CN105182330A - Flight type radar life detector - Google Patents
Flight type radar life detector Download PDFInfo
- Publication number
- CN105182330A CN105182330A CN201510683245.3A CN201510683245A CN105182330A CN 105182330 A CN105182330 A CN 105182330A CN 201510683245 A CN201510683245 A CN 201510683245A CN 105182330 A CN105182330 A CN 105182330A
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- CN
- China
- Prior art keywords
- life
- signal
- control box
- radar
- detection instrument
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Classifications
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- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention belongs to the electron equipment technical field, and discloses a flight type radar life detector comprising a control box, an operation page, a display, aircraft direction control handles, a human life information screen, an equipment cabin, an antenna, a rotor, a motor and an undercarriage; a flight type radar life detector control system comprises an LED light source, a power supply portion, a camera, a radar detection wave, a microphone, a noise reduction unit, a loudspeaker, a signal amplifier1, a signal acquisition portion, a filter signal sensor, a signal amplifier 2, a video reception end, a voice reception end and life characteristic information; the top of the control box is provided with the human life information screen; two sides of the control box are respectively provided with the aircraft direction control handle; one end of the control box is provided with the operation page and the display arranged on the top of the operation page; the bottom of the equipment cabin is provided with the undercarriage; the flight type radar life detector is strong in function, wide in life detection scope, thus greatly improving rescue strength.
Description
Technical field
The present invention relates to a kind of radar life-detection instrument, be specifically related to a kind of flight formula radar life-detection instrument, belong to technical field of electronic equipment.
Background technology
Life-detection instrument, be applicable to the mechanisms such as fire-fighting, municipal administration, mine rescue for earthquake, cave in, ruins rescue under building collapsing.Ocean patrol is affixed one's name to, customs, border, harbour, security staff can detect laminated container and whether steal into another country personnel, based on the safe life-saving system (life-detection instrument) of this new technology, successfully solve the problem of multinomial puzzlement conventional security life saving system, make search-and-rescue work rapider than ever, more accurate, also safer, it is present state-of-the-art life-detection system in the world, existing technology, be mostly hand-held vital detection instrument, and Effect on Detecting is poor, and, some rescue site is more dangerous, the personal safety of rescue personnel cannot be protected, for this reason, we propose a kind of flight formula radar life-detection instrument.
Summary of the invention
The technical problem to be solved in the present invention overcomes existing defect, provides a kind of flight formula radar life-detection instrument, this flight formula radar life-detection instrument, by force functional, life detection scope is wide, substantially increases rescue dynamics, effectively can solve the problem in background technology.
In order to solve the problems of the technologies described above, the invention provides following technical scheme:
The invention provides a kind of flight formula radar life-detection instrument, comprise control box, operation pages, display screen, aircraft direction control handle, human life information is shielded, equipment compartment, antenna, rotor, motor and undercarriage, described flight formula radar life-detection instrument control system comprises LED light source, power supply unit, camera, radar detection ripple, microphone, noise reduction unit, loudspeaker, signal amplifier, signal acquisition part, filtering signal sensor, signal amplifier, video receiver, phonetic incepting end and vital signs information, described control box top is provided with human life information's screen, described control box both sides are equipped with aircraft direction control handle, described control box one end is provided with operation pages and is arranged on the display screen at operation pages top, undercarriage is provided with bottom described equipment compartment, described equipment compartment surrounding is provided with rotor and is arranged on the motor bottom rotor, and described equipment compartment top is provided with antenna, and described equipment compartment is separately provided with camera, radar detection ripple and microphone, described camera is provided with LED light source and is arranged on the power supply unit on LED light source, and described microphone is provided with loudspeaker and noise reduction unit, described camera, radar detection ripple and microphone will detect data by signal amplifier through antenna transmission to signal acquisition part.
As a preferred technical solution of the present invention, described control box built-in signal collection portion, filtering signal sensor, signal amplifier 2, video receiver, phonetic incepting end and vital signs information.
As a preferred technical solution of the present invention, data are transported to video receiver, phonetic incepting end and vital signs information to described signal acquisition part by signal transducer and signal amplifier 2 after filtering successively.
As a preferred technical solution of the present invention, described video receiver, phonetic incepting end and vital signs information are presented on display screen and human life information's screen successively.
As a preferred technical solution of the present invention, described vital signs information comprises body temperature, breathing, health.
The beneficial effect that the present invention reaches is: a kind of flight formula radar life-detection instrument, adopt aircraft as the transport agent of radar detector, expand investigative range, ensure that the life safety of rescue personnel, because LED light source is arranged on camera, can allow camera to adopt the image taken the photograph more clear, be convenient to rescue, adopt signal amplifier 1 and signal amplifier 2 circuit, the information dropout that radar can be avoided to gather or the interference by environment, greatly improve rescue dynamics, ensure that survivor is found in time, because noise reduction unit and loudspeaker are arranged on microphone, can effectively avoid noise to the collection of voice messaging.
Accompanying drawing explanation
Accompanying drawing is used to provide a further understanding of the present invention, and forms a part for instructions, together with embodiments of the present invention for explaining the present invention, is not construed as limiting the invention.
In the accompanying drawings:
Fig. 1 is the one flight formula radar life-detection instrument one-piece construction schematic diagram described in the embodiment of the present invention;
Fig. 2 is the one flight formula radar life-detection instrument radar Flight Vehicle Structure schematic diagram described in the embodiment of the present invention;
Fig. 3 is that the one flight formula radar life-detection instrument information acquisition described in the embodiment of the present invention controls schematic diagram;
Number in the figure: 1, control box; 2, operation pages; 3, display screen; 4, aircraft direction control handle; 5, human life information's screen; 6, equipment compartment; 7, antenna; 8, rotor; 9, motor; 10, undercarriage.
Embodiment
Below in conjunction with accompanying drawing, the preferred embodiments of the present invention are described, should be appreciated that preferred embodiment described herein is only for instruction and explanation of the present invention, is not intended to limit the present invention.
Embodiment: refer to Fig. 1-3, a kind of flight formula of the present invention radar life-detection instrument, comprises control box 1, operation pages 2, display screen 3, aircraft direction control handle 4, human life information shields 5, equipment compartment 6, antenna 7, rotor 8, motor 9 and undercarriage 10, described flight formula radar life-detection instrument control system comprises LED light source, power supply unit, camera, radar detection ripple, microphone, noise reduction unit, loudspeaker, signal amplifier 1, signal acquisition part, filtering signal sensor, signal amplifier 2, video receiver, phonetic incepting end and vital signs information, described control box 1 top is provided with human life information and shields 5, described control box 1 both sides are equipped with aircraft direction control handle 4, described control box 1 one end is provided with operation pages 2 and is arranged on the display screen 3 at operation pages 2 top, undercarriage 10 is provided with bottom described equipment compartment 6, described equipment compartment 6 surrounding is provided with rotor 8 and is arranged on the motor 9 bottom rotor 8, and described equipment compartment 6 top is provided with antenna 7, and described equipment compartment 6 is separately provided with camera, radar detection ripple and microphone, described camera is provided with LED light source and is arranged on the power supply unit on LED light source, and described microphone is provided with loudspeaker and noise reduction unit, described camera, detection data are transferred to signal acquisition part by signal amplifier 1 through antenna 7 by radar detection ripple and microphone.
Described control box 1 built-in signal collection portion, filtering signal sensor, signal amplifier 2, video receiver, phonetic incepting end and vital signs information, data are transported to video receiver to described signal acquisition part by signal transducer and signal amplifier 2 after filtering successively, phonetic incepting end and vital signs information, described video receiver, phonetic incepting end and vital signs information are presented at display screen 3 successively and human life information is shielded on 5, described vital signs information comprises body temperature, breathe, health, adopt aircraft as the transport agent of radar detector, expand investigative range, ensure that the life safety of rescue personnel, because LED light source is arranged on camera, can allow camera to adopt the image taken the photograph more clear, be convenient to rescue, adopt signal amplifier 1 and signal amplifier 2 circuit, the information dropout that radar can be avoided to gather or the interference by environment, greatly improve rescue dynamics, ensure that survivor is found in time, because noise reduction unit and loudspeaker are arranged on microphone, can effectively avoid noise to the collection of voice messaging, this flight formula radar life-detection instrument, by force functional, life detection scope is wide, substantially increase rescue dynamics.
It should be noted that, the present invention is a kind of flight formula radar life-detection instrument, during work, after rescue personnel arrives rescue site, first by the heading in aircraft direction control handle 4 opertaing device cabin 6, camera, radar detection ripple and microphone can by the information of collection successively through signal amplifiers 1, signal acquisition part, filtering signal sensor, video receiver transported to by signal amplifier 2, phonetic incepting end and vital signs information, finally transfer to display screen 3 and human life information shields 5, this flight formula radar life-detection instrument improves the probability of surviving of survivor greatly.
Last it is noted that the foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, although with reference to previous embodiment to invention has been detailed description, for a person skilled in the art, it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.
Claims (5)
1. fly a formula radar life-detection instrument, comprises control box (1), operation pages (2), display screen (3), aircraft direction control handle (4), human life information shields (5), equipment compartment (6), antenna (7), rotor (8), motor (9) and undercarriage (10), is characterized in that, described flight formula radar life-detection instrument control system comprises LED light source, power supply unit, camera, radar detection ripple, microphone, noise reduction unit, loudspeaker, signal amplifier 1, signal acquisition part, filtering signal sensor, signal amplifier 2, video receiver, phonetic incepting end and vital signs information, described control box (1) top is provided with human life information's screen (5), described control box (1) both sides are equipped with aircraft direction control handle (4), described control box (1) one end is provided with operation pages (2) and is arranged on the display screen (3) at operation pages (2) top, described equipment compartment (6) bottom is provided with undercarriage (10), described equipment compartment (6) surrounding is provided with rotor (8) and is arranged on the motor (9) of rotor (8) bottom, described equipment compartment (6) top is provided with antenna (7), and (6) are separately provided with camera to described equipment compartment, radar detection ripple and microphone, described camera is provided with LED light source and is arranged on the power supply unit on LED light source, and described microphone is provided with loudspeaker and noise reduction unit, described camera, radar detection ripple and microphone will detect data and transfer to signal acquisition part by signal amplifier 1 through antenna (7).
2. a kind of flight formula radar life-detection instrument according to claim 1, it is characterized in that, described control box (1) built-in signal collection portion, filtering signal sensor, signal amplifier 2, video receiver, phonetic incepting end and vital signs information.
3. a kind of flight formula radar life-detection instrument according to claim 1, is characterized in that, data are transported to video receiver, phonetic incepting end and vital signs information to described signal acquisition part by signal transducer and signal amplifier 2 after filtering successively.
4. a kind of flight formula radar life-detection instrument according to claim 1, is characterized in that, described video receiver, phonetic incepting end and vital signs information are presented on display screen (3) and human life information's screen (5) successively.
5. a kind of flight formula radar life-detection instrument according to claim 1, it is characterized in that, described vital signs information comprises body temperature, breathing, health.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510683245.3A CN105182330A (en) | 2015-10-20 | 2015-10-20 | Flight type radar life detector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510683245.3A CN105182330A (en) | 2015-10-20 | 2015-10-20 | Flight type radar life detector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105182330A true CN105182330A (en) | 2015-12-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510683245.3A Pending CN105182330A (en) | 2015-10-20 | 2015-10-20 | Flight type radar life detector |
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| CN (1) | CN105182330A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106737704A (en) * | 2016-11-23 | 2017-05-31 | 河池学院 | A kind of rabid ox disease detects flight Micro-Robot |
| CN106737705A (en) * | 2016-11-23 | 2017-05-31 | 河池学院 | A kind of rabid ox disease detection and in time anesthesia flight Micro-Robot |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101508344A (en) * | 2009-03-25 | 2009-08-19 | 江苏省安全生产科学研究院 | Emergency rescue assisting device and use thereof |
| CN203444123U (en) * | 2013-08-05 | 2014-02-19 | 朱小炜 | Flight life detector |
| CN104608929A (en) * | 2015-02-10 | 2015-05-13 | 襄阳宏伟航空器有限责任公司 | Low-altitude rescue flight platform |
| CN204415739U (en) * | 2015-01-23 | 2015-06-24 | 武汉大学 | Rescue system is assisted in a kind of scene of fire based on quadrotor |
-
2015
- 2015-10-20 CN CN201510683245.3A patent/CN105182330A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101508344A (en) * | 2009-03-25 | 2009-08-19 | 江苏省安全生产科学研究院 | Emergency rescue assisting device and use thereof |
| CN203444123U (en) * | 2013-08-05 | 2014-02-19 | 朱小炜 | Flight life detector |
| CN204415739U (en) * | 2015-01-23 | 2015-06-24 | 武汉大学 | Rescue system is assisted in a kind of scene of fire based on quadrotor |
| CN104608929A (en) * | 2015-02-10 | 2015-05-13 | 襄阳宏伟航空器有限责任公司 | Low-altitude rescue flight platform |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106737704A (en) * | 2016-11-23 | 2017-05-31 | 河池学院 | A kind of rabid ox disease detects flight Micro-Robot |
| CN106737705A (en) * | 2016-11-23 | 2017-05-31 | 河池学院 | A kind of rabid ox disease detection and in time anesthesia flight Micro-Robot |
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Application publication date: 20151223 |
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| RJ01 | Rejection of invention patent application after publication |