Electricity generating apparatus and unmanned aerial vehicle equipped with same
An electricity generating apparatus capable of efficiently and safely charging a storage battery in an unmanned aerial vehicle during its flight and an unmanned aerial vehicle equipped with such apparatus. The apparatus is mounted in the vehicle, including a fuel tank which is a container body to reserve fuel, an electric generator unit connected to the fuel tank, tilt measurement means capable of measuring a tilt of the fuel tank, and electricity generation control means for controlling operation of generating electricity by the electric generator unit, wherein the electric generator unit is capable of charging a storage battery in the vehicle during flight, and the electricity generation control means drives the electric generator unit when a tilt angle of the fuel tank indicated by the tilt measurement means is within a safe angle which is a predetermined threshold angle, as well as an unmanned aerial vehicle equipped with such apparatus.
1. An electricity generating apparatus which is mounted in an unmanned aerial vehicle, comprising: a fuel tank which is a container body to reserve fuel; an electric generator to which the fuel tank is connected; electricity generation control controller for controlling operation of generating electricity by the electric generator; and an inertial measurement unit for detecting a fall of the unmanned aerial vehicle, wherein the electricity generation controller deactivates driving of the electric generator when the inertial measurement unit fall has detected a fall of the unmanned aerial vehicle.
2. An unmanned aerial vehicle equipped with the electricity generating apparatus as described in claim 1 .
3. The unmanned aerial vehicle according to claim 2 , wherein the unmanned aerial vehicle is a rotorcraft equipped with a plurality of rotors.
4. The electricity generating apparatus according to claim 1 , wherein the inertial measurement unit comprises an inertial sensor.
5. The electricity generating apparatus according to claim 1 , wherein the inertial measurement unit includes a triaxial acceleration sensor and a triaxial angular velocity sensor.
6. An electricity generating apparatus which is mounted in an unmanned aerial vehicle, comprising: a fuel tank which is a container body to reserve fuel; an electric generator to which the fuel tank is connected; electricity generation control controller for controlling operation of generating electricity by the electric generator; a memory in which a noise restriction area which is a predetermined area in geography or within a plant is registered; and a global positioning system (GPS) receiver for locating a flying position of the unmanned aerial vehicle in geography or within the plant, wherein the electricity generation controller deactivates driving of the electric generator when the flying position falls within the noise restriction area.
7. An unmanned aerial vehicle equipped with the electricity generating apparatus as described in claim 6 .
8. The unmanned aerial vehicle according to claim 7 , wherein the unmanned aerial vehicle is a rotorcraft equipped with a plurality of rotors.