[0027]Bonded belowFigures 1 to 7The present invention will be described in detail, which is convenient, and now, the orientation of the following statement is as follows: The upper and lower directions of the upper and lower directions said belowfigure 1 The projection relationship of the projection is consistent with the front and back and so on.
[0028]A construction road survey drone according to the present invention includes a body 11, and a storage chamber 12 is provided in the body 11, and the lower side of the receiving chamber 12 is provided on the lower side, and the body 11 is provided. The four-axis aircraft 101, the four-axis aircraft 101 is used to fly moving to the survey, and the air mechanism 102 is provided in the vehicle body 11, and the body 11 is provided with a horizontal support mechanism 103, the level. The support mechanism 103 can automatically adjust the body 11 posture, so that the body 11 can face the horizontal position required to cover different terrain and hold the survey, and the receiving chamber 124 is provided with a photovoltaic plate unfolding mechanism 104, the photovoltaic The board deployment mechanism 104 is associated with the horizontal support mechanism 103, and the photovoltaic plate 2 17 is deployed when the body 11 is landing. When charging during the survey, the battery is improved, the pneumatic mechanism 102 is the horizontal support mechanism 103, The photovoltaic plate deployment mechanism 104 provides kinetic energy, the horizontal support mechanism 103, comprising a four-piece annular array distribution and a support plate 20 on the inner wall of the receiving cavity 12, the support plate 20 rotates the shaft one 25, The rotary shaft one 25 is fixedly connected to the arm 26, and the rotating shaft one 25 is fixedly connected to the gear 4 56, and the rotation shaft hole is rotated and the cam 22 is rotated, the cam 22 and the support plate 20 The support frame 74 is fixedly connected, the swivel arm 26 slides to connect the push plate 57 abutting with the rotating shaft one 25, the push plate 57 fixedly connected to the rack 4 61, the rack 4 61 The fixed connection is fixed to the sub-fixing block 60, and the arm 26 is fixed to a fixed block 58 located between the push plate 57 and the sub-fixing block 60, the fixing block 58 and the sub-fixing block 60. A stretch spring is connected to the arm 26, and the rotary arm 26 is rotated, and the rotating shaft 5 65 is fixedly coupled to the passage 64, and the rotating shaft 5 65 is fixedly connected to the rack four 61 Meshing The connected gear 5 66 is fixed to the lower end surface of the rotor 64, and a cylinder 27 is fixed to the cylinder 27, which is provided with an opening downstream.
[0029]It is advantageous, the gear 46, the cam 22, the arm 26 extending to the end surface of the body 11.
[0030]It is advantageously beneficial, the four-axis aircraft 101 includes a four-ring array that is distributed over the outer end surface of the body 11, and the support arm 23 is provided with a propeller propeller 24, the upper surface of the body 11. A photovoltaic plate is fixedly attached to the upper side surface of the body 11 fixed to a total station 16.
[0031]It is advantageously beneficial, and the pneumatic mechanism 102 includes a gas pump 34 fixed to the lower end surface of the body 11, and the gas pump 34 is communicated with a tracheal 1 53, and the gas pipe 1 53 is provided with a pressure valve 54, said The tracheal 1 53 is connected to the trachea 2 55 located on the left side of the pressure valve 54, and the inner wall of the upper side of the body 11 is fixedly connected to a cylinder 1 15, and the cylinder is provided with an opening upright air chamber. 39. A three-way solenoid valve 2 70 is provided on the left side of the gas chamber one 39, and the gas chamber is slidably connected to the piston one 38, the piston one 38 and the upper side inner wall of the air chamber one 39. There is a stretch spring 2 71, and the piston frame 37 is fixed to the lower end surface of the piston one 38, and the piston rod one 37 is fixedly connected to the lifting plate 35 located on the lower side of the cylinder 1 15, the three A hose 140 is connected to the trachea 53, and the hose first 14 is located on the right side of the pressure valve 54, and the pressure valve 54 is turned on, and the gas pressure is large, in the The piston one 38 is moved to the lower limit position before it can be turned on.
[0032]It is advantageously advantageous, and there is a three-way solenoid valve one 32 on the end surface of the air chamber 28, and the three-way solenoid valve one 32 is connected to the trachea 255, and the hose 23 is connected to the air chamber 28. Sliding is attached to the piston 2 29, and the piston 29 is fixed to the piston rod 2 30, and the piston 2 29 is connected to the inner wall of the air cavity 28, and the compression spring is connected between the inner walls. The piston rod 2 is provided with a slider 63 towards the right and toward the right, and the inner wall of the lumen 63 is provided on the left side of the upper and upper array distribution of the limit switch 69, the inner wall of the lumen 63 The support rod 31 is slid on, and the support rod 31 is connected to the upper side of the upper side wall of the la cavity 63, and the upper end surface of the support rod 31 is fixedly connected to the L-shaped rod 68, the The L-shaped rod 68 can trigger the limit switch 69, and the support plate 20 is slidably connected to the rack 2 21, the rack 2 21 meshes the connection, the racks 22 and the place A link one 36 is hinged between the lift plate 35.
[0033]It is advantageously beneficial, and the photovoltaic board deployment mechanism 104 includes a rotating shaft 48 that is rotatably coupled to the support plate 20, and a gear three 45 is fixed to the rotating shaft 48, the gear three 45 and the racks 21 21 Meshing connection, the rotary shaft 48 is fixedly connected to the crank 47, the support plate 20 slides to connect the push rod 49 located on the upper side 21, and the push rod 49 and the crank 47 The hinged rod 2 46 is hinged, and the push rod 49 is fixedly coupled with a slide pin one 50 which is rotated on the support plate 3 44 located on the upper side of the push rod 49, and fixed axis three 44 fixed The lever 43 is connected, and there is two upper and lower symmetry and the sliding groove 51 that penetrates before and after, and the slider 51 is slidably connected to the slip pin 50, and the support plate 20 slide connection There is a rack three 42 on the upper side of the rotary shaft 3 44, and the rack 3 42 is fixedly coupled to the sliding pin 2 52, and the slide pin 2 52 is slidable with the upper side of the chute 51, said The support plate 20 is rotated and connected to the shaft six 73 on the upper side of the rack three 42, and the gear six 72 is fixed to the rotating shaft six 73, and the gear six 72 meshes the connection with the rack three 42. The support plate 20 is rotatably connected to a shaft 2 40 on the upper side of the rack three 42, and a gear 2 41 is fixed to the rotating shaft 2 40, and the gear 2 41 is engaged with the gear six 72. A gear 1 19 is fixed to the axis 2 40, and the inner wall of the housing chamber 12 is slidably connected to the photovoltaic plate 2 17 of the four annular array distribution, the photovoltaic plate 2 17 lower end faces fixed to teeth Bar 18, the rack one 18 meshes the connection with the gear one 19.
[0034]It is advantageously advantageous, the rack plate 27, the rack one 18 can extend to the end surface of the body 11.
[0035]The following combinationFigures 1 to 7The use steps of the engineering construction road survey drone in this article are described in detail:
[0036]Initial state: Under the action of the tension spring 2 71, the piston one 38, the lift plate 35 is located at the upper limit, and the rack 2 21 is located adjacent the cylinder 1 15 side limit, the photovoltaic plate 2 17, the rack one 18 is located The cylinder 1 15 side, the arm 26, the rotor 64, and the cylinder 27 are parallel to the support arm 23, and under the action of the lumen 63, the piston rod 2 30 is located at the upper limit, under the action of the compression spring 2 67, The support rod 31 is located at the lower limit position with respect to the piston rod 2 30, and the L-shaped rod 68 is connected to the lowermost limit switch 69, under the action of the tension spring, the push plate 57, the rack 4 61 is located close to the axis One 25 side limit;
[0037]When working, the manual remote control body 11 fly to the set survey point, then the body 11 slowly decreases, and the air pump 34 starts generating the gas stream, the three-way solenoid valve one 32 makes the hose two 33 and the air cavity two 28 communicate, three-way solenoid valve The second 70 is connected to the hose first and the gas chamber 39, the airflow is passed through the gas pipe 1 53, the hose first 14 is transported to the gas chamber 39 to push the piston one 38 down, the piston one 38 drives the lifting plate 35 to the lower limit At the point, the lifting plate 35 moves away from the lifting plate 35 by the link one 36, and the rack 2 21 is rotated by the rotation of the gear three 45 by meshing, and the gear three 45 rides the crank 47 through the rotating shaft 48. Rotate, crank 47 Move the push rod 49 by the connecting rod 2 46 towards the side of the lifting plate 35, the push rod 49 slides to the sliding guide 51 by the slide 51 slide, the lever 43 is rotated, the lever 43 passes through the upper side slide 51. With the slip pin 2 52, the rack three 42 moves away from the cylinder 1 15, and the rack three 42 drives the gear six 72, the gear two 41, the gear one 19 by meshing, and the gear 1 19 is rotated by the meshing connection. 18 Move away from the cylinder 15 side to achieve the photovoltaic plate 2 17;
[0038]At the same time, the rack 2 21 rotates by meshing the gear four 56, and the gear four 56 rotates the shaft hole 25, the rotating shaft hole 25 is rotated, the shaft hole 25 is fixed, the shaft one 25 pushes the rack 4 61 to move away from fixed On one side of the block 58, the rack 4 61 rotates by engaging the gear 5 66, and the gear 5 66 is rotated by the rotating shaft 5 65, the rotary 27 rotates, allowing the cylinder 27 perpendicular to the support arm 23, that is, the cylinder 27 is perpendicular to the horizontal plane, At this time, the piston one 38 is moved to the lower limit, and the gas stream generated by the air pump 34 opens the pressure valve 54 and passes through the trachea 255, the hose two 33 is delivered into the cavity 28, and pushes the piston 2 29, the piston rod 2 30, The support rod 31 is moved down;
[0039]When the support rod 31 is moved in contact with the ground, the ground on the support rod 31 drives the support rod 31 to move the L-shaped rod 68, and when the L-bar 68 triggers the intermediate limit switch 69, corresponding three-way The solenoid valve is turned off, so that the hose 23 is not in communication with the cavity 28, and if one of the L-shaped rod 68 is in contact with the upper limit switch 69, the corresponding three-way solenoid valve one 32 operates. The pneumatic chamber 28 is in communication with the three-way solenoid valve one 32 exhaust port, and under the action of the compression spring 62, the piston 2 29 is moved to the distance, so that the L-shaped rod 68 is again contacted with the intermediate limit switch 69, after three connections The solenoid valve one 32 is closed, and when the four L-shaped rods 68 are in contact with the intermediate limit switch 69, the air pump 34 is closed, and the body 11 is turned off, and the adjustment posture is completed, the body 11, the whole station device 16 maintains a parallel level, then The whole station system can perform survey;
[0040]Photovolt plate 1, photovoltaic plate 27 can be charged during the detection, using solar energy to charge the battery life;
[0041]When the survey is completed, the propeller propeller 24 starts the carrier body 11 to boost, the three-way solenoid valve two 70 action makes the air cavity one 39 and the three-way solenoid valve two 70 exhaust port, three-way solenoid valve one 32 action, The air cavity 28 is connected to the three-way solenoid valve one 32 exhaust port, under the action of the compression spring 62, the piston 2 29 is reset, under the action of the tension spring 2 71, the piston one 38 is transferred, the piston rod 37 drives the lifting plate 35 to be reset, the racks 2 21, the rack one 18 moves the reset, the arm 26, the rotor 64, and the cylinder 27 reverse reset by the side of the cylinder 1 15 side.
[0042]The beneficial effect of the present invention is that the present invention uses a four-axis aircraft as a full station, the horizontal support mechanism automatically adjusts the four-axis aircraft and the full station gesture during the four-axis aircraft landing process, which automatically adapts to the ground of different terrain. It is guaranteed that the four-axis aircraft and the whole station are in parallel levels, and there is no need to manually carry the whole station and the tripod to significantly reduce the labor intensity of technical personnel. It is not necessary to manually adjust the tripod to keep the whole station to maintain the level, greatly enhance the survey efficiency, The photovoltaic board expansion mechanism can carry up charging after landing and improve the battery life.
[0043]By way of the above, those skilled in the art can make various changes according to the mode of operation within the scope of the present invention.
