CN216375045U - Novel land surveying and mapping aviation device - Google Patents
Novel land surveying and mapping aviation device Download PDFInfo
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- CN216375045U CN216375045U CN202122570150.4U CN202122570150U CN216375045U CN 216375045 U CN216375045 U CN 216375045U CN 202122570150 U CN202122570150 U CN 202122570150U CN 216375045 U CN216375045 U CN 216375045U
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- 238000013507 mapping Methods 0.000 title claims abstract description 34
- 230000000694 effects Effects 0.000 claims description 13
- 238000004080 punching Methods 0.000 claims description 11
- 230000005484 gravity Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 8
- 230000008569 process Effects 0.000 description 7
- 230000009471 action Effects 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a novel land surveying and mapping aviation device, which comprises a machine head and a machine body, wherein the machine head is fixedly arranged at one end of the machine body, two pairs of frame rods are symmetrically fixed on the outer walls of the two sides of the machine head and the machine body, one end of each frame rod is provided with a wing, a retraction groove is formed in the machine head, a high-definition surveying and mapping camera is arranged in the retraction groove, a stamping assembly and a steering assembly are arranged at the bottom of the machine head, the floor rod is pressed downwards under the additional holding of the device by the gravity and inertia, a movable support rod is pushed by the floor rod, the machine head moves downwards by stamping, a rack moves upwards relative to the machine head in a limiting sliding groove, and the high-definition surveying and mapping camera rotates clockwise around a fixed shaft rod and retracts in the retraction groove through the meshing relationship of a full gear, a rack and a half gear, meanwhile, the impact pressure can be buffered, and the stable falling of the equipment is kept.
Description
Technical Field
The utility model belongs to the technical field related to land surveying and mapping, and particularly relates to a novel aviation device for land surveying and mapping.
Background
In traditional homeland survey and drawing application, compare satellite image, the image that unmanned aerial vehicle acquireed has removed the resolution ratio higher, consequently unmanned aerial vehicle's application is very extensive in survey and drawing application.
The prior art of the land mapping aviation device has the following problems: traditional ground survey and drawing aviation device is falling to the ground the in-process, because the dead weight of fuselage and the impulsive force when descending very easily cause the damage of landing pole, cause camera and inside components and parts to receive the striking damage and influence the use, the camera need just can accomplish through plus actuating mechanism in addition and receive and release, needs extra consumption electric power, influences the duration of equipment.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a novel land surveying and mapping aviation device to solve the problems of collision damage and influence on equipment endurance in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a novel land survey and drawing aviation device, includes aircraft nose and fuselage, aircraft nose fixed mounting is in the one end of fuselage, the symmetry is fixed with two pairs of hack levers on the both sides outer wall of aircraft nose and fuselage, the wing is installed to the one end of hack lever, the inside of aircraft nose has been seted up and has been receive and release the groove, receive and release and be provided with high definition survey and drawing camera in the groove, the bottom of aircraft nose is provided with the punching press subassembly, the bottom of aircraft nose still is provided with and is used for cooperating the punching press subassembly to make high definition survey and drawing camera auto-eject or shrink the subassembly that turns to in receiving and releasing the groove.
Preferably, the punching press subassembly includes the floor pole, the intermediate position fixedly connected with movable branch's of floor pole one end, movable branch's the other end and aircraft nose sliding connection, fixedly connected with and the fixed diaphragm of movable branch direction vertically on movable branch's the outer wall.
Preferably, the outside cover of activity branch is equipped with the spring, the one end and the fixed diaphragm fixed connection of spring, the other end and the diapire fixed connection of aircraft nose of spring.
Preferably, the steering assembly comprises a rack, the rack is vertically fixed on the upper surface of the middle position of the fixed transverse plate, a limiting sliding groove is further formed in the machine head, and the rack is connected with the limiting sliding groove in a sliding mode.
Preferably, a fixed block is arranged between the limiting sliding groove and the retracting groove, the fixed block is fixedly connected with the inner wall of the machine head, a fixed support is fixedly connected to the lower end face of the fixed block, a complete gear is rotatably connected to the fixed support, and the complete gear is meshed with the rack.
Preferably, one end of the high-definition mapping camera is symmetrically fixed with two fixing clamp plates, a fixing shaft rod is fixedly connected between the two fixing clamp plates, two ends of the fixing shaft rod are rotatably connected with the inner wall of the retraction groove, a half gear is fixedly connected to the middle position of the fixing shaft rod, and the half gear is meshed with the complete gear.
Compared with the prior art of the land surveying and mapping aviation device, the utility model provides a novel land surveying and mapping aviation device, which has the following beneficial effects:
1. according to the utility model, the punching component and the steering component are arranged at the bottom of the machine head, the floor rod is pressed down under the action of the gravity and inertia of the device, the movable support rod is pushed by the floor rod, the machine head moves downwards by punching downwards, the rack moves upwards in the limiting chute relative to the machine head, the complete gear rotates anticlockwise through the meshing relation between the rack and the complete gear, the half gear rotates clockwise through the meshing relation between the complete gear and the half gear, and the high-definition surveying and mapping camera rotates clockwise around the fixed shaft rod as an axis and contracts into the retraction groove;
2. in the take-off process of the device, the fixed transverse plate is driven to move downwards by the elastic force of the spring, the fixed transverse plate is provided with the movable support rod and the movable rack which extends downwards to form the limiting chute, the complete gear rotates anticlockwise in the process through the meshing relation of the rack and the complete gear, and the high-definition mapping camera automatically pops out of the retraction groove by rotating anticlockwise around the fixed shaft rod as an axis, so that the irradiation direction of the high-definition mapping camera is inclined downwards for mapping, the expansion of the camera can be completed without increasing a driving mechanism, the electric power is saved, and the endurance time of the device is increased.
Drawings
The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the principles of the utility model without limiting the utility model in which:
fig. 1 is a schematic view of a novel land surveying and mapping aerial device provided by the utility model;
FIG. 2 is a schematic view of a front view of a handpiece according to the present invention;
FIG. 3 is a side view of a partial cross-sectional structure of a handpiece according to the present invention;
FIG. 4 is an enlarged view of a portion A of FIG. 3 according to the present invention;
in the figure: 1. a machine head; 2. a body; 3. a frame bar; 4. an airfoil; 5. a steering assembly; 6. a stamping assembly; 7. a high-definition mapping camera; 8. a retraction slot; 9. a limiting chute; 51. a rack; 52. a fixed support; 53. a fixed block; 54. a half gear; 55. fixing the shaft lever; 56. a full gear; 61. a floor pole; 62. a movable strut; 63. fixing the transverse plate; 64. a spring; 71. and fixing the splint.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a novel land survey and drawing aviation device, including aircraft nose 1 and fuselage 2, 1 fixed mounting of aircraft nose is in the one end of fuselage 2, the symmetry is fixed with two pairs of hack levers 3 on the both sides outer wall of aircraft nose 1 and fuselage 2, wing 4 is installed to the one end of hack lever 3, through the rotatory power that produces of wing 4, it is stable to keep flying aloft, and set up in the inside of aircraft nose 1 and receive and release groove 8, receive and release and be provided with high definition mapping camera 7 in the groove 8, the device is on the way of flying, can carry out image shooting and record the video by high definition mapping camera 7, and then survey and draw the shape appearance of land.
It should be noted that, the bottom of aircraft nose 1 is provided with punching press subassembly 6, punching press subassembly 6 includes floor pole 61, the one end of the intermediate position fixedly connected with activity branch 62 of floor pole 61, the other end and the aircraft nose 1 sliding connection of activity branch 62, fixedly connected with and activity branch 62 direction vertically fixed diaphragm 63 on the outer wall of activity branch 62, the outside cover of activity branch 62 is equipped with spring 64, the one end and the fixed diaphragm 63 fixed connection of spring 64, the other end and the diapire fixed connection of aircraft nose 1 of spring 64, when the device falls to the ground, because the device self gravity adds down, push down floor pole 61, by floor pole 61 top activity branch 62, and then extrude spring 64.
It is worth understanding that the bottom of the machine head 1 is further provided with a steering assembly 5 which is used for being matched with the stamping assembly 6 to enable the high-definition mapping camera 7 to automatically pop up or shrink in the retraction groove 8, the steering assembly 5 comprises a rack 51, the rack 51 is vertically fixed on the upper surface of the middle position of the fixed transverse plate 63, the inside of the machine head 1 is further provided with a limiting sliding groove 9, the rack 51 is connected with the limiting sliding groove 9 in a sliding mode, the machine head 1 moves downwards due to inertia and gravity action after falling to the ground, and the rack 51 moves upwards in the limiting sliding groove 9 relative to the machine head 1.
It should be noted that a fixing block 53 is arranged between the limiting chute 9 and the retraction slot 8, the fixing block 53 is fixedly connected with the inner wall of the handpiece 1, a fixing support 52 is fixedly connected with the lower end face of the fixing block 53, a complete gear 56 is rotatably connected with the fixing support 52, the complete gear 56 is meshed with the rack 51, two fixing splints 71 are symmetrically fixed at one end of the high-definition surveying and mapping camera 7, a fixing shaft rod 55 is fixedly connected between the two fixing splints 71, two ends of the fixing shaft rod 55 are rotatably connected with the inner wall of the retraction slot 8, a half gear 54 is fixedly connected with the middle position of the fixing shaft rod 55, the half gear 54 is meshed with the complete gear 56, when the rack 51 moves upwards in the limiting chute 9, the complete gear 56 rotates anticlockwise through the meshing relationship between the rack 51 and the complete gear 56, through the meshing relationship between the complete gear 56 and the half gear 54, the half gear 54 is rotated clockwise, and then the high-definition mapping camera 7 is rotated clockwise around the fixed shaft rod 55 as an axis and is retracted in the retraction groove 8.
The working principle and the using process of the utility model are as follows: during taking off, the wing 4 rotates to generate power, the flight stability is kept in the air, and the device can be used for shooting images and recording videos by a high-definition mapping camera 7 in the flight process so as to map the shape and appearance of the land;
in the take-off process, the fixed transverse plate 63 is under the elastic force action of the spring 64 to drive the movable support rod 62 to move downwards, meanwhile, the fixed transverse plate 63 drives the rack 51 to extend downwards out of the limiting chute 9, in the process, the complete gear rotates anticlockwise through the meshing relation of the rack 51 and the complete gear 56, so that the high-definition surveying and mapping camera 7 automatically pops out of the retraction groove 8 by rotating anticlockwise around the fixed shaft rod 55 as an axis, and the irradiation direction of the high-definition surveying and mapping camera 7 is inclined downwards to perform surveying and mapping;
in the descending process, because device self gravity and inertia add under holding, press down floor pole 61, by floor pole 61 top activity branch 62, the downward punching press makes aircraft nose 1 downstream, rack 51 is for aircraft nose 1 in to spacing spout 9 up-movement, through the meshing relation of rack 51 and complete gear 56, make complete gear 56 anticlockwise rotation, through the meshing relation of complete gear 56 and half-gear 54, make half-gear 54 clockwise rotation, and then make high definition survey and drawing camera 7 round fixed axostylus axostyle 55 for the axle center clockwise rotation and shrink in receiving and releasing groove 8, play the guard action to high definition survey and drawing camera 7.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a novel land surveying and mapping aviation device, includes aircraft nose (1) and fuselage (2), aircraft nose (1) fixed mounting is in the one end of fuselage (2), the symmetry is fixed with two pairs of hack levers (3) on the both sides outer wall of aircraft nose (1) and fuselage (2), wing (4), its characterized in that are installed to the one end of hack lever (3): the inside of aircraft nose (1) has been seted up and has been receive and release groove (8), receive and release and be provided with high definition survey and drawing camera (7) in groove (8), the bottom of aircraft nose (1) is provided with punching press subassembly (6), the bottom of aircraft nose (1) still is provided with and is used for cooperation punching press subassembly (6) to make high definition survey and drawing camera (7) auto-eject or shrink turn to subassembly (5) in receiving and releasing groove (8).
2. A novel ground mapping aviation device as claimed in claim 1, wherein: punching press subassembly (6) include floor pole (61), the one end of the intermediate position fixedly connected with activity branch (62) of floor pole (61), the other end and aircraft nose (1) sliding connection of activity branch (62), fixedly connected with and activity branch (62) direction vertically fixed diaphragm (63) on the outer wall of activity branch (62).
3. A novel ground mapping aviation device as claimed in claim 2, characterized in that: the outside cover of activity branch (62) is equipped with spring (64), the one end and the fixed diaphragm (63) fixed connection of spring (64), the other end and the diapire fixed connection of aircraft nose (1) of spring (64).
4. A novel ground mapping aviation device as claimed in claim 2, characterized in that: the steering assembly (5) comprises a rack (51), the rack (51) is vertically fixed on the upper surface of the middle position of the fixed transverse plate (63), a limiting sliding groove (9) is further formed in the machine head (1), and the rack (51) is connected with the limiting sliding groove (9) in a sliding mode.
5. A novel land mapping aviation device as claimed in claim 4, wherein: a fixing block (53) is arranged between the limiting sliding groove (9) and the retracting groove (8), the fixing block (53) is fixedly connected with the inner wall of the machine head (1), a fixing support (52) is fixedly connected to the lower end face of the fixing block (53), a complete gear (56) is rotatably connected to the fixing support (52), and the complete gear (56) is meshed with the rack (51).
6. A novel land mapping aviation device as claimed in claim 5, wherein: one end of the high-definition mapping camera (7) is symmetrically fixed with two fixing clamping plates (71), two fixing shaft rods (55) are fixedly connected between the fixing clamping plates (71), the two ends of each fixing shaft rod (55) are rotatably connected with the inner wall of the corresponding retraction groove (8), a half gear (54) is fixedly connected to the middle position of each fixing shaft rod (55), and the half gear (54) is meshed with the complete gear (56).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122570150.4U CN216375045U (en) | 2021-10-25 | 2021-10-25 | Novel land surveying and mapping aviation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122570150.4U CN216375045U (en) | 2021-10-25 | 2021-10-25 | Novel land surveying and mapping aviation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216375045U true CN216375045U (en) | 2022-04-26 |
Family
ID=81248346
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122570150.4U Expired - Fee Related CN216375045U (en) | 2021-10-25 | 2021-10-25 | Novel land surveying and mapping aviation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216375045U (en) |
-
2021
- 2021-10-25 CN CN202122570150.4U patent/CN216375045U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220426 |