CN214824194U - Flight type radar life detection instrument - Google Patents
Flight type radar life detection instrument Download PDFInfo
- Publication number
- CN214824194U CN214824194U CN202120907241.XU CN202120907241U CN214824194U CN 214824194 U CN214824194 U CN 214824194U CN 202120907241 U CN202120907241 U CN 202120907241U CN 214824194 U CN214824194 U CN 214824194U
- Authority
- CN
- China
- Prior art keywords
- fixed
- detection instrument
- inserted block
- instrument body
- aircraft
- 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
Links
Images
Landscapes
- Geophysics And Detection Of Objects (AREA)
Abstract
The application relates to a flight type radar life detection instrument, including the detection instrument body, be provided with the aircraft on the detection instrument body, be provided with connecting device between aircraft and the detection instrument body, connecting device is including connecting the platform and connecting the inserted block, it has two and all sets up at aircraft towards detection instrument body one side to connect the platform, connect the inserted block and insert and establish between two connection platforms, connect the inserted block and set up in detection instrument body towards aircraft one side. This application has and drives the detection instrument body through the aircraft and surveys in the space to avoid the road and the house of collapse, reduce the effect of the road of collapse and the performance of house restriction radar life detection instrument.
Description
Technical Field
The application relates to the field of rescue equipment, in particular to a flight type radar life detection instrument.
Background
The radar life detection instrument is high-tech lifesaving equipment which is developed by integrating a micropower ultra-wideband radar technology and a biomedical engineering technology, is specially used for emergency rescue tasks such as earthquake disasters, collapse accidents and the like, and effectively improves the rescue quality and the working efficiency; the working principle of the radar detection device is that whether life bodies exist in the ruins and specific position information of the life bodies are obtained through analysis and judgment based on the time domain Doppler effect generated by human body movement on radar echoes.
The traditional Chinese utility model with the publication number of CN208399678U discloses a radar life detector, which comprises a detector body (1), wherein two height adjusting assemblies (2) are fixed on one opposite side of the detector body (1); the two height adjusting components (2) are rotationally matched with a limiting component (4); the height adjusting assembly (2) comprises a rectangular connecting guide post (3); one end face of the rectangular connecting guide post (3) is provided with a first guide round hole (301); an inner wall of the first guide round hole (301) is hinged with an electric telescopic rod (5) through a first hinged support; the other end of the electric telescopic rod (5) is hinged with an end cover (11) through a second hinged support; the peripheral side surface of one end of the end cover (11) is in threaded connection with a leveling column guide cylinder (6); a first notch (601) is formed in the peripheral side surface of the leveling column guide cylinder (6); two fixed short shafts (602) are fixed on the peripheral side surface of the leveling column guide cylinder (6); the peripheral side surface of the leveling column guide cylinder (6) is in sliding fit with the inner wall of the first guide round hole (301); the inner wall of the first guide round hole (301) is in sliding fit with a leveling column (7); annular grooves (701) are axially arranged on the peripheral side surface of the leveling column (7); one end of the leveling column (7) is fixed with a cross universal joint (8) through a first screw; the other end of the cross universal joint (8) is fixed with a base plate (9) through a second screw; the limiting assembly (4) comprises a control rod (401); two end faces of the control rod (401) are respectively fixed with a U-shaped frame (402); a limiting plate (403) is fixed on one side surface of the U-shaped frame (402); one end of the limiting plate (403) is matched with the annular groove (701); a first through hole (405) is formed in one side face of the U-shaped frame (402); the first through hole (405) is in rotating fit with the fixed short shaft (602).
In view of the above-mentioned related art, the inventor believes that a collapsed road and house may occur after an earthquake, and it is difficult to walk on the collapsed road and house, thereby limiting the performance of the radar life detection device.
SUMMERY OF THE UTILITY MODEL
In order to reduce the exertion of collapsed road and house limit radar life detection instruments, the application provides a flight type radar life detection instrument.
The application provides a flight formula radar life detection instrument adopts following technical scheme:
the utility model provides a flight type radar life detection instrument, includes the detection instrument body, be provided with the aircraft on the detection instrument body, be provided with connecting device between aircraft and the detection instrument body, connecting device is including connecting the platform and connecting the inserted block, connect the platform have two and all set up at aircraft towards detection instrument body one side, connect the inserted block and insert and establish between two connection platforms, connect the inserted block and set up in detection instrument body towards aircraft one side.
By adopting the technical scheme, the detecting instrument body is driven by the aircraft to detect in space, so that a collapsed road and a collapsed house are avoided, and the collapsed road and the collapsed house are reduced to limit the radar life detecting instrument.
Optionally, connect the platform and include vertical board and horizontal plate, vertical board width direction one end sets firmly at the aircraft towards detection instrument body one side, the horizontal plate sets firmly at the vertical board width direction other end, and the vertical board of two sets of connection platforms is respectively in connecting the inserted block width direction butt on connecting the inserted block, and the equal butt of horizontal plate of two sets of connection platforms deviates from aircraft one end in connecting the inserted block.
Through adopting above-mentioned technical scheme, vertical board and horizontal plate butt respectively are at the lateral wall and the diapire of connecting the inserted block to the realization is to connecting the fixed of inserted block.
Optionally, the aircraft is fixed with the baffle towards detection instrument body one end, the baffle sets firmly in vertical board length direction one end, and the baffle butt is in connecting inserted block length direction one end.
Through adopting above-mentioned technical scheme, the setting of baffle can restrict the slip of connecting the inserted block to reduce the probability that connects the inserted block and break away from connecting the bench.
Optionally, be provided with fixed subassembly between vertical board and the connection inserted block, fixed subassembly includes fixed spout, fixed inserted block, fixed spring and fixed slot, fixed spout is seted up and is being connected inserted block width direction one end, fixed inserted block slides and sets up in fixed spout, fixed spring places in fixed spout, and fixed spring one end sets firmly in the fixed spout tank bottom, and the other end sets firmly in fixed inserted block towards fixed spout bottom one end, fixed slot sets up on vertical board, and fixed spring drives fixed inserted block and inserts and locate in the fixed slot.
Through adopting above-mentioned technical scheme, fixed subassembly set up can make the more stable fixing of connecting the inserted block connect the bench to reduce and connect the inserted block and receive the probability that external force influences and break away from the connection platform.
Optionally, the fixing slot penetrates through the vertical plate, and the fixing insert penetrates through the vertical plate through the fixing slot.
Through adopting above-mentioned technical scheme, fixed inserted block runs through fixed slot and can conveniently drive fixed inserted block and break away from fixed slot to the dismantlement of inserted block is conveniently connected.
Optionally, a connecting piece is arranged between the connecting plug block and the detecting instrument body, the detecting instrument body is connected with the connecting plug block through the connecting piece, one end of the connecting piece is fixed at one end, facing the aircraft, of the detecting instrument body, and the other end of the connecting piece is arranged on the connecting plug block in a universal rotating mode.
Through adopting above-mentioned technical scheme, the connecting piece makes connection plug block and detection instrument body link to each other to realize the universal rotation of detection instrument body on connecting the plug block, thereby adjust the angle of surveying.
Optionally, the connecting piece includes spliced pole and connecting ball, spliced pole one end sets firmly on the detection instrument body, the connecting ball sets firmly and keeps away from detection instrument body one end at the spliced pole, and the universal rotation of connecting ball sets up on connecting the inserted block.
Through adopting above-mentioned technical scheme, the universal regulation of detection instrument body on connecting the inserted block has been realized to the connecting ball cooperation spliced pole.
Optionally, one end of the detecting instrument body, which is far away from the aircraft, is provided with a balancing weight.
Through adopting above-mentioned technical scheme, setting up of balancing weight can make the detection instrument body perpendicular orientation ground all the time to reduce the probability that detection instrument body skew leads to surveying the appearance deviation.
In summary, the present application includes at least one of the following beneficial technical effects:
the detector body is driven by the aircraft to detect in space, so that collapsed roads and houses are avoided, and the collapse roads and houses are reduced to limit the radar life detector;
the vertical plate and the horizontal plate are respectively abutted against the side wall and the bottom wall of the connecting plug block, so that the connecting plug block is fixed;
the arrangement of the fixing component can enable the connecting plug block to be more stably fixed on the connecting table, so that the probability that the connecting plug block is separated from the connecting table under the influence of external force is reduced;
the connecting piece enables the connecting plug block to be connected with the detector body, and the detector body can rotate on the connecting plug block in a universal mode, so that the detection angle can be adjusted;
the universal adjustment of the detector body on the connecting plug block is realized by matching the connecting ball with the connecting column.
Drawings
Fig. 1 is a schematic view of the overall structure of the present embodiment.
Fig. 2 is a partial sectional view of the present embodiment.
Fig. 3 is an enlarged view of a portion a in fig. 2.
Description of reference numerals: 1. a detector body; 2. an aircraft; 3. a connecting device; 31. a connecting table; 311. a vertical plate; 312. a horizontal plate; 32. connecting the plug blocks; 4. a baffle plate; 5. a fixing assembly; 51. fixing the chute; 52. fixing the insert block; 53. fixing the spring; 54. fixing the slot; 6. a connecting member; 61. connecting columns; 62. a connecting ball; 7. and a balancing weight.
Detailed Description
The present application is described in further detail below with reference to figures 1-3.
The embodiment of the application discloses a flying type radar life detection instrument, which comprises a detection instrument body 1, wherein a storage battery, a radar transmitter, a signal receiver, a signal analyzer and a wireless transmitter are arranged in the detection instrument body 1, the radar transmitter transmits radar signals, the signal receiver receives the returned radar signals, the signal analyzer analyzes the received radar signals to distinguish whether people buried in ruins exist or not, the wireless transmitter transmits the analyzed information to terminals such as a computer and the like, the storage battery is used for storing power supplies for electric appliances, an aircraft 2 is arranged on the detection instrument body 1, the aircraft 2 is an unmanned aerial vehicle, a connecting device 3 is arranged between the aircraft 2 and the detection instrument body 1, the connecting device 3 comprises two connecting platforms 31 and connecting plug blocks 32, the two connecting platforms 31 are respectively arranged on one side of the aircraft 2 facing the detection instrument body 1, the connecting plug blocks 32 are inserted between the two connecting platforms 31, the connection plug block 32 is arranged on one side, facing the aircraft 2, of the detector body 1, and the aircraft 2 drives the detector body 1 to detect in space, so that a collapsed road and a house are avoided, and the collapsed road and the house are reduced to limit the performance of the radar life detector.
Referring to fig. 1 and 2, the connection table 31 includes a vertical plate 311 and a horizontal plate 312, one end of the vertical plate 311 in the width direction is fixedly arranged on one side of the aircraft 2 facing the detector body 1, the horizontal plate 312 is fixedly arranged on the other end of the vertical plate 311 in the width direction, the vertical plates 311 of the two groups of connection tables 31 abut against the connection insert blocks 32 in the width direction of the connection insert blocks 32, and the horizontal plates 312 of the two groups of connection tables 31 abut against one end of the connection insert blocks 32 away from the aircraft 2; aircraft 2 is fixed with baffle 4 towards 1 one end of detection instrument body, and baffle 4 sets firmly in vertical board 311 length direction one end, and 4 butt of baffle are connecting inserted block 32 length direction one end, and baffle 4's setting can reduce and connect inserted block 32 and break away from directly from leading one end when inserting, connects inserted block 32 and does not be provided with baffle 4 one end from vertical board 311 length direction and inserts or break away from and connect platform 31 to the installation or the dismantlement of inserted block are linked in the realization.
Referring to fig. 2 and 3, two groups of fixing assemblies 5 are arranged between the vertical plate 311 and the connecting insert block 32, the two groups of fixing assemblies 5 are respectively arranged at two ends of the two vertical plates and the two ends of the connecting insert block 32 in the width direction, each fixing assembly 5 comprises a fixing chute 51 arranged at one end of the connecting insert block 32 in the width direction, a fixing insert block 52 arranged in the fixing chute 51 in a sliding manner, a fixing spring 53 arranged in the fixing chute 51 and a fixing slot 54 arranged on the vertical plate 311, one end of the fixing spring 53 is fixedly arranged at the bottom of the fixing chute 51, the other end of the fixing spring 53 is fixedly arranged at one end, facing the bottom of the fixing chute 51, of the fixing insert block 52, and the fixing spring 53 drives the fixing insert block 52 to be inserted into the fixing slot 54; fixed slot 54 runs through vertical board 311, fixed inserted block 52 runs through vertical board 311 through fixed slot 54, the wedge-face has been seted up towards connecting inserted block 32 length direction one end to fixed inserted block 52, the vertical board 311 of wedge-face butt makes fixed inserted block 52 slide and extrude fixed spring 53 towards fixed slot 51 tank bottom direction, conveniently connect inserted block 32 and insert between two connection platforms 31, after connecting block butt baffle 4, fixed inserted block 52 aligns with fixed slot 54, fixed inserted block 52 slides through fixed spring 53's resilience and inserts and locate in fixed slot 54, accomplish the reinforcement of connecting inserted block 32, when needs demolish connecting inserted block 32, promote fixed inserted block 52 through the hole that runs through vertical board 311, make fixed inserted block 52 break away from fixed slot 54, thereby make connecting inserted block 32 can quick convenient dismantlement.
Referring to fig. 2 and 3, a connecting piece 6 is arranged between the connecting plug block 32 and the detecting instrument body 1, the detecting instrument body 1 is connected with the connecting plug block 32 through the connecting piece 6, one end of the connecting piece 6 is fixed at one end of the detecting instrument body 1 facing the aircraft 2, and the other end of the connecting piece is arranged on the connecting plug block 32 in a universal rotation manner; the connecting piece 6 comprises a connecting column 61 with one end fixedly arranged on the detecting instrument body 1 through a bolt and a connecting ball 62 integrally formed and fixedly arranged at one end of the connecting column 61 far away from the detecting instrument body 1, and the connecting ball 62 is arranged on the connecting plug block 32 in a universal rotation manner; detection instrument body 1 deviates from 2 one ends of aircraft and is provided with balancing weight 7, and balancing weight 7 is the rectangle iron plate, and balancing weight 7 has the stone to dismantle through rope and knocker respectively and connect in 1 four corners department of detection instrument body, and balancing weight 7 cooperates universal pivoted detection instrument body 1 can make detection instrument body 1 perpendicular to ground all the time to reduce detection instrument body 1 and rotate the precision that the skew influences the detection result.
The implementation principle of the embodiment of the application is as follows: installing the balancing weight 7 on the detector body 1, and then fixedly arranging the connecting column 61 on the detector body 1 through a bolt; the connecting ball 62 is mounted on the connecting plug 32, then the connecting plug 32 is inserted into the connecting table 31, the connection between the probe body 1 and the aircraft 2 is completed, and then the aircraft 2 is started to carry the probe body 1 to detect the ground.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (8)
1. A flight type radar life detection instrument, includes detection instrument body (1), its characterized in that: be provided with aircraft (2) on detection instrument body (1), be provided with connecting device (3) between aircraft (2) and detection instrument body (1), connecting device (3) are including connecting platform (31) and connecting inserted block (32), connect platform (31) have two and all set up at aircraft (2) towards detection instrument body (1) one side, connect inserted block (32) and insert and establish between two connection platforms (31), connect inserted block (32) and set up in detection instrument body (1) towards aircraft (2) one side.
2. The flying radar life detector of claim 1, wherein: connect platform (31) including vertical board (311) and horizontal plate (312), vertical board (311) width direction one end sets firmly in aircraft (2) towards detection instrument body (1) one side, horizontal plate (312) sets firmly at vertical board (311) width direction other end, and vertical board (311) of two sets of connection platforms (31) are respectively in connecting inserted block (32) width direction butt on connecting inserted block (32), and horizontal plate (312) of two sets of connection platforms (31) all butt in connecting inserted block (32) and deviating from aircraft (2) one end.
3. A flying radar life detector as claimed in claim 2, wherein: aircraft (2) are fixed with baffle (4) towards detection instrument body (1) one end, baffle (4) set firmly in vertical board (311) length direction one end, and baffle (4) butt is in connecting plug block (32) length direction one end.
4. A flying radar life detector as claimed in claim 3, wherein: be provided with between vertical board (311) and the connection inserted block (32) fixed subassembly (5), fixed subassembly (5) are including fixed spout (51), fixed inserted block (52), fixed spring (53) and fixed slot (54), set up in connection inserted block (32) width direction one end fixed spout (51), fixed inserted block (52) slide and set up in fixed spout (51), place in fixed spout (51) fixed spring (53), and fixed spring (53) one end sets firmly in fixed spout (51) tank bottom, and the other end sets firmly in fixed inserted block (52) towards fixed spout (51) bottom one end, set up on vertical board (311) fixed slot (54), and fixed spring (53) drive fixed inserted block (52) are inserted and are located in fixed slot (54).
5. The flying radar life detector of claim 4, wherein: the fixing slot (54) penetrates through the vertical plate (311), and the fixing insertion block (52) penetrates through the vertical plate (311) through the fixing slot (54).
6. The flying radar life detector of claim 1, wherein: be provided with connecting piece (6) between connection inserted block (32) and detection instrument body (1), detection instrument body (1) passes through connecting piece (6) and is connected inserted block (32) interconnect, and connecting piece (6) one end is fixed at detection instrument body (1) towards aircraft (2) one end, connects even the universal rotation setting of the other end on connecting inserted block (32).
7. The flying radar life detector of claim 6, wherein: connecting piece (6) are including spliced pole (61) and connection ball (62), spliced pole (61) one end sets firmly on detection instrument body (1), connect ball (62) and set firmly and keep away from detection instrument body (1) one end at spliced pole (61), connect ball (62) universal rotation and set up on connecting inserted block (32).
8. The flying radar life detector of claim 7, wherein: one end, deviating from the aircraft (2), of the detecting instrument body (1) is provided with a balancing weight (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120907241.XU CN214824194U (en) | 2021-04-28 | 2021-04-28 | Flight type radar life detection instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120907241.XU CN214824194U (en) | 2021-04-28 | 2021-04-28 | Flight type radar life detection instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214824194U true CN214824194U (en) | 2021-11-23 |
Family
ID=78770027
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120907241.XU Active CN214824194U (en) | 2021-04-28 | 2021-04-28 | Flight type radar life detection instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214824194U (en) |
-
2021
- 2021-04-28 CN CN202120907241.XU patent/CN214824194U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN214824194U (en) | Flight type radar life detection instrument | |
| CN109484630B (en) | A multidirectional survey and drawing is with erectting support for complicated topography | |
| CN112033357B (en) | Leveling-free polygon prism measuring device and method for triangulation elevation measurement | |
| CN210689648U (en) | Protective total station | |
| CN204228167U (en) | Flip chip type fiber gyro north seeker | |
| CN115824158A (en) | Slope measuring instrument for natural resource surveying | |
| KR102272683B1 (en) | Underground facility confirmation management system | |
| CN211877005U (en) | Hand-held type laser range finder | |
| CN214225160U (en) | Tripod for geological exploration | |
| CN212929383U (en) | Novel adjustable total powerstation support | |
| KR102271037B1 (en) | Geodetic survey system for underground facilities according to topographic change by reference point | |
| CN214839804U (en) | Remote sensing location marking device for surveying and mapping | |
| CN112393718A (en) | Azimuth angle measuring device and method for building construction | |
| CN211118367U (en) | Construction is measured and is surveyed and use fixed point device | |
| CN210221080U (en) | Unmanned aerial vehicle measuring equipment and system integrated with depth camera | |
| CN208506251U (en) | A kind of laser range finder of mountainous region construction rescue | |
| CN212672756U (en) | Anti-shaking compass for mine measurement | |
| CN217083745U (en) | Accurate detection device of bent cap surface roughness | |
| CN212903003U (en) | Device for measuring geotechnical geological investigation depth | |
| CN214308769U (en) | Multi-terrain surveying instrument | |
| CN218098775U (en) | Mining dust instrument | |
| CN210953790U (en) | Remote sensing based yellow substance remote sensing inversion analysis device | |
| CN213088081U (en) | Tunnel engineering surveys device with big dipper location | |
| CN213240503U (en) | Portable radar detector | |
| CN220221172U (en) | Horizontal take-off platform for unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |