Tilt-rotor multicopters with variable pitch propellers
Aircraft are configured to facilitate propeller blade pitch adjustability. According to one example, an aircraft can include a plurality of propellers, where each propeller includes plurality of blades. At least one pitch adjust mechanism may be associated with at least on propeller, where the pitch adjust mechanism is configured to adjust a pitch of the plurality of blades for at least one propeller in response to airflow from at least one other propeller influencing an airflow at the at least one propeller. Other aspects, embodiments, and features are also included.
1. An aircraft, comprising:
a plurality of propellers, each propeller including a plurality of blades; and
at least one pitch adjust mechanism associated with at least one propeller, the at least one pitch adjust mechanism configured to adjust a pitch of the plurality of blades for at least one propeller in response to
an airspeed and a propeller axis of orientation with respect to the airspeed, wherein the pitch of the plurality of blades for at least one propeller is increased in response to an increase in airspeed and an increase in an angle of attack for the propeller axis of orientation with respect to the airspeed, and the pitch is decreased in response to a decrease in airspeed.
2. The aircraft of claim 1 , further comprising:
a storage medium; and
a processing circuit coupled to the storage medium, the plurality of propellers and the at least one pitch adjust mechanism, the processing circuit adapted to:
adjust a pitch of the plurality of blades for at least one propeller utilizing the at least one pitch adjust mechanism.
3. The aircraft of claim 1 , further comprising at least one tilt adjust mechanism associated with one or more respective propellers, the at least one tilt adjust mechanism configured to adjust a tilt of the one or more respective propellers.
4. The aircraft of claim 3 , further comprising:
a storage medium; and
a processing circuit coupled to the storage medium, the plurality of propellers, the at least one tilt adjust mechanism, and the at least one pitch adjust mechanism, the processing circuit adapted to:
adjust a tilt of at least one propeller of the plurality of propellers utilizing the at least one tilt adjust mechanism; and
adjust a pitch of the plurality of blades for at least one propeller utilizing the at least one pitch adjust mechanism.
5. The aircraft of claim 3 , wherein the at least one tilt adjust mechanism is configured to adjust the tilt of the one or more respective propellers to control a pitch of the aircraft independent of a propeller thrust vector for each of the one or more respective propellers.
6. The aircraft of claim 3 , wherein the at least one tilt adjust mechanism is configured to adjust the tilt of the one or more respective propellers independent of a tilt of one or more other propellers.
7. The aircraft of claim 1 , wherein the at least one pitch adjust mechanism is configured to adjust the pitch of the plurality of blades for the at least one propeller further in response to a tilt of a leading propeller that is upstream to the at least one propeller.
8. The aircraft of claim 1 , wherein the at least one pitch adjust mechanism configured to adjust the pitch of the plurality of blades for the at least one propeller in response to an airspeed and a propeller axis of orientation with respect to the airspeed comprises the at least one pitch adjust mechanism configured to adjust the pitch of the plurality of blades for the at least one propeller in response to at least one of
a speed of air entering the at least one propeller from an airspeed vector of the aircraft,
a speed of air entering the at least one propeller after exiting at least one propeller leading the at least one propeller,
a change in pressure of air exiting the at least one propeller as a result of the air exiting the at least one propeller subsequently entering at least one propeller trailing the at least one propeller, or
at least one of a speed, direction, or turbulent condition of air surrounding the at least one propeller.
9. A method operational on an aircraft, comprising:
setting a speed for a plurality of propellers, each propeller including a plurality of blades; and
adjusting a pitch of the plurality of blades for at least one propeller in response to
an airspeed and a propeller axis of orientation with respect to the airspeed, wherein the pitch of the plurality of blades for the at least one propeller is increased in response to an increase in airspeed and an increase in an angle of attack for the propeller axis of orientation with respect to the airspeed, and the pitch is decreased in response to a decrease in airspeed.
10. The method of claim 9 , further comprising adjusting a tilt of one or more respective propellers.
11. The method of claim 10 , wherein adjusting the tilt of the one or more respective propellers comprises:
adjusting the tilt of the one or more respective propellers independent of a tilt of one or more other propellers.
12. The method of claim 10 , wherein adjusting the tilt of the one or more respective propellers comprises:
adjusting the tilt of the one or more respective propellers to control a pitch of the aircraft independent of a propeller thrust vector for each of the one or more respective propellers.
13. The method of claim 9 , wherein adjusting the pitch of the plurality of blades for at least one propeller comprises:
adjusting the pitch of the plurality of blades utilizing a pitch adjust mechanism.
14. The method of claim 9 , wherein adjusting the pitch of the plurality of blades for at least one propeller in response to an airspeed and a propeller axis of orientation with respect to the airspeed comprises:
adjusting the pitch of the plurality of blades for at least one propeller further in response to at least one of
a speed of air entering the at least one propeller from an airspeed vector of the aircraft,
a speed of air entering the at least one propeller after exiting at least one propeller leading the at least one propeller,
a change in pressure of air exiting the at least one propeller as a result of the air exiting the at least one propeller subsequently entering at least one propeller trailing the at least one propeller, or
at least one of a speed, direction, or turbulent condition of air surrounding the at least one propeller.
15. A non-transitory processor-readable storage medium storing processor-executable programming for causing a processing circuit to:
set a speed for a plurality of propellers, each propeller including a plurality of blades; and
adjust a pitch of the plurality of blades for at least one propeller in response to
an airspeed and a propeller axis of orientation with respect to the airspeed, wherein the pitch of the plurality of blades for the at least one propeller is increased in response to an increase in airspeed and an increase in an angle of attack for the propeller axis of orientation with respect to the airspeed, and the pitch is decreased in response to a decrease in airspeed.
16. The processor-readable storage medium of claim 15 , further comprising processor-executable programming for causing a processing circuit to:
adjust a tilt of the one or more respective propellers.
17. The processor-readable storage medium of claim 16 , wherein the processor-executable programming for causing a processing circuit to adjust a tilt of the one or more respective propellers comprises processor-executable programming for causing a processing circuit to:
adjust the tilt of the one or more respective propellers utilizing at least one tilt adjust mechanism.
18. The processor-readable storage medium of claim 16 , wherein the processor-executable programming for causing a processing circuit to adjust a tilt of the one or more respective propellers comprises processor-executable programming for causing a processing circuit to:
adjust the tilt of the one or more respective propellers to control a pitch of the aircraft independent of a propeller thrust vector for each of the one or more respective propellers.
19. The processor-readable storage medium of claim 16 , wherein the processor-executable programming for causing a processing circuit to adjust a tilt of the one or more respective propellers comprises processor-executable programming for causing a processing circuit to:
adjust the tilt of the one or more respective propellers independent of a tilt of one or more other propellers.
20. The processor-readable storage medium of claim 15 , wherein the processor-executable programming for causing a processing circuit to adjust the pitch of the plurality of blades for at least one propeller in response to an airspeed and a propeller axis of orientation with respect to the airspeed comprises processor-executable programming for causing a processing circuit to:
adjust the pitch of the plurality of blades for at least one propeller in response to at least one of
a speed of air entering the at least one propeller from an airspeed vector of the aircraft,
a speed of air entering the at least one propeller after exiting at least one propeller leading the at least one propeller,
a change in pressure of air exiting the at least one propeller as a result of the air exiting the at least one propeller subsequently entering at least one propeller trailing the at least one propeller, or
at least one of a speed, direction, or turbulent condition of air surrounding the at least one propeller.