Specialized honeycomb removing device for transmission line tower
A transmission line and honeycomb technology, applied in the direction of overhead lines/cable equipment, etc., to reduce the risk and speed up the removal
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Embodiment 1
[0033] Embodiment 1, the present invention provides a special cell removal device for power transmission line towers, including a drone body 4, a protective mechanism is set on the drone body 4 corresponding to the rotor 2, and a movable setting is provided below the drone body 4 A workbench 10, on which a control mechanism 7, a communication mechanism 8 and an observation mechanism 9 are set, and a honeycomb removal mechanism is arranged below the workbench 10; the protection mechanism protects the rotor to prevent the seal from colliding with the wind under the pull of the wind Rotors, damage to the rotors or adhesion of sticky matter affect the performance of the drone. The workbench is movable under the drone body and can be placed separately after use. The present invention is mainly aimed at the honeycomb on the line and insulator, and there is also a honeycomb clearing mechanism on the steel frame of the tower. replace.
[0034] The honeycomb clearing mechanism include...
Embodiment 2
[0038] The difference between this embodiment and Embodiment 1 is:
[0039] The oil supply mechanism includes a piston cylinder 22 arranged on the first electric telescopic rod 15, and the upper end of the piston cylinder 22 is downwardly provided with a second electric telescopic rod 20 through an L-shaped bracket 19, and the second electric telescopic rod 20 A push rod 21 matched with the piston barrel 22 is arranged at the end, the front end of the push rod 21 is inserted into the piston barrel 22 and a piston plate 23 is provided, and the front end of the piston barrel 22 communicates with the spray head 17 through the hose 16 . When the second electric telescopic rod is extended, the fuel can be extruded from the piston barrel, supplied to the nozzle through the hose and sprayed out. The piston plate adopts a hard plate and is provided with a rubber layer at the front end to ensure sealing. The connection between the piston barrel and the spray nozzle must use a hose, be...
Embodiment 3
[0042] The difference between this embodiment and Embodiment 1 is:
[0043] The ignition mechanism includes a pulse igniter 12 arranged on the first electric telescopic rod 15 and a storage battery for powering the pulse igniter 12, and the end of the first electric telescopic rod 15 is connected to the pulse igniter 12 18 of the discharge tip. The pulse igniter is a pulse high-frequency oscillator composed of electronic components. The high-frequency voltage generated by the oscillator is raised to a high voltage of 15KV through a step-up transformer, and the tip discharge is carried out, and the fuel is ignited by the spark of the discharge. In order to ensure safety, the nozzle can be set downward through a bracket, while the discharge tip can be set upward through a bracket, so that the two are far apart to avoid burning the nozzle when fuel is burning.
[0044] The protective mechanism includes a circle of shields 3 provided on the UAV body 4 corresponding to the rotor 2...
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