Isolated electronic backbone architecture for aerial devices
An electronic backbone architecture is configured to provide electrical power to an aerial device. The isolated electronic backbone architecture comprises: a power source for generating electrical power, a first actuator, a first electrical motor for powering the first actuator, a second actuator, a second electrical motor for powering the second actuator, and a protected electrical line. The first actuator is disposed adjacent to the first electrical motor. The second actuator is disposed adjacent to the second electrical motor. The protected electrical line is configured to carry electrical current between the power source, the first electrical motor, and the second electrical motor.
1. An aerial device comprising:
a grounded base;
an insulated utility platform disposed at a distal end of a boom assembly;
an isolated electronic backbone architecture for providing electrical power at the utility platform,
said electronic backbone architecture comprising—
a power source for generating electrical power;
a first actuator;
a first electrical motor for powering the first actuator,
wherein the first actuator is disposed adjacent to the first electrical motor;
a second actuator;
a second electrical motor for powering the second actuator,
wherein the second actuator is disposed adjacent to the second electrical motor;
at least one protected electrical cable that traverses from the base to the utility platform,
wherein the protected electrical cable provides electrical current to electrical components at the utility platform and the grounded base while being electrically isolated from both the insulated utility platform and the grounded base; and
wherein the first and second electrical motors are associated with the insulated utility platform and electrically isolated from the utility platform and the grounded base.
2. The aerial device of claim 1 ,
wherein the grounded base is electrically isolated from both the electronic backbone architecture and the insulated utility platform,
wherein the electronic backbone architecture is electrically isolated from both the grounded base and the insulated utility platform,
wherein the insulated utility platform is electrically isolated from both the grounded base and the electronic backbone architecture.
3. The aerial device of claim 2 ,
wherein an incidental contact at the insulated utility platform with an electrified source would be prevented from discharging through the grounded base.
4. The aerial device of claim 1 ,
wherein the first actuator is a linear actuator,
wherein the second actuator is a rotary actuator.
5. The aerial device of claim 4 ,
wherein the first actuator is disposed on the aerial device and secured such that an elongation of the first actuator corresponds to an elongation or pivoting of a component of the aerial device,
wherein the second actuator is disposed on the aerial device and secured such that a rotation of the second actuator corresponds to a rotation of a component of the aerial device.
6. The aerial device of claim 5 ,
wherein the first motor supplies power to the first actuator only so long as the elongation or pivoting is desired,
wherein the second motor supplies power to the second actuator only so long as the rotation is desired,
wherein each said desire is respectively indicated by by an input by a utility worker into a set of controls.
7. The aerial device of claim 1 , wherein the insulated utility platform further comprises:
a platform level assembly, and
a platform control assembly,
wherein the platform level assembly and the platform control assembly are actuated by the first electrical motor.
8. The aerial device of claim 1 , wherein the protected electrical cable is resistive to particular voltage levels, electrical fields, and magnetic fields.