Two vehicle transportation system
A first and a second aircraft are detachably coupled where the first aircraft is configured to perform a vertical landing using a first battery while the first aircraft is unoccupied and the unoccupied first aircraft includes the first battery. In response to detecting a second, removable battery being detachably coupled to the first aircraft, a power source for the first aircraft is switched from the first battery to the second, removable battery. After the switch, the first aircraft takes off vertically using the second, removable battery while occupied. The detachably coupled first aircraft and second aircraft are flown using the second aircraft (the power to keep the detachably coupled first aircraft and second aircraft airborne comes exclusively from the second aircraft and not the first aircraft).
1. A vertical takeoff and landing (VTOL) aircraft, comprising:
at least one rotor;
a first battery;
a battery compartment for a removable battery, wherein:
the VTOL aircraft is configured to perform a vertical landing at least once using the first battery while there is no removable battery in the battery compartment;
after the VTOL aircraft performs the vertical landing at least once using the first battery, the battery compartment is configured to have the removable battery inserted into the battery compartment; and
the VTOL aircraft is configured to perform a vertical takeoff at least once using the removable battery in the battery compartment; and
a coupler configured to detachably couple the VTOL aircraft to a second aircraft, wherein the second aircraft is configured to tow the VTOL aircraft via the coupler such that the second aircraft supplies the power to keep the VTOL aircraft and the second aircraft airborne.
2. The VTOL aircraft recited in claim 1 , wherein the VTOL aircraft and the second aircraft are configured to detachably couple via the coupler while both the VTOL aircraft and the second aircraft are airborne.
3. The VTOL aircraft recited in claim 1 , wherein the VTOL aircraft and the second aircraft are configured to detach from each other while both the VTOL aircraft and the second aircraft are airborne.
4. The VTOL aircraft recited in claim 1 , wherein the second aircraft is a tilt rotor aircraft.
5. The VTOL aircraft recited in claim 1 , wherein:
the second aircraft is a tilt rotor aircraft;
the tilt rotor aircraft and the VTOL aircraft are configured to detachably couple via the coupler while at least one tilt rotor in the tilt rotor aircraft is in a hovering position; and
at least one tilt rotor in the tilt rotor aircraft is configured to be in a forward flight position while the second aircraft tows the VTOL aircraft via the coupler.
6. The VTOL aircraft recited in claim 1 , wherein the second aircraft is a fixed wing aircraft.
7. The VTOL aircraft recited in claim 1 , wherein the VTOL aircraft and the second aircraft are configured to detach from each other, including by:
the second aircraft is configured to descend such that the VTOL aircraft is swung forward;
on a downswing of the VTOL aircraft, the VTOL aircraft is configured to land; and
the VTOL aircraft and the second aircraft are configured to detach after the VTOL aircraft lands.
8. A method, comprising:
performing a vertical landing at least once using a first battery in a vertical takeoff and landing (VTOL) aircraft while there is no removable battery in a battery compartment of the VTOL aircraft, wherein after the VTOL aircraft performs the vertical landing at least once using the first battery, the battery compartment is configured to have the removable battery inserted into the battery compartment; and
performing a vertical takeoff at least once using the removable battery in the battery compartment, wherein:
the VTOL aircraft further includes a coupler that is configured to detachably couple the VTOL aircraft to a second aircraft; and
the second aircraft is configured to tow the VTOL aircraft via the coupler such that the second aircraft supplies the power to keep the VTOL aircraft and the second aircraft airborne.
9. The method recited in claim 8 , wherein the VTOL aircraft and the second aircraft are configured to detachably couple via the coupler while both the VTOL aircraft and the second aircraft are airborne.
10. The method recited in claim 8 , wherein the VTOL aircraft and the second aircraft are configured to detach from each other while both the VTOL aircraft and the second aircraft are airborne.
11. The method recited in claim 8 , wherein the second aircraft is a tilt rotor aircraft.
12. The method recited in claim 8 , wherein:
the second aircraft is a tilt rotor aircraft;
the tilt rotor aircraft and the VTOL aircraft are configured to detachably couple via the coupler while at least one tilt rotor in the tilt rotor aircraft is in a hovering position; and
at least one tilt rotor in the tilt rotor aircraft is configured to be in a forward flight position while the second aircraft tows the VTOL aircraft via the coupler.
13. The method recited in claim 8 , wherein the second aircraft is a fixed wing aircraft.
14. The method recited in claim 8 , wherein the VTOL aircraft and the second aircraft are configured to detach from each other, including by:
the second aircraft is configured to descend such that the VTOL aircraft is swung forward;
on a downswing of the VTOL aircraft, the VTOL aircraft is configured to land; and
the VTOL aircraft and the second aircraft are configured to detach after the VTOL aircraft lands.
15. A computer program product, the computer program product being embodied in a non-transitory computer readable storage medium included in a vertical takeoff and landing (VTOL) aircraft and comprising computer instructions for:
performing a vertical landing at least once using a first battery in the VTOL aircraft while there is no removable battery in a battery compartment of the VTOL aircraft, wherein after the VTOL aircraft performs the vertical landing at least once using the first battery, the battery compartment is configured to have the removable battery inserted into the battery compartment; and
performing a vertical takeoff at least once using the removable battery in the battery compartment, wherein:
the VTOL aircraft further includes a coupler that is configured to detachably couple the VTOL aircraft to a second aircraft; and
the second aircraft is configured to tow the VTOL aircraft via the coupler such that the second aircraft supplies the power to keep the VTOL aircraft and the second aircraft airborne.
16. The computer program product recited in claim 15 , wherein the VTOL aircraft and the second aircraft are configured to detachably couple via the coupler while both the VTOL aircraft and the second aircraft are airborne.
17. The computer program product recited in claim 15 , wherein the VTOL aircraft and the second aircraft are configured to detach from each other while both the VTOL aircraft and the second aircraft are airborne.
18. The computer program product recited in claim 15 , wherein the second aircraft is a tilt rotor aircraft.
19. The computer program product recited in claim 15 , wherein:
the second aircraft is a tilt rotor aircraft;
the tilt rotor aircraft and the VTOL aircraft are configured to detachably couple via the coupler while at least one tilt rotor in the tilt rotor aircraft is in a hovering position; and
at least one tilt rotor in the tilt rotor aircraft is configured to be in a forward flight position while the second aircraft tows the VTOL aircraft via the coupler.
20. The computer program product recited in claim 15 , wherein the VTOL aircraft and the second aircraft are configured to detach from each other, including by:
the second aircraft is configured to descend such that the VTOL aircraft is swung forward;
on a downswing of the VTOL aircraft, the VTOL aircraft is configured to land; and
the VTOL aircraft and the second aircraft are configured to detach after the VTOL aircraft lands.