Aerial vehicle with hybrid drive and rotor unit including rotor shafts coupled by inclined synchro gear wheels
An aerial vehicle is disclosed having a hybrid drive unit and a rotor unit wherein the hybrid drive unit includes at least a combustion engine, a generator and a first electric motor and the rotor unit includes a first rotor. The combustion engine is configured to drive the generator to produce electricity, and the generator is coupled to the first electric motor in such a way that the first electric motor is feedable with electricity from the generator. The rotor unit includes a second rotor and the hybrid drive unit includes a second electric motor, wherein the generator is coupled to the second electric motor in such a way that the second electric motor is feedable with electricity from the generator. The first rotor is driven by the first electric motor and the second rotor is driven by the second electric motor.
1. An aerial vehicle comprising:
a hybrid drive unit; and
a rotor unit,
wherein the hybrid drive unit comprises a combustion engine, a generator, a first electric motor, and a second electric motor,
wherein the rotor unit comprises a first rotor, and a second rotor,
wherein the combustion engine is configured to drive the generator to produce electricity,
wherein the generator is coupled to the first electric motor such that the first electric motor is feedable with electricity from the generator,
wherein the generator is coupled to the second electric motor such that the second electric motor is feedable with electricity from the generator,
wherein the first electric motor is coupled to the first rotor to drive the first rotor,
wherein the second electric motor is coupled to the second rotor to drive the second rotor,
wherein a shaft of the first rotor and a shaft of the second rotor are coupled to one another by a coupling unit,
wherein the coupling unit is a gear unit comprising a first synchro gear wheel being coupled to the shaft of the first rotor and a second synchro gear wheel being coupled to the shaft of the second rotor,
wherein the first synchro gear wheel directly engages with the second synchro gear wheel,
wherein the first synchro gear wheel as well as the shaft and rotor blades of the first rotor rotate about a common first rotational axis,
wherein the second synchro gear wheel as well as the shaft and rotor blades of the second rotor rotate about a common second rotational axis, and
wherein the first rotational axis and the second rotational axis are inclined with regard to a vertical axis in opposite directions, wherein an inclination of the first and the second rotational axes with regard to the vertical axis is between 5° and 20°.
2. The aerial vehicle according to claim 1 , wherein the hybrid drive unit further comprises at least one buffer battery which is coupled
to the generator to be fed with electricity produced by the generator, and
to the first electric motor and/or the second electric motor to feed the first electric motor and/or the second electric motor.
3. The aerial vehicle according to claim 1 , wherein the first rotor and the second rotor are configured to rotate in opposite directions and to mesh in an interleaved manner.
4. The aerial vehicle according to claim 1 , wherein the first rotor and the second rotor are configured to rotate at an angular offset of 90°.
5. The aerial vehicle according to claim 1 , wherein the first rotor and the second rotor are inclined with regard to a horizontal axis in opposite directions.
6. The aerial vehicle according to claim 5 , wherein an inclination of the rotor blades with regard to the horizontal axis is between 5° and 20°.
7. The aerial vehicle according to claim 1 , wherein at least at one of the two rotors a sensor is provided for measuring a rotor speed.
8. The aerial vehicle according to claim 1 , wherein the hybrid drive unit is formed as serial hybrid drive.
9. The aerial vehicle according to claim 5 , wherein an inclination of the rotor blades with regard to the horizontal axis is between 10° and 15°.
10. The aerial vehicle according to claim 1 , wherein an inclination of the first and the second rotational axes with regard to the vertical axis is between 10° and 20° or between 10° and 15°.
11. The aerial vehicle according to claim 1 , wherein the rotor unit comprises upper rotating swash plates, and lower non-rotating swash plates.
12. The aerial vehicle according to claim 11 , wherein at least one servo drive is arranged at the lower non-rotating swash-plate.