CN215285285U - Unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus - Google Patents
Unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus Download PDFInfo
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- CN215285285U CN215285285U CN202121594327.8U CN202121594327U CN215285285U CN 215285285 U CN215285285 U CN 215285285U CN 202121594327 U CN202121594327 U CN 202121594327U CN 215285285 U CN215285285 U CN 215285285U
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- 230000001681 protective effect Effects 0.000 claims abstract description 23
- 238000005096 rolling process Methods 0.000 claims abstract description 23
- 230000006378 damage Effects 0.000 abstract description 16
- 230000000694 effects Effects 0.000 abstract description 12
- 230000003139 buffering effect Effects 0.000 abstract description 8
- 208000027418 Wounds and injury Diseases 0.000 abstract description 7
- 208000014674 injury Diseases 0.000 abstract description 7
- 230000014759 maintenance of location Effects 0.000 description 7
- 238000003384 imaging method Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000001066 destructive effect Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000011090 solid board Substances 0.000 description 1
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle-mounted synthetic aperture radar data positioning and capturing device, which comprises a machine body; the bottom end of the machine body is fixedly connected with a shell; a protective shell is fixedly connected to the bottom end of the shell; a sliding rail piece is fixedly connected to the inner side wall of the shell; a first elastic rope is fixedly connected to the inner side wall of the shell; a rolling part is fixedly connected to the side end of the first elastic rope; a second elastic rope is fixedly connected to the inner side wall of the top end of the slide rail piece; the sliding block piece is connected to the inner part of the sliding rail piece in a sliding manner; the inner side wall of the sliding rail piece is fixedly connected with a retaining block; a first power connection piece is fixedly connected inside the sliding block piece; a clamping part is fixedly connected to the side end of the sliding block part; thereby roll through the rolling member makes slider spare slip, and the slip of slider spare and then make protection piece take place the inflation, has the effect of buffering when the organism drops on ground to reduce the injury that drops and bring, can improve the protectiveness to the organism through protection piece.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, specific unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus that says so.
Background
The unmanned plane is called as an unmanned plane for short, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device; traditional unmanned aerial vehicle's safeguard measure is simple.
Among the prior art at present, synthetic aperture radar is a high resolution imaging radar, and unmanned aerial vehicle can shoot the work in the high altitude, when unmanned aerial vehicle breaks down and drops suddenly, no matter be radar equipment or unmanned aerial vehicle all be devastating injury to make unmanned aerial vehicle damage, we provide unmanned aerial vehicle and carry synthetic aperture radar data location trapping apparatus here.
SUMMERY OF THE UTILITY MODEL
In order to compensate prior art's not enough, solve among the present prior art, synthetic aperture radar is a high resolution imaging radar, and unmanned aerial vehicle can shoot work in the high altitude, when unmanned aerial vehicle breaks down and drops suddenly, no matter be radar equipment or unmanned aerial vehicle all are devastating injury to make the problem of unmanned aerial vehicle damage, the utility model provides an unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus.
The utility model provides a technical scheme that its technical problem adopted is: the utility model relates to an unmanned aerial vehicle-mounted synthetic aperture radar data positioning and capturing device, which comprises a machine body; the bottom end of the machine body is fixedly connected with a shell; a protective shell is fixedly connected to the bottom end of the shell; a sliding rail piece is fixedly connected to the inner side wall of the shell; a first elastic rope is fixedly connected to the inner side wall of the shell; a rolling part is fixedly connected to the side end of the first elastic rope; a second elastic rope is fixedly connected to the inner side wall of the top end of the slide rail piece; the sliding block piece is connected to the inner part of the sliding rail piece in a sliding manner; the inner side wall of the sliding rail piece is fixedly connected with a retaining block; a first power connection piece is fixedly connected inside the sliding block piece; a clamping part is fixedly connected to the side end of the sliding block part; a second number of power connection pieces are fixedly connected inside the retention block; a clamping groove piece is fixedly connected inside the retaining block; a miniature inflator pump is fixedly connected to the inner side wall of the shell; an air pipe is fixedly connected to the side end of the micro inflator pump; the inside wall rigid coupling of protective housing has the effect that protection piece has the buffering when the organism drops on ground to reduce the injury that drops and bring.
Preferably, a supporting piece is fixedly connected to the inner side wall of the protective shell; a machine fixing groove piece is fixedly connected to the supporting piece; a fixing piece is fixedly connected inside the machine fixing groove piece; radar equipment is installed in the machine fixing groove piece; a clamping plate part is fixedly connected to the side end of the radar equipment; a fixing plate piece is fixedly connected to the side end of the radar equipment; a fixing screw is fixedly connected to the fixing plate; the situation that the radar equipment is loosened when the airplane body works in flight is avoided.
Preferably, a first magnet is fixedly connected to the side end of the retaining block; a second magnet is fixedly connected inside the sliding block piece; the separation when the miniature inflator pump outputs is avoided, and then the protection effect is influenced.
Preferably, one end of the second elastic rope is fixedly connected to the inner side wall of the top end of the sliding rail piece; the other end of the second elastic rope is fixedly connected to the side end of the sliding block piece; the second elastic rope can limit the sliding of the sliding block piece.
Preferably, a limiting piece is fixedly connected to the inner side wall of the slide rail piece; the upper end and the lower end of the clamp plate part are fixedly connected with a fixing part; the sliding block piece is prevented from sliding towards the direction far away from the retaining block.
Preferably, an elastic piece is arranged inside the protective shell; an elastic piece is fixedly connected to the side end of the machine fixing groove piece; the elasticity of the elastic member has a buffering effect when the body falls on the ground.
The utility model has the advantages that:
1. the utility model provides an unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus thereby makes slider spare slip through the roll of rolling member, and the slip of slider spare and then make protection piece take place the inflation, has the effect of buffering when the organism falls on ground to reduce the injury that drops and bring, can improve the protectiveness to the organism through protection piece.
2. The utility model provides an unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus can fix radar equipment in solid quick-witted groove spare through the cooperation of maintenance screw and solid board spare, and the card piece of deuterogamying can make radar equipment fix in solid quick-witted groove spare, avoids the organism to take place not hard up problem at flight during operation radar equipment to avoid not hard up work that influences the seizure.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the invention without undue limitation to the invention. In the drawings:
FIG. 1 is a front view of the first embodiment;
FIG. 2 is a perspective view of the first embodiment;
FIG. 3 is an enlarged view taken at A in FIG. 1;
FIG. 4 is an enlarged view at B in FIG. 3;
FIG. 5 is an enlarged view at C of FIG. 1;
FIG. 6 is a schematic view of another embodiment of the protective shell structure of the first embodiment;
illustration of the drawings:
1. a body; 21. a housing; 22. a protective shell; 231. an elastic rope I; 232. a rolling member; 233. A second elastic rope; 234. a slider member; 235. a retention block; 24. a slide rail member; 251. a signal connecting piece; 252. a clamping piece; 253. the second number is connected with the power strip; 254. a slot member; 261. a micro inflator; 262. an air tube; 263. a protective member; 31. a support member; 32. fixing a machine groove piece; 33. a fixing member; 34. a radar device; 35. a clamp plate member; 36. a fixing plate member; 37. a retention screw; 41. a first magnet; 42. A magnet II; 43. a limiting member; 44. a retention member; 45. an elastic member; 51. a cushion member.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Example one
Referring to fig. 1-5, the data positioning and capturing device for the unmanned aerial vehicle-mounted synthetic aperture radar comprises a body 1; a shell 21 is fixedly connected to the bottom end of the machine body 1; a protective shell 22 is fixedly connected to the bottom end of the shell 21; a sliding rail piece 24 is fixedly connected to the inner side wall of the shell 21; a first elastic rope 231 is fixedly connected to the inner side wall of the shell 21; a rolling element 232 is fixedly connected to the side end of the first elastic rope 231; a second elastic rope 233 is fixedly connected with the inner side wall of the top end of the slide rail piece 24; a slider member 234 is slidably connected to the inside of the slide member 24; a fixing block 235 is fixedly connected to the inner side wall of the slide rail piece 24; a signal connecting piece 251 is fixedly connected inside the sliding block piece 234; a clamping part 252 is fixedly connected to the side end of the sliding block 234; a second electric connecting piece 253 is fixedly connected inside the retaining block 235; a slot clamping piece 254 is fixedly connected inside the retaining block 235; a micro inflator 261 is fixedly connected to the inner side wall of the shell 21; an air pipe 262 is fixedly connected to the side end of the micro air pump 261; a protective piece 263 is fixedly connected to the inner side wall of the protective shell 22; when the aircraft works, when the aircraft body 1 suddenly fails and falls off when flying at high altitude, the aircraft body 1 can incline in high amplitude when falling, so that the rolling piece 232 rolls, the first elastic rope 231 has good elasticity, when the aircraft body 1 flies normally, the first elastic rope 231 can limit the rolling of the rolling piece 232, only when the aircraft body 1 fails and falls off in large amplitude, the rolling piece 232 can roll towards the sliding piece 234, so that the sliding piece 234 is attached to the fixing piece 235 through the thrust of the rolling piece 232, the sliding piece 234 can slide in the sliding rail piece 24, the fixing piece 235 is fixed in the sliding rail piece 24, when the aircraft body 1 flies normally, the second elastic rope 233 can limit the sliding of the sliding piece 234, only when the aircraft body 1 fails and falls off in large amplitude, the sliding piece 234 can be attached to the fixing piece 235 through the thrust of the rolling piece 232, the limiting piece 43 can limit the sliding direction of the sliding piece 234, the sliding block piece 234 is prevented from sliding away from the retaining block 235, the sliding block piece 234 is attached to the retaining block 235, so that the first electric connection piece 251 and the second electric connection piece 253 are attached to each other, the micro inflator 261 starts to output, gas generated by the output of the micro inflator 261 reaches the protection piece 263 through the air pipe 262, the protection piece 263 is made of air bags, the protection piece 263 is expanded due to the gas, the machine body 1 can have a buffering effect when falling on the ground, so that the damage caused by falling is reduced, when the sliding block piece 234 is attached to the retaining block 235, the clamping piece 252 can slide into the clamping groove piece 254, due to the fact that the sliding block piece 234 is pushed strongly, the clamping piece 252 is provided with an uneven rubber body, when the clamping piece 252 slides into the clamping groove piece 254, the clamping piece 252 can be clamped into the clamping groove piece 254, so that the first electric connection piece 251 is firmly attached to the second electric connection piece 253, and the protection effect is prevented from being influenced by the interruption of the micro inflator 261 during output, the first magnet 41 and the second magnet 42 are attracted by the magnets, and when the slider member 234 and the retention block 235 are attached, the first magnet 41 slides into the second magnet 42, so that the first connecting piece 251 and the second connecting piece 253 are firmly fixed together, are prevented from being separated when the micro inflator 261 outputs, further influencing the protection effect, the synthetic aperture radar is a high-resolution imaging radar, an unmanned aerial vehicle can carry out shooting work at high altitude, when the unmanned aerial vehicle breaks down and drops suddenly, both the radar equipment and the unmanned aerial vehicle are destructive injuries, thereby causing the damage of the drone, the sliding of the sliding member 234 by the rolling of the rolling member 232, the sliding of the sliding member 234 and the expansion of the protection member 263, when the drone body 1 falls on the ground, having a cushioning effect, thereby reducing the damage caused by falling and improving the protection of the body 1 by the protection member 263.
A support member 31 is fixedly connected to the inner side wall of the protective shell 22; a machine fixing groove piece 32 is fixedly connected to the supporting piece 31; a fixing piece 33 is fixedly connected inside the machine fixing groove piece 32; a radar device 34 is arranged in the machine fixing groove piece 32; a clamping plate part 35 is fixedly connected to the side end of the radar device 34; a fixing plate piece 36 is fixedly connected to the side end of the radar device 34; a retaining screw 37 is fixedly connected to the fixing plate 36; the support 31 can fix the positions of the protective shell 22 and the machine fixing groove member 32, the protective member 263 wraps the support 31, the work of the protective member 263 cannot be influenced by the support 31, the radar equipment 34 is firstly slid into the machine fixing groove member 32 to be installed during the work, the fixing screw 37 and the fixing member 33 are both provided with threads, the fixing plate member 36 is fixed on the fixing member 33 through the thread matching, so that the radar equipment 34 is fixed on the machine fixing groove member 32, the situation that the radar equipment 34 is loosened during the flight work of the machine body 1 is avoided, the clamping plate member 35 slides into the fixing member 33 along with the radar equipment 34, the upper position and the lower position of the radar equipment 34 can be fixed, the fixing member 44 is made of soft rubber, the elastic material and can also be subjected to micro-deformation, the clamping plate member 35 slides into the fixing member 33 by force to slide the clamping plate member 35 and the fixing member 44 into the fixing member 33, and the fixing member 44 can be extruded and deformed, the resiliency of retaining members 44 causes the card member 35 to be secured within the securing member 33, thereby further securing the card member 35 within the securing member 33.
A first magnet 41 is fixedly connected to the side end of the retaining block 235; a second magnet 42 is fixedly connected inside the sliding block piece 234; first magnet 41 and No. two magnets 42 are because of the magnet absorption together, and when slider spare 234 and maintenance piece 235 laminating together, first magnet 41 can slide in No. two magnets 42 to make No. one connect electric piece 251 and No. two firmly fixed together of connecting electric piece 253, avoid separating when miniature pump 261 outputs, and then influence the protection effect.
One end of the second elastic rope 233 is fixedly connected with the inner side wall of the top end of the slide rail piece 24; the other end of the second elastic rope 233 is fixedly connected with the side end of the sliding block 234; the second elastic cord 233 can limit the sliding of the sliding block 234, when the machine body 1 flies normally, the sliding block 234 will slide along with the flying direction of the machine body 1, the second elastic cord 233 will limit the sliding of the sliding block 234, and when the machine body 1 breaks down, the elasticity of the second elastic cord 233 will make the sliding block 234 and the retention block 235 fit.
A limiting part 43 is fixedly connected to the inner side wall of the slide rail part 24; the upper end and the lower end of the clamp plate part 35 are fixedly connected with a retaining part 44; the limiting member 43 can limit the sliding direction of the sliding block member 234, so as to prevent the sliding block member 234 from sliding away from the retaining block 235, the retaining member 44 is made of soft rubber, has elasticity and can slightly deform, the clamping plate member 35 and the retaining member 44 need to be forced to slide into the fixing member 33 when the clamping plate member 35 slides into the fixing member 33, the retaining member 44 can be extruded and deformed, and the elasticity of the retaining member 44 can fix the clamping plate member 35 in the fixing member 33, so that the clamping plate member 35 is more fixed in the fixing member 33.
An elastic piece 45 is arranged inside the protective shell 22; the side end of the machine fixing groove part 32 is fixedly connected with an elastic part 45; the elastic member 45 has good elasticity, and when the body 1 falls on the ground, the elasticity of the elastic member 45 has a buffering effect, and the protection effect can be improved by matching with the protection member 263.
Example two
Referring to fig. 6, in a first comparative example, as another embodiment of the present invention, the cushion 51 is fixedly connected to the bottom end of the protective shell 22; during operation, the soft pad 51 is made of sponge material, and when the body 1 falls to the ground, the soft pad 51 can play a buffering effect, and the protection capability of the body 1 can be improved by the protection piece 263, so that the damage to the body 1 caused by the falling of the fault can be reduced.
The working principle is as follows: when the aircraft works, when the aircraft body 1 suddenly fails and falls off when flying at high altitude, the aircraft body 1 can incline in high amplitude when falling, so that the rolling piece 232 rolls, the first elastic rope 231 has good elasticity, when the aircraft body 1 flies normally, the first elastic rope 231 can limit the rolling of the rolling piece 232, only when the aircraft body 1 fails and falls off in large amplitude, the rolling piece 232 can roll towards the sliding piece 234, so that the sliding piece 234 is attached to the fixing piece 235 through the thrust of the rolling piece 232, the sliding piece 234 can slide in the sliding rail piece 24, the fixing piece 235 is fixed in the sliding rail piece 24, when the aircraft body 1 flies normally, the second elastic rope 233 can limit the sliding of the sliding piece 234, only when the aircraft body 1 fails and falls off in large amplitude, the sliding piece 234 can be attached to the fixing piece 235 through the thrust of the rolling piece 232, the limiting piece 43 can limit the sliding direction of the sliding piece 234, the sliding block piece 234 is prevented from sliding away from the retaining block 235, the sliding block piece 234 is attached to the retaining block 235, so that the first electric connection piece 251 and the second electric connection piece 253 are attached to each other, the micro inflator 261 starts to output, gas generated by the output of the micro inflator 261 reaches the protection piece 263 through the air pipe 262, the protection piece 263 is made of air bags, the protection piece 263 is expanded due to the gas, the machine body 1 can have a buffering effect when falling on the ground, so that the damage caused by falling is reduced, when the sliding block piece 234 is attached to the retaining block 235, the clamping piece 252 can slide into the clamping groove piece 254, due to the fact that the sliding block piece 234 is pushed strongly, the clamping piece 252 is provided with an uneven rubber body, when the clamping piece 252 slides into the clamping groove piece 254, the clamping piece 252 can be clamped into the clamping groove piece 254, so that the first electric connection piece 251 is firmly attached to the second electric connection piece 253, and the protection effect is prevented from being influenced by the interruption of the micro inflator 261 during output, the first magnet 41 and the second magnet 42 are attracted by the magnets, and when the slider member 234 and the retention block 235 are attached, the first magnet 41 slides into the second magnet 42, so that the first connecting piece 251 and the second connecting piece 253 are firmly fixed together, are prevented from being separated when the micro inflator 261 outputs, further influencing the protection effect, the synthetic aperture radar is a high-resolution imaging radar, an unmanned aerial vehicle can carry out shooting work at high altitude, when the unmanned aerial vehicle breaks down and drops suddenly, both the radar equipment and the unmanned aerial vehicle are destructive injuries, thereby causing the damage of the drone, the sliding of the sliding member 234 by the rolling of the rolling member 232, the sliding of the sliding member 234 and the expansion of the protection member 263, when the drone body 1 falls on the ground, having a cushioning effect, thereby reducing the damage caused by falling, and the protection of the machine body 1 can be improved through the protection piece 263; the support 31 can fix the positions of the protective shell 22 and the machine fixing groove member 32, the protective member 263 wraps the support 31, the work of the protective member 263 cannot be influenced by the support 31, the radar equipment 34 is firstly slid into the machine fixing groove member 32 to be installed during the work, the fixing screws 37 and the fixing members 33 are provided with threads, the fixing plate members 36 are fixed on the fixing members 33 through the thread matching, so that the radar equipment 34 is fixed on the machine fixing groove member 32, the situation that the radar equipment 34 is loosened during the flight work of the machine body 1 is avoided, the clamping plate members 35 slide into the fixing members 33 along with the radar equipment 34, the upper and lower positions of the radar equipment 34 can be fixed, the fixing members 44 are made of soft rubber materials, the elastic property and the micro-deformation can be generated, the clamping plate members 35 slide into the fixing members 33 forcibly to slide the clamping plate members 35 and the fixing members 44 into the fixing members 33, and the fixing members 44 can be extruded and deformed, the resiliency of retaining members 44 causes the card member 35 to be secured within the securing member 33, thereby further securing the card member 35 within the securing member 33.
In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention.
Claims (6)
1. Unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus, its characterized in that: comprises a machine body (1); a shell (21) is fixedly connected to the bottom end of the machine body (1); a protective shell (22) is fixedly connected to the bottom end of the shell (21); a sliding rail piece (24) is fixedly connected to the inner side wall of the shell (21); a first elastic rope (231) is fixedly connected to the inner side wall of the shell (21); a rolling element (232) is fixedly connected to the side end of the first elastic rope (231); a second elastic rope (233) is fixedly connected with the inner side wall of the top end of the slide rail piece (24); a sliding block piece (234) is connected inside the sliding rail piece (24) in a sliding way; a fixing block (235) is fixedly connected to the inner side wall of the sliding rail piece (24); a signal connecting piece (251) is fixedly connected inside the sliding block piece (234); a clamping part (252) is fixedly connected to the side end of the sliding block part (234); a second number connecting piece (253) is fixedly connected inside the retaining block (235); a clamping groove piece (254) is fixedly connected inside the retaining block (235); a micro inflator pump (261) is fixedly connected to the inner side wall of the shell (21); an air pipe (262) is fixedly connected with the side end of the micro air pump (261); and a protection piece (263) is fixedly connected to the inner side wall of the protection shell (22).
2. The unmanned airborne synthetic aperture radar data positioning capture device of claim 1, wherein: a support piece (31) is fixedly connected to the inner side wall of the protective shell (22); a machine fixing groove piece (32) is fixedly connected to the supporting piece (31); a fixing piece (33) is fixedly connected inside the machine fixing groove piece (32); radar equipment (34) is installed in the machine fixing groove piece (32); a clamping plate part (35) is fixedly connected to the side end of the radar device (34); a fixing plate piece (36) is fixedly connected to the side end of the radar equipment (34); a fixing screw (37) is fixedly connected to the fixing plate piece (36).
3. The unmanned airborne synthetic aperture radar data positioning capture device of claim 2, wherein: a first magnet (41) is fixedly connected to the side end of the retaining block (235); and a second magnet (42) is fixedly connected inside the sliding block piece (234).
4. The unmanned airborne synthetic aperture radar data positioning capture device of claim 3, wherein: one end of the second elastic rope (233) is fixedly connected with the inner side wall of the top end of the sliding rail piece (24); the other end of the second elastic rope (233) is fixedly connected with the side end of the sliding block piece (234).
5. The UAV data location capture device of claim 4, wherein: a limiting piece (43) is fixedly connected to the inner side wall of the slide rail piece (24); and the upper end and the lower end of the clamp plate part (35) are fixedly connected with a retaining part (44).
6. The unmanned airborne synthetic aperture radar data positioning capture device of claim 5, wherein: an elastic piece (45) is arranged inside the protective shell (22); the side end of the machine fixing groove piece (32) is fixedly connected with an elastic piece (45).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121594327.8U CN215285285U (en) | 2021-07-13 | 2021-07-13 | Unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121594327.8U CN215285285U (en) | 2021-07-13 | 2021-07-13 | Unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215285285U true CN215285285U (en) | 2021-12-24 |
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ID=79522518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121594327.8U Expired - Fee Related CN215285285U (en) | 2021-07-13 | 2021-07-13 | Unmanned aerial vehicle carries synthetic aperture radar data location trapping apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215285285U (en) |
-
2021
- 2021-07-13 CN CN202121594327.8U patent/CN215285285U/en not_active Expired - Fee Related
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Granted publication date: 20211224 |