
CN208582895U (en) It is a kind of to break window fire extinguisher bomb without control drive
CN105963882A (en) Air-to-surface rocket fire extinguisher and method
CN104679987B (en) A kind of system efficiency evaluation method of military aircraft in the master-plan stage
CN107670201A (en) UAV system type fire extinguishing system
CN109436329A (en) A kind of small drone precisely emits the device and method of relief supplies in the air
CN207860442U (en) Fire-fighting fire extinguishing unmanned helicopter system
CN108619641A (en) A kind of fire extinguishing system and method for Vertical Launch guidance firefighting cartridge
CN206007850U (en) Air-to-surface missile fire extinguisher
CN108248838A (en) Fire-fighting fire extinguishing unmanned helicopter system
CN112618992B (en) Low-cost suicide networking fire extinguishing method and unmanned aerial vehicle system
CN103471472B (en) A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet
CN204275349U (en) A kind of fire extinguishing system
CN207860455U (en) Unmanned helicopter-mounted fire-fighting fire extinguishing gondola
CN112810815B (en) Low-cost suicide type fire extinguishing method and unmanned aerial vehicle
CN104492018A (en) Fire extinguishing method and fire extinguishing system in air mode
CN211996145U (en) Reconnaissance and fire fighting integrated forest fire-fighting fixed wing unmanned aerial vehicle with accurate fire extinguishing function
CN107008017B (en) A kind of dedicated multifunction detecting dummy vehicle of teenager's defence education
Dildy Dambusters: Operation Chastise 1943
CN1597019A (en) Fire extinguishing isolation bullet for forest having GPS guidance
Lardas Japan 1944–45: LeMay’s B-29 strategic bombing campaign
CN101975529A (en) High-altitude rocket launching system

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant