Battery and unmanned aerial vehicle with the battery
The disclosure provides a battery which can include a power supply and power supply circuit, the power supply circuit connected to the power supply. The power supply can discharge through the power supply circuit. An electronic switch can control the power-on or off of the power supply, thereby avoiding the generation of sparks during the power on process and allowing for the normal use of the battery and the safety of the aircraft. The disclosure also provides an aircraft having the battery.
1. A power supply assembly for an unmanned aerial vehicle (UAV), comprising:
a housing comprising a bottom casing and a cover member, wherein the cover member is positioned to cover an opening of the bottom casing;
a power supply configured to power the UAV, wherein the power supply is disposed in the bottom casing;
a circuit board positioned inside the housing, wherein the circuit board is electrically connected to the power supply;
an input device carried by the circuit board and configured to receive a user input;
an electronic switch in electrical communication with the power supply to control a supply of power from the power supply to the UAV, wherein the input device is electrically connected with the electronic switch to control at least one of a switch-on state or a switch-off state of the electronic switch;
a power measurement device in electrical communication with the power supply, wherein the power measurement device is configured to calculate at least one of a level of charge or remaining capacity of the power supply;
a connector interface configured to transmit, to the UAV, a signal indicating the level of charge or a remaining capacity of the power supply; and
wherein the at least one venting opening of the bottom casing is not exposed at the exterior surface of the UAV when the bottom casing is inserted into the UAV.
2. The power supply assembly of claim 1 , wherein the bottom casing has at least one venting opening.
3. The power supply assembly of claim 2 , wherein the bottom casing is configured to be inserted into the UAV, and wherein the cover member forms at least a portion of an exterior surface of the UAV when the bottom casing is inserted into the UAV.
4. The power supply assembly of claim 2 , wherein the bottom casing is a rectangular casing.
5. The power supply assembly of claim 4 , wherein the rectangular casing includes two semi-rectangular casings coupled together.
6. The power supply assembly of claim 4 , wherein each of at least two sides of the rectangular casing has a venting opening.
7. The power supply assembly of claim 1 , further comprising:
an indication device comprising multiple LEDs configured to display the remaining capacity of the power supply.
8. The power supply assembly of claim 4 , further comprising:
a light guide module configured to fit in the cover member, wherein the light guide module is positioned to allow light from the LEDs to pass through the cover member.
9. The power supply assembly of claim 5 , wherein the light guide module includes a transparent acrylic material.
10. The power supply assembly of claim 1 , wherein the power measurement device comprises a current sampling device configured to detect at least one of a current signal during charging or discharging of the power supply.
11. The power supply assembly of claim 1 , wherein the input device is a key switch, and wherein the electronic switch comprises at least one of a power MOSFET, a solid state relay, a power transistor, or an insulated gate bipolar transistor (IGBT).
12. The power supply assembly of claim 1 , wherein the circuit board includes a first surface and a second surface opposite the first surface, wherein the connector interface is disposed on the first surface and the input device is disposed on the second surface of the circuit board.
13. The power supply assembly of claim 12 , wherein the connector interface is in electrical communication with an input interface of the UAV.
14. The power supply assembly of claim 1 , wherein the signal transmitted to the UAV contains voltage information of the power supply.
15. A power supply assembly for an unmanned aerial vehicle (UAV), comprising:
a housing comprising a bottom casing and a cover member, wherein the bottom casing is configured to be inserted into the UAV, wherein the cover member forms at least a portion of an exterior surface of the UAV when the bottom casing is inserted into the UAV, and wherein the bottom casing has at least one venting opening that is not exposed at the exterior surface of the UAV when the bottom casing is inserted into the UAV;
a power supply configured to power the UAV, wherein the power supply is disposed in the bottom casing;
a circuit board inside the housing, wherein the circuit board is electrically connected to the power supply;
an input device carried by the circuit board and configured to receive a user input;
an electronic switch in electrical communication with the power supply to control a supply of power from the power supply to the UAV, wherein the input device is electrically connected with the electronic switch to control t at least one of a switch-on state or a switch-off state of the electronic switch;
a power measurement device in electrical communication with the power supply, wherein the power measurement device is configured to calculate at least one of a level of charge or remaining capacity of the power supply; and
a connector interface configured to transmit, to the UAV, a signal indicating the level of charge or remaining capacity of the power supply.
16. An unmanned aerial vehicle system, comprising:
an unmanned aerial vehicle (UAV) having one or more propulsion units;
a power supply assembly including
a housing comprising a bottom casing and a cover member, wherein the bottom casing is configured to be inserted into the UAV, wherein the cover member forms at least a portion of an exterior surface of the UAV when the bottom casing is inserted into the UAV, and wherein the bottom casing has at least one venting opening that is not exposed at the exterior surface of the UAV when the bottom casing is inserted into the UAV;
a power supply configured to power the one or more propulsion units of the UAV, wherein the power supply is disposed in the bottom casing;
a circuit board inside the housing, wherein the circuit board is electrically connected to the power supply;
an input device disposed on the circuit board and configured to receive a user input;
an electronic switch in electrical communication with the power supply to control a supply of power from the power supply to the UAV, wherein the input device is electrically connected with the electronic switch to control at least one of a switch-on state or a switch-off state of the electronic switch;
a power measurement device in electrical communication with the power supply, wherein the power measurement device is configured to calculate at least one of a level of charge or remaining capacity of the power supply; and
a connector interface configured to transmit, to the UAV, a signal indicating the level of charge or remaining capacity of the power supply.
17. The power supply assembly of claim 16 , wherein the power supply operates to power a carrier of the UAV.
18. The power supply assembly of claim 16 , wherein the power supply operates to power a payload carried by the carrier of the UAV.