CN105137464A - Emergency rescue positioning system for helicopter - Google Patents
Emergency rescue positioning system for helicopter Download PDFInfo
- Publication number
- CN105137464A CN105137464A CN201510494214.3A CN201510494214A CN105137464A CN 105137464 A CN105137464 A CN 105137464A CN 201510494214 A CN201510494214 A CN 201510494214A CN 105137464 A CN105137464 A CN 105137464A
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- CN
- China
- Prior art keywords
- helicopter
- positioning system
- emergency rescue
- positioning
- rescue
- 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.)
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
- G01S19/421—Determining position by combining or switching between position solutions or signals derived from different satellite radio beacon positioning systems; by combining or switching between position solutions or signals derived from different modes of operation in a single system
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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Transmitters (AREA)
Abstract
The invention discloses an emergency rescue positioning system for a helicopter. The emergency rescue positioning system for the helicopter comprises a transmitter and a receiver. The transmitter is provided with a host machine, an antenna and a control box. The receiver is provided with a host machine and an antenna. According to the emergency rescue positioning system, double systems are used for backup. The emergency rescue positioning system is provided with a GPS positioning unit, a Beidou positioning unit and a wireless signal positioning unit. The emergency rescue positioning system is provided with an automatic positioning information transmitting unit and a manual starting positioning information transmitting unit. When a fault of the helicopter occurs, automatic transmission or manual control box opening for transmitting is performed. The receiver performs active searching, thereby realizing efficient, stable and reliable long-distance emergency rescue target object positioning.
Description
Technical field
The present invention relates to a kind of helicopter accessory, particularly relate to a kind of helicopter emergency management and rescue positioning system.
Background technology
From the local war several times that the nineties in 20th century occurs, the U.S. and some western developed countries in order to realize the target of " zero injures and deaths " in war, except greatly developing advanced weaponry, also increase input in aviation lifesaving, establish advanced aviation lifesaving's system, this system becomes when helicopter can not be saved, and ensures the important technology equipment of aircrew's safe life-saving.Facts have proved that this system has played vital role in the various accident of helicopter daily workout, war and process.
China from the Wenchuan earthquake disaster relief finally several country rescue action, helicopter embodies obvious advantage in rescue action, it has reaction in time, action is fast, mountain area can be adapted to, forest, the ability of the multiple geographical environment such as ocean, can serve and search and rescue rescue, air resuce, police service is supported, fire-fighting fire extinguishing, aerial survety, the plurality of application scenes such as government affairs support, to meet the needs that each side's emergency management and rescue and government affairs are flown, China has had recognized that the importance and the urgency that strengthen China's aviation emergency management and rescue strength and build China's air rescue system, in construction aviation Lash-up succor system process, the quantity of helicopter and aerial mission will progressively increase, it will inevitably bring the increase of helicopter fault, therefore, the rescue ability of helicopter self is also important all the more.
Progressively promote along with military equipment is modern, military helicopter starts progressively to equip our troops in enormous quantities, the daily workout of army's helicopter and the amount of executing the task also synchronously increase, in the urgent need to the capability of fast response of Synchronous lifting daily workout management level and abnormal conditions process;
At daily workout with when executing the task, lead aircraft and controHower person need to obtain the current location information understood and specify wing plane in time sometimes;
Wish as required the flight path of assigned aircraft and parameter to be sent to ground in real time, be convenient to control tower and carry out floor manager and the technical Analysis after training, improve training management level;
When abnormal conditions appear in helicopter, because helicopter pilot is general without ejection escape device, now should guarantee persons on board's safety and disembark, needing to launch search rescue as early as possible simultaneously, take back distress personnel, etc.And emergency management and rescue positioning system is the key equipment launching quick rescue.
Summary of the invention
The object of this invention is to provide a kind of helicopter emergency management and rescue positioning system of efficient, stable, reliable remote emergency rescue location.
The object of the invention is to be achieved through the following technical solutions:
Helicopter emergency management and rescue positioning system of the present invention, comprise transmitter, receiver, described transmitter is provided with main frame, antenna and control enclosure, and described receiver is provided with main frame and antenna.
As seen from the above technical solution provided by the invention, the helicopter emergency management and rescue positioning system that the embodiment of the present invention provides, owing to comprising transmitter, receiver, transmitter is provided with main frame, antenna and control enclosure, receiver is provided with main frame and antenna, automatically launch when helicopter fault or the transmitting of manual unlocking control enclosure, receiver is initiatively searched, and reaches efficient, stable, reliable remote emergency rescue localizing objects.
Accompanying drawing explanation
The structural representation of the helicopter emergency management and rescue positioning system that Fig. 1 provides for the embodiment of the present invention.
Embodiment
To be described in further detail the embodiment of the present invention below.
Helicopter emergency management and rescue positioning system of the present invention, its preferably embodiment be:
Comprise transmitter, receiver, described transmitter is provided with main frame, antenna and control enclosure, and described receiver is provided with main frame and antenna.
This system adopts dual system backup.
This system has been provided with GPS positioning unit, Big Dipper positioning unit and wireless signal positioning unit.
This system is provided with automatic locating information transmitting element and manually boots locating information transmitting element.
Helicopter emergency management and rescue positioning system of the present invention, it contains transmitter and receiver composition, and described transmitter divides three part composition main frame, control enclosure, antennas.Described main frame is connected with described control enclosure by cable, and described main frame is connected with described antenna by cable.Described receiver divides two parts to form main frame, antenna.Described main frame is connected with described antenna by cable.By GPS and Big Dipper Dual positioning, automatically launch when helicopter fault or the transmitting of manual unlocking control enclosure, receiver is initiatively searched, and reaches efficient, stable, reliable remote emergency rescue localizing objects.System has fully used the advanced technology such as high-precision location technique, wireless communication technology, achieves high precision positioning position information, the object of long-distance transmissions location information data.
Specific embodiment:
As shown in Figure 1, utilize GPS and Big Dipper Dual positioning, automatically control transmitter when helicopter fault and to transmit or manual unlocking control enclosure transmits, whole space is extensively transmitted into by antenna, receiver is search signal initiatively, turn back to receiver main frame when antenna receives rescue signal, transmitter is positioned, reach efficient, stable, the localizing objects of remote emergency rescue reliably.
The above; be only the present invention's preferably embodiment, but protection scope of the present invention is not limited thereto, is anyly familiar with those skilled in the art in the technical scope that the present invention discloses; the change that can expect easily or replacement, all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain of claims.
Claims (4)
1. a helicopter emergency management and rescue positioning system, is characterized in that, comprises transmitter, receiver, and described transmitter is provided with main frame, antenna and control enclosure, and described receiver is provided with main frame and antenna.
2. helicopter emergency management and rescue positioning system according to claim 1, is characterized in that, this system adopts dual system backup.
3. helicopter emergency management and rescue positioning system according to claim 2, is characterized in that, this system has been provided with GPS positioning unit, Big Dipper positioning unit and wireless signal positioning unit.
4. the helicopter emergency management and rescue positioning system according to claim 1,2 or 3, is characterized in that, this system is provided with automatic locating information transmitting element and manually boots locating information transmitting element.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510494214.3A CN105137464A (en) | 2015-08-12 | 2015-08-12 | Emergency rescue positioning system for helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510494214.3A CN105137464A (en) | 2015-08-12 | 2015-08-12 | Emergency rescue positioning system for helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105137464A true CN105137464A (en) | 2015-12-09 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510494214.3A Pending CN105137464A (en) | 2015-08-12 | 2015-08-12 | Emergency rescue positioning system for helicopter |
Country Status (1)
| Country | Link |
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| CN (1) | CN105137464A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108688800A (en) * | 2017-04-03 | 2018-10-23 | 贝尔直升机德事隆公司 | System and method for the position for determining rotor craft |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0795760A2 (en) * | 1996-03-14 | 1997-09-17 | Koji Akai | Location search system |
| CN202563079U (en) * | 2012-04-28 | 2012-11-28 | 合肥佳讯科技有限公司 | Positioning tracker |
| CN202871093U (en) * | 2012-07-17 | 2013-04-10 | 北京华胜天成信息技术发展有限公司 | Vehicle smart terminal based on dual-mode navigation and positioning technology |
| CN203705642U (en) * | 2013-12-02 | 2014-07-09 | 太原航空仪表有限公司 | Emergency locating rescue device for aircraft |
| CN104280753A (en) * | 2014-02-11 | 2015-01-14 | 南京波格微电子有限公司 | Beidou emergency rescue terminal |
-
2015
- 2015-08-12 CN CN201510494214.3A patent/CN105137464A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0795760A2 (en) * | 1996-03-14 | 1997-09-17 | Koji Akai | Location search system |
| CN202563079U (en) * | 2012-04-28 | 2012-11-28 | 合肥佳讯科技有限公司 | Positioning tracker |
| CN202871093U (en) * | 2012-07-17 | 2013-04-10 | 北京华胜天成信息技术发展有限公司 | Vehicle smart terminal based on dual-mode navigation and positioning technology |
| CN203705642U (en) * | 2013-12-02 | 2014-07-09 | 太原航空仪表有限公司 | Emergency locating rescue device for aircraft |
| CN104280753A (en) * | 2014-02-11 | 2015-01-14 | 南京波格微电子有限公司 | Beidou emergency rescue terminal |
Non-Patent Citations (2)
| Title |
|---|
| 王文瑜: ""基于北斗卫星的授时系统研制"", 《中国优秀硕士学位论文全文数据库基础科学辑（月刊）》 * |
| 王文瑜: "基于北斗卫星的授时系统研制", 《中国优秀硕士学位论文全文数据库基础科学辑（月刊）》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108688800A (en) * | 2017-04-03 | 2018-10-23 | 贝尔直升机德事隆公司 | System and method for the position for determining rotor craft |
| CN108688800B (en) * | 2017-04-03 | 2021-09-24 | 贝尔直升机德事隆公司 | System and method for determining the position of a rotorcraft |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20151209 |
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| RJ01 | Rejection of invention patent application after publication |