CN101927068B - Airline extinguishment auxiliary device and airline extinguishment method - Google Patents

Airline extinguishment auxiliary device and airline extinguishment method Download PDF

Info

Publication number
CN101927068B
CN101927068B CN2010102235291A CN201010223529A CN101927068B CN 101927068 B CN101927068 B CN 101927068B CN 2010102235291 A CN2010102235291 A CN 2010102235291A CN 201010223529 A CN201010223529 A CN 201010223529A CN 101927068 B CN101927068 B CN 101927068B
Authority
CN
China
Prior art keywords
fire
extinguishment
information
aircraft
flight
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
CN2010102235291A
Other languages
Chinese (zh)
Other versions
CN101927068A (en
Inventor
齐林
孙晓敏
王娜
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.)
Shanghai Avionics Co ltd
Original Assignee
China Aeronautical Radio Electronics Research Institute
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 China Aeronautical Radio Electronics Research Institute filed Critical China Aeronautical Radio Electronics Research Institute
Priority to CN2010102235291A priority Critical patent/CN101927068B/en
Publication of CN101927068A publication Critical patent/CN101927068A/en
Application granted granted Critical
Publication of CN101927068B publication Critical patent/CN101927068B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention discloses a device and a method for assisting airplanes to conduct airline extinguishment. The device is an onboard airline electronic system, comprising a navigation and combustion source sensor, a database system, a voice communication system, a data link, a human-computer interface, a display system, a data interface system and a comprehensive task processing system, wherein all systems are connected with a comprehensive task processing system. The device is utilized to conveniently formulate a flight plan on flying to the scene of fire, an extinguishment strategy flight plan and a round-trip water-drawing flight plan. Meanwhile, the device can monitor and alarm fire behavior display, extinguishment material spray suggestion, extinguishment material spray prediction and extinguishment flight tasks. The method and the device for implementing airline extinguishment researched by the invention can effectively assist pilots to conduct extinguishment, improve extinguishment success rate, save cost, and strengthen safety in the process of executing the tasks.

Description

A kind of airline extinguishment servicing unit and airline extinguishment method
Technical field
The present invention relates to a kind of Aerial extinguisher and method, particularly airborne avionics, flight plan, navigation, the auxiliary extinguishing material that sprays, the Aerial extinguisher and the method for the monitoring of fire extinguishing flight safety.
Background technology
The fire of diffusion is difficult to control usually on a large scale, causes serious harm for people's property and life security.Especially forest fire can spread in meadow and forest rapidly by wind action, forms the huge scene of a fire, and the scene of fire usually is in remote districts, and landform is dangerous in addition, makes control and stamps out a fire very difficulty.Current have many kinds of modes to control and stop spreading of fire, comprises conventional floor fire fighter and equipment, also comprises and use aircraft from the aerial extinguishing material that directly sprays.Adopt aircraft directly technological from the airline extinguishment of aerial spraying extinguishing material; Can directly stamp out a fire or form one section isolation strip, have good effect, the landform that particularly is difficult to arrive for ground fire-putting-out strength; Or remote scene of fire, the advantage of airline extinguishment is more obvious.Yet because fire is various informative; The influence of landform, wind makes that the situation of scene of fire is very complicated in addition; Guarantee that the safety of flight and effective input of extinguishing material are the comparison difficulties; Usually need the pilot to possess superb technology and rich experience, otherwise can cause the fire extinguishing poor effect, even the fatal crass.United States Patent (USP) U.S.No.5; 549; 259 " Innovative airtankers and innovative methods for aerial fire fighting " mentioned a kind of it is misty with the condition at night under the detection of fires symptom of a trend; And in time suppress the mode of fire with spraying liquid exactly, but can not formulate effective flight plan and vector aircraft flight to the characteristics of fire extinguishing task in this patent, need special acceleration liquid device and special military sighting device for the sprinkling of liquid; Cost is high, and not general for general air tanker.United States Patent (USP) U.S.No.5; 878; 819 " Device for assisting with the extinguishing of fires by water-bombing aircraft " have proposed a kind of detection and have accurately located burning things which may cause a fire disaster, and spray flight path and the flight path of leaving the scene of fire according to aircraft position and topographic database planning.This patent does not well solve the problem that extinguishing material sprays accuracy; Particularly do not show, provide the pilot, and effectively do not cooperate with Ground Control administrative center ground with reference to decision-making with form intuitively; Mode is dumb, can not bring into play the advantage of coordinated fire extinguishing better.United States Patent (USP) U.S.No.2010/0036549A1 " Methods And Systems For Display a predicted distribution of fire retardant material form an aircraft " has proposed a kind of flight management system prediction extinguishing material that uses and has landed the method in zone; Can on map, predict the landing zone of extinguishing material; Assisting in flying person throws in extinguishing material; But this mode is not considered the situation of aircraft on vertical section; Do not carry out performance suggestion, and do not consider the characteristics of fire and formulate the prediction fire extinguishing plan of optimization to the characteristics of fire extinguishing aerial mission.In addition, current airline extinguishment technology does not provide aboard yet can be used for the water source information that air tanker draws water, and to the characteristics of fire extinguishing aerial mission air tanker is not monitored, and ensures the technology of flight safety.
Summary of the invention
In order to change the main experience according to the fire extinguishing pilot of current airline extinguishment, complicated operation is difficult to accurately throw extinguishing material; The state of the art that lacks special monitoring fire extinguishing flight safety; The present invention provides a kind of general airline extinguishment method and servicing unit thereof, and the pilot that can help to put out a fire formulates rapidly and carries out the fire extinguishing plan, carries out the input of extinguishing material exactly; Thereby improve the ability of airline extinguishment; Alleviate driver's burden, and a kind of security monitoring and alarming mechanism are provided, effectively improve the security of fire extinguishing flight.
In order to realize goal of the invention of the present invention, the present invention adopts following technical scheme:
A kind of airline extinguishment servicing unit, this device is general airborne avionics, comprising: navigation and burning things which may cause a fire disaster sensor, Database Systems, voice communication system; The data chain, man-machine interface, display system, data-interface system and comprehensive task treatment system, said navigation and burning things which may cause a fire disaster sensor; Database Systems, voice communication system, data chain, man-machine interface; Display system, the data-interface system all links to each other with the comprehensive task treatment system, wherein
Navigation sensor is used for calculating the necessary navigation information of aircraft flight;
The burning things which may cause a fire disaster sensor is detection of fires zone and grade in certain distance;
Information such as Database Systems storage airport, way point, instrument flight procedure, available water source;
Voice communication system provides speech communication between pilot and ground control centre, ground fire-putting-out strength, other air attack strength;
The data chain, various data messages such as the transmission condition of a fire, fire extinguishing flight plan and meteorological condition;
Man-machine interface provides the pilot to formulate and revises flight plan and the interface of importing the information that from the speech communication system, transmits;
Display system provides flight plan information, navigation information, and condition of a fire situation information is sprayed the demonstration of advising;
Data interface unit provides the interface that other avionics system communicates on this device and the aircraft;
The comprehensive task treatment system is carried out described various calculating and information processing.
Said burning things which may cause a fire disaster sensor is the sensor of infrared sensor or imageing sensor or other form.
Said navigation sensor is the built-in GPS receiver of airline extinguishment servicing unit, or existing inertial navigation system, radionavigation sensor on the aircraft.
Said display system is the EFIS on multi-functional control display or the aircraft.
Said data interface unit is ARINC 429, CAN bus, bus forms such as MIL-STD-1553B.
Said Database Systems comprise standard database and self-defining database.
Can the be coupled storage extinguishing material device of aircraft of said man-machine interface is controlled the switch of storage extinguishing material device and the flow in the launch process.
A kind of method of airline extinguishment comprises the steps:
1) pilot is according to the requirement of sending at control and management center, ground, utilizes data such as airport in the navigational route database, guidance station, way point, water source to formulate the flight of scene of fire and the plan of drawing water of flying to;
2) after flight plan activates, display system shows flight plan information and navigation information, and the prestissimo suggestion is provided, and pilot's vector aircraft arrives the scene of fire rapidly;
3) behind the arrival scene of fire; Utilize sensor to survey burning things which may cause a fire disaster and accurately definite fire location of navigation sensor and scope; Show supplementary and send to other control force to the pilot; The pilot formulates fire extinguishing route planning and the route planning that withdraws from the scene of fire according to supplementary or through receiving mapping out the plan of Ground Control administrative center;
4) according to current air speed, highly, information prediction extinguishing material such as wind land the zone, and the aid decision advisory information is provided according to the estimation range of landing of conflagration area and extinguishing material;
5) according to the landform of aircraft current location calculating front region,, calculate the flight envelope of a safety, the demonstration of vertical section is provided in conjunction with the type of fire;
6) pilot is with reference to decision recommendation information, the control aircraft along the fire extinguishing route planning at appropriate heights, speed, be in due course and spray with suitable flow, form buffer zone or directly put out fire.
Repeatedly coming and going in the process that draws water, can store the path and the way point of self-defined flight plan, repeatedly directly call in the two-way process and carry out.After the sprinkling extinguishing material finished, the pilot called the information in the water source database, and the also maintenance plan of drawing water is formulated as drawing water the destination in the nearest water source of selecting to provide, and repeatedly enforcement fire extinguishing operation again draws water.
Basic principle of the present invention is when fire takes place; Ground Control administrative center disposes the airline extinguishment plan and sends air tanker to implement airline extinguishment, and the pilot formulates effective flight plan according to mapping out the plan and flies to draw water to the available waters of appointment, and aircraft flies to the scene of fire after accomplishing and drawing water; Confirm the aircraft position through sensor on the machine or communication system; Wind, the condition of a fire, the pilot confirms fire type; According to corresponding performance prompting, implement the sprinkling of extinguishing material with reference to the suggestion control aircraft of fire extinguishing decision information.In fire extinguishing task implementation, flight safety is monitored the security that the enhancing task is carried out.
The present invention has following advantage:
A) in fire extinguishing procedure, carry out air-ground dialogue in real time, the pilot can know the variation of the condition of a fire, the variation of strategic plan.And the mechanism change of flight plan rapidly of providing convenience.
B), can improve the security of flight through the state of surveillance aircraft on vertical section.
C) through keeping the historical data of flight plan, can in repeatedly coming and going draw water operation and sprinkling extinguishing material operation process, alleviate driver's burden effectively, raise the efficiency.
D) through setting up the water source distributed data base, and provide nearest water source selective, convenient the best flight plan that draws water of formulating is saved valuable attack time and fire extinguishing cost.
E) through machine upper sensor or data chain, and correlation experience and Performance Calculation, assisting in flying person carries out the accurate sprinkling of extinguishing material with suitable height, speed, and extinguishing material is utilized effectively.
In a word, use this patent can improve the efficient of airline extinguishment significantly, improve the security that fire extinguishing is flown.
Description of drawings
Fig. 1 implements the sketch map of airline extinguishment for aircraft.
Fig. 2 is the demonstration of the auxiliary fire extinguishing information on the horizontal profile of scene of fire.
Fig. 3 is for selecting the man-machine interface page of fire type.
Fig. 4 is the man-machine interface page of auxiliary extinguishing property suggestion.
Fig. 5 is near the monitoring flight plan on the vertical section and the page of the flight safety fire.
Fig. 6 is the structure chart of airline extinguishment servicing unit.
Fig. 7 is the functional block diagram of airline extinguishment servicing unit.
The specific embodiment
How further specify the present invention below in conjunction with accompanying drawing 1-Fig. 7 realizes.
Embodiment
Fig. 1 has explained a kind of method of having equipped the air tanker 101 enforcement airline extinguishments of apparatus of the present invention.When fire 102 took place, Ground Control administrative center 103 formulated fire extinguishing and maps out the plan, and sent air tanker 101 to implement airline extinguishment then, and when sending, mapping out the plan also can send air tanker 101 to through data chain 104a.Air tanker 101 is formulated the concrete flight plan 105a that comprises the process that draws water in the way according to mapping out the plan of control and management center, ground 103 before taking off; The pilot flies to the water source 106 according to flight plan 105a guiding air tanker 101 and draws water then, accomplishes the aircraft that loads water in the back that draws water and flies to implement airline extinguishments to fire 102.Aircraft is from aerial spraying extinguishing material 107, and extinguishing material 107 directly stamps out a fire 102, perhaps forms the burning things which may cause a fire disaster isolation strip, and tie surface personnel put out a fire.
The pilot can select to utilize airport, guidance station, the course line that is stored in the navigational route database when formulating concrete flight plan 105a, also can be self-defining longitude and latitude way point, special anchor point.The present invention also provides near the available water source 106 the fire 102 selective, and the pilot selects suitable water source according to specific circumstances, thereby makes apart from the shortest fire extinguishing flight plan 105a that draws water in the way that comprises.
In the way of fire 102 of flying to, display system provides the demonstration of flight plan 105a, and the demonstration of air tanker 101 current locations is provided, and the reference of flight guiding is provided for the pilot.The present invention can provide aircraft to arrive the speed suggestion of scene of fire the soonest according to aeroplane performance.
Implement in the process of fire extinguishing among Fig. 1, air tanker 101 constantly communicates through data chain 104b and Ground Control administrative center 103, transmits the on-the-spot condition of a fire and gives Ground Control administrative center 103, and receive new mapping out the plan.
Repeatedly coming and going in the process that draws water, can store the path 105b of self-defined flight plan, repeatedly directly call in the two-way process and carry out.For the driver reduces the heavy burdens.
Near the auxiliary fire extinguishing information sketch map that Fig. 2 has shown when having explained arriving fire 201.Sensing system on the air tanker 202 detects position, shape and the scope of fire, and the present invention can predict the rate of propagation of fire.
Navigation sensor is confirmed the position of air tanker 202, and highly, navigation information such as speed, other sensor can detect wind speed, direction.
The pilot can make according to these auxiliary information and implement the fire tactics flight plan 203 that extinguishing material sprays; If the scope of fire 201 is smaller; Can directly stamp out a fire 201; If fire 201 scopes are bigger, the tactical flying plan of then making can form the isolation strip on the ground, stops the diffusion of fire 201.
The present invention according to the speed of aircraft, highly, the extinguishing material weight of loading, throw in the speed of flow, wind and extinguishing material that direction prediction goes out to spray land zone 204.
The present invention estimates the zone of landing of when leaping fire 201 extinguishing material according to supplementary; If prediction is landed the zone and is departed from predetermined zone; Then provide side-play amount 205 promptings; The present invention provides directly fire tactics flight plan 203 is carried out the mode that parallel offset is provided with, and the pilot can generate the fire tactics flight plan 206 of skew easily according to side-play amount 205 promptings modification on the basis of original fire tactics flight plan 203.Thereby guarantee the accurate input of extinguishing material in the horizontal.
The present invention calculates best input extinguishing material constantly, and provides an input prompting, and the pilot confirms to topple over extinguishing material according to throwing in to point out, thereby exactly extinguishing material is sprayed to predetermined zone.In another kind is implemented, the pilot according to fire tactics flight plan 203 with land zone 204 and confirm that the moment of suitable input extinguishing material is sprayed to predetermined zone with extinguishing material.
The man-machine interface that Fig. 3 provides the pilot to select fire type is divided into the ground fire with fire according to self character, and the top fire spreads fire, vexed combustion fire, torch fire, flaring fire, spot fire, whirlwind fire.The pilot selects fire type according to observation or other external strength communication.
Fig. 4 has provided the man-machine interface of extinguishing property suggestion, and the present invention can calculate suitable flying height, speed, input flow confession pilot reference according to the fire type of selecting.Suggestion and the demonstration of release time are provided simultaneously, and the demonstration of residue extinguishing material is provided.The pilot with reference to aircraft flight vertical section control aircraft along the fire extinguishing route planning at appropriate heights, the flow of speed and extinguishing material sprays, form buffer zone or directly put out fire.
Parameter among Fig. 4 can be a computation optimization of the present invention, also can manually import through the pilot, and they will be distinguished with various colors.
Provided in the fire extinguishing implementation process display format among Fig. 5 to monitoring and the alarm of air tanker 202.Display system demonstrates current landform 501 along fire tactics flight plan 205 paths according to topographic database; The present invention can calculate a fire extinguishing flight safety envelope 503; And will show with fire extinguishing flight safety envelope 503 along the vertical section 504 of fire tactics flight plan 205, a kind of typical display mode is as shown in Figure 5.When the height along the vertical section 504 of fire tactics flight plan 205 that predicts aircraft is lower than fire extinguishing flight safety envelope 503; Aircraft will send alarm; Warning information 505 may be displayed on the display system, also can offer the pilot with the form of alarm sound.The pilot revises fire tactics flight plan 505 according to alarm, thereby ensures flight safety.
When calculating fire extinguishing flight safety envelope 503, need to consider landform 501, fire 502 situation, the vegetation along fire tactics flight plan 205, current meteorological condition, and the performance characteristics of aircraft itself.
Shown in Figure 6 is a kind of device of auxiliary aviation fire extinguishing, comprising:
Burning things which may cause a fire disaster sensor 601 can be surveyed the zone and the grade of burning things which may cause a fire disaster in certain distance.Can be infrared sensor, also can be the sensor of imageing sensor or other form.
Navigation sensor 602 calculates the necessary navigation information of aircraft flight, comprises the position, speed, height of aircraft etc.Navigation sensor can be the built-in GPS receivers of apparatus of the present invention, also can be existing inertial navigation system on the aircraft, radionavigation sensor.
Voice communication system 603 provides pilot and Ground Control administrative center, ground fire-putting-out strength, the wherein speech communication between the air attack strength.
Data chain 604 can transmit the condition of a fire, fire extinguishing flight plan, various data messages such as meteorological condition, and message form can be figure and text.Can be forms such as very high frequency(VHF) (VHF), high frequency (HF), satellite communication.
Display system 605 provides flight plan information, navigation information, condition of a fire situation information, the demonstration of sprinkling suggestion etc.The mode that shows can be a graphical symbol, text prompt.Display system can be the multi-functional control display, also can be the EFIS on the aircraft.
Data interface unit 606, the interface that provides this device and other avionics system to communicate.Can be ARINC 429, CAN bus, bus forms such as MIL-STD-1553B.EBI also can be configured according to the special bus of aircraft platform.
Database Systems 607, information such as storage airport, way point, instrument flight procedure, available water source.Database Systems also comprise terrain data.Database can comprise standard database, also comprises self-defining database, particularly the water source database.
Man-machine interface 608 provides the pilot to formulate flight plan, confirms the interface of the condition of a fire and various task operatings.A kind of typical man-machine interface is the form that multi-functional control shows.Also can the be coupled storage extinguishing material device of aircraft of man-machine interface 608 is controlled the switch of storage extinguishing material device and the flow in the launch process.
Comprehensive task handles 609, carries out described various calculating and processing.
Fig. 7 is a kind of typical functions module map of described auxiliary aviation extinguishing device.Fire source probing 701 is handled burning things which may cause a fire disaster sensor 601 information, confirms the shape and the scope of fire, concentration etc., and give demonstration with process result and handle Unit 710.Numerical map 702 extracts terrain data and handles from database 607, and gives demonstration with the result and handle 710.The input that navigation information that navigation calculating 703 provides according to navigation sensor 602 and man-machine interface 709 the provide Management Calculation of navigating provides suitable navigation information.Atmosphere height 704 calculates the height of aircraft according to atmospheric information.Data chain 705 is handled the data that transmit from Ground Control administrative center 103.Interface is handled 706 and is handled the crosslinked various information of other avionic device from the aircraft, comprises input and output.The calculating of landing performance suggestion among calculating and the Fig. 4 in zone 204 of foregoing extinguishing material is accomplished in extinguishing property prediction/suggestion 707, and the calculating decision-making assistant information.Flight plan 708 is accomplished the foundation of foregoing fire tactics flight plan 205 and is revised and handle.Fire extinguishing pilot and interactive information of the present invention are handled in man-machine interface 709.Display system 710 is carried out synthesis display with the result of fire source probing 701, numerical map 702, navigation calculating 703, radar altitude 704, data chain 705, interface processing 706, extinguishing property prediction/suggestion 707, flight plan 708, man-machine interface 709 and is handled; Various information are had clearly present to the pilot, assisting in flying person makes a strategic decision.

Claims (9)

1. airline extinguishment servicing unit, this device is general airborne avionics, comprising: navigation and burning things which may cause a fire disaster sensor, Database Systems, voice communication system; The data chain, man-machine interface, display system, data-interface system and comprehensive task treatment system is characterized in that: said navigation and burning things which may cause a fire disaster sensor; Database Systems, voice communication system, data chain, man-machine interface; Display system, the data-interface system all links to each other with the comprehensive task treatment system, wherein
Navigation sensor is used for calculating the necessary navigation information of aircraft flight;
The burning things which may cause a fire disaster sensor is detection of fires zone and grade in certain distance;
Database Systems storage airport, way point, guidance station, instrument flight procedure, course line, available water source information;
Voice communication system provides speech communication between pilot and ground control centre, ground fire-putting-out strength, other air attack strength;
The data chain, the transmission condition of a fire, fire extinguishing flight plan and meteorological conditional information;
Man-machine interface provides the pilot to formulate and revises flight plan and the interface of importing the information that from the speech communication system, transmits;
Display system provides flight plan information, navigation information, and condition of a fire situation information is sprayed the demonstration of advising;
Data interface unit provides the interface that other avionics system communicates on this device and the aircraft;
The comprehensive task treatment system is carried out described various calculating and information processing.
2. a kind of airline extinguishment servicing unit according to claim 1 is characterized in that said burning things which may cause a fire disaster sensor is infrared sensor or imageing sensor.
3. a kind of airline extinguishment servicing unit according to claim 1 is characterized in that, said navigation sensor is the built-in GPS receiver of airline extinguishment servicing unit, or existing inertial navigation system, radionavigation sensor on the aircraft.
4. a kind of airline extinguishment servicing unit according to claim 1 is characterized in that said display system is the EFIS on multi-functional control display or the aircraft.
5. a kind of airline extinguishment servicing unit according to claim 1 is characterized in that said data interface unit is ARINC429, CAN bus or MIL-STD-1553B bus form.
6. a kind of airline extinguishment servicing unit according to claim 1 is characterized in that said Database Systems comprise standard database and self-defining database.
7. a kind of airline extinguishment servicing unit according to claim 1 is characterized in that, can the be coupled storage extinguishing material device of aircraft of man-machine interface is controlled the switch of storage extinguishing material device and the flow in the launch process.
8. the method for an airline extinguishment comprises the steps:
1) pilot utilizes airport, guidance station, way point, instrument flight procedure, course line, water source data in the navigational route database to formulate the flight of scene of fire and the plan of drawing water of flying to according to the requirement of sending at control and management center, ground;
2) after flight plan activates, display system shows flight plan information and navigation information, and the suggestion of the fastest speed of aircraft is provided, and pilot's vector aircraft arrives the scene of fire rapidly;
3) behind the arrival scene of fire; Utilize sensor to survey burning things which may cause a fire disaster and accurately definite fire location of navigation sensor and scope; Show supplementary and send to other control force to the pilot; The pilot formulates fire extinguishing route planning and the route planning that withdraws from the scene of fire according to supplementary or through receiving mapping out the plan of Ground Control administrative center;
4) according to current air speed, highly, the information prediction extinguishing material of wind land the zone, and the aid decision advisory information is provided according to the estimation range of landing of conflagration area and extinguishing material;
5) according to the landform of aircraft current location calculating front region,, calculate the flight envelope of a safety, the demonstration of vertical section is provided in conjunction with the type of fire;
6) pilot is with reference to decision recommendation information, the control aircraft along the fire extinguishing route planning at appropriate heights, speed, be in due course and spray with suitable flow, form buffer zone or directly put out fire.
9. a kind of airline extinguishment method according to claim 8 is characterized in that, repeatedly coming and going in the process that draws water, stores the path and the way point of self-defined flight plan, repeatedly directly calls in the two-way process and carries out.
CN2010102235291A 2010-07-05 2010-07-05 Airline extinguishment auxiliary device and airline extinguishment method Active CN101927068B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010102235291A CN101927068B (en) 2010-07-05 2010-07-05 Airline extinguishment auxiliary device and airline extinguishment method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010102235291A CN101927068B (en) 2010-07-05 2010-07-05 Airline extinguishment auxiliary device and airline extinguishment method

Publications (2)

Publication Number Publication Date
CN101927068A CN101927068A (en) 2010-12-29
CN101927068B true CN101927068B (en) 2012-04-11

Family

ID=43366661

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010102235291A Active CN101927068B (en) 2010-07-05 2010-07-05 Airline extinguishment auxiliary device and airline extinguishment method

Country Status (1)

Country Link
CN (1) CN101927068B (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103253373A (en) * 2012-02-21 2013-08-21 吴泽邦 Multifunctional unmanned machine platform capable of feeding water continuously for in-air fire-fighting rescue and rescue method thereof
CN103310578B (en) * 2013-07-04 2015-07-08 东北林业大学 Forest aviatic firefighting water fire extinguishing system and method
CN104127971B (en) * 2014-08-21 2015-10-21 国家电网公司 A kind of helicopter of transmission line forest fire of putting out a fire to save life and property carries high-pressure water-saving extinguishing water cannon
CN104808620A (en) * 2015-03-09 2015-07-29 中国航空工业集团公司沈阳飞机设计研究所 GJB289A serial bus-based distributed aircraft management system architecture
CN105527382B (en) * 2016-01-05 2018-03-02 杭州潮流玩具有限公司 A kind of fly able air detection equipment and use its mobile terminal
CN106384403B (en) * 2016-09-21 2018-11-30 江西天祥通用航空股份有限公司 A kind of airplane spray track recording method and system
JP6962720B2 (en) 2017-06-21 2021-11-05 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドSz Dji Technology Co., Ltd Flight control methods, information processing equipment, programs and recording media
CN107272737A (en) * 2017-07-11 2017-10-20 广东容祺智能科技有限公司 It is a kind of accurately to be jettisoninged control system based on unmanned plane
KR102617265B1 (en) * 2018-03-13 2023-12-26 삼성전자주식회사 The apparatus for processing user voice input
CN110025905A (en) * 2019-03-29 2019-07-19 芜湖市极星航空科技有限公司 A kind of airline extinguishment auxiliary device and airline extinguishment method
CN110201339A (en) * 2019-05-29 2019-09-06 李成 Home safety management system based on Internet of Things
CN110812732A (en) * 2019-10-12 2020-02-21 中航通飞研究院有限公司 Fire extinguishing method and system based on airplane platform
CN111013046A (en) * 2019-11-30 2020-04-17 芜湖市努尔航空信息科技有限公司 Aviation fire extinguishing auxiliary device and aviation fire extinguishing method
CN111401715B (en) * 2020-03-10 2023-10-10 国网湖南省电力有限公司 Aviation accurate fire extinguishing evaluation method and evaluation system thereof
CN113599738B (en) * 2021-07-07 2023-03-14 庆安集团有限公司 Aviation fire extinguishing task control system and control method
CN113975697A (en) * 2021-10-25 2022-01-28 中航通飞华南飞机工业有限公司 Fire-fighting aircraft water-drawing takeoff alarming method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5794889A (en) * 1995-06-06 1998-08-18 Raytheon Company Fire retardant delivery system
CN1223155A (en) * 1998-11-12 1999-07-21 易元明 Low-temp. oxygen free air forest fire-extinguishing machine
US20050072880A1 (en) * 2003-10-01 2005-04-07 Nolan Brooks R. Systems and methods for aerial dispersion of materials

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5794889A (en) * 1995-06-06 1998-08-18 Raytheon Company Fire retardant delivery system
CN1223155A (en) * 1998-11-12 1999-07-21 易元明 Low-temp. oxygen free air forest fire-extinguishing machine
US20050072880A1 (en) * 2003-10-01 2005-04-07 Nolan Brooks R. Systems and methods for aerial dispersion of materials

Also Published As

Publication number Publication date
CN101927068A (en) 2010-12-29

Similar Documents

Publication Publication Date Title
CN101927068B (en) Airline extinguishment auxiliary device and airline extinguishment method
AU2018317851B2 (en) An unmanned aerial vehicle system for inspecting railroad assets
EP0965118B1 (en) Apparatus for indicating air traffic and terrain collision threat to an aircraft
US11787560B2 (en) Computer-based systems and methods for facilitating aircraft approach
US7437225B1 (en) Flight management system
RU2550887C2 (en) On-board integrated crew support information system and cognitive format of presenting flight information at take-off phase of multi-engine aircraft
US10766605B2 (en) Emergency control of an aircraft
US20080270020A1 (en) Method, Arrangement and Monitoring Device for Navigation of Aircraft and Ground Vehicles Using Satellite-Assisted Positioning
RU2520174C2 (en) Helicopter onboard hardware complex
US20070150124A1 (en) Methods and systems for displaying enroute moving maps
WO1994027162A1 (en) Apparatus and method for closing flight plans and locating aircraft
RU2654660C2 (en) Device and method of direct broadcasting alarm system
CN103699132B (en) Device and method for assisting visual disc to precess and approach
JP4174559B2 (en) Advanced visibility information providing system and method using satellite image and flight obstacle recognition system and method
US10502584B1 (en) Mission monitor and controller for autonomous unmanned vehicles
US10984664B2 (en) System for determining potential landing sites for aircraft prior to landing assist device deployment
ITRM20070214A1 (en) ELECTRONIC EQUIPMENT FOR HIGH-PROTECTION SURVEILLANCE OF AIR TRAFFIC TO INHIBIT THE UNAUTHORIZED USE OF AIRCRAFT
JPH1144551A (en) Mounted-type navigation apparatus including topography display function
RU100836U1 (en) COMPLEX OF CONTROL AND CONTROL FOR SELF-DRIVING ON LOCAL AIRLINES ON THE BASIS OF MODERN TECHNOLOGIES
JP2003127997A (en) Obstacle avoiding system for flying object and manned flying object
JPH0672390A (en) Aviation system of aircraft
JP2006338132A (en) Dynamic state information monitoring device for airplane
Bueno et al. Human and technical performance aspects in RPAS integration trials in controlled airspace
Vengadesh et al. Design and development of aircraft to aircraft communication by Ad-Hoc networks
Nakamura et al. Flight demonstration for information sharing to avoid collisions between small unmanned aerial systems (sUASs) and manned helicopters

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20220720

Address after: 200241 Building 5, No. 432, ziyue Road, Minhang District, Shanghai

Patentee after: Shanghai avionics Co.,Ltd.

Address before: 200233 No. 432, Guiping Road, Shanghai

Patentee before: CHINA AERONAUTICAL RADIO ELECTRONICS Research Institute