Modular aircraft
A modular vertical take-off and landing aircraft for transporting persons and/or loads, comprising a flight module with multiple drive units arranged on a supporting framework structure, each drive unit having an electric motor and a propeller operatively connected to the electric motor, a transport module having a conveying pod and a connection device for connecting the conveying pod to the flight module. The connection device has an elongated shaft, one end of which is attached to the conveying pod, and a coupling device for connecting the flight module to another end of the elongate shaft of the transport module.
1. A vertical take-off and landing modular aircraft for transporting people and/or loads, wherein the aircraft comprises:
a flight module comprising a plurality of drive units arranged on a supporting framework structure, each drive unit comprising an electric motor and one propeller operatively connected to the electric motor;
a transport module comprising a conveying pod and a connecting device for connecting the conveying pod with the flight module, the connecting device comprising a longitudinally extended shaft, one end of which connects to the conveying pod; and
a coupling device, configured for coupling and decoupling the flight module, wherein for reversibly connecting the flight module to another end of the longitudinally extended shaft of the transport module a first part of the coupling device is arranged on the flight module and a second part of the coupling device is arranged as a counterpart on the other end of the longitudinal shaft of the transport module.
2. The aircraft of claim 1 , wherein the flight module and/or the transport module comprises one or more air guiding devices.
3. The aircraft of claim 2 , wherein an angle of incidence ß of the one or more air guiding devices is variable.
4. The aircraft of claim 1 , wherein the flight module comprises a central unit.
5. The aircraft of claim 1 , wherein the flight module and/or the transport module further comprises a charging module.
6. The aircraft of claim 1 , wherein the supporting framework structure of the flight module comprises framework struts connected to each other at node points and wherein a number of drive units are arranged outside of the node points.
7. The aircraft of claim 1 , wherein a number of drive units of the flight module are arranged concentrically around a center axis of the flight module.
8. The aircraft of claim 1 , wherein rotors of the propellers of some number of the drive units have different diameters.
9. The aircraft of claim 1 , wherein the supporting framework structure of the flight module comprises framework struts, all or some of which have a hollow profile with an oval profile cross-section.
10. The aircraft of claim 1 , wherein the shaft of the connecting device is designed in an elongated fashion to create a safety height clearance of the coupling device above the conveying pod.
11. The aircraft of claim 1 , wherein the shaft of the connecting device is substantially rotationally symmetrical and/or wherein the conveying pod of the transport module is rotationally symmetrical and/or substantially drop-shaped.
12. The aircraft of claim 1 , wherein the coupling device is designed as an articulated coupling device.
13. The aircraft of claim 1 , wherein a tilt angle α of the flight module is variable.
14. The aircraft of claim 1 , wherein the supporting framework structure and/or the central unit and/or a number of the drive units comprises components which are made of fiber-reinforced composite or consist of fiber-reinforced composite and/or wherein the shaft and/or the conveying pod include fiber composite material or are made of fiber composite material.
15. The aircraft of claim 1 , wherein the transport module comprises fiber composite material or is made of fiber composite material.
16. The aircraft of claim 14 , wherein the fiber composite material comprises textile reinforcing elements and/or unidirectionally arranged reinforcing fibers.
17. The aircraft of claim 1 , wherein the aircraft further comprises a control unit which is arranged and designed to output a control signal to switch the drive units on or off and/or to open or close the coupling device and/or to set a tilt angle α of the flight module and/or to set an angle of incidence ß of one or more air guiding devices comprised in the aircraft.
18. The aircraft of claim 1 , wherein, in a coupled state, the transport module is arranged below the flight module.
19. The aircraft of claim 1 , wherein the coupling device is designed as an automatic coupling device.
20. A combination for transporting people and/or loads with a vertical take-off and landing modular aircraft, wherein the combination comprises:
a first flight module comprising a plurality of drive units arranged on a supporting framework structure, each drive unit comprising an electric motor and one propeller operatively connected to the electric motor;
a first transport module comprising a conveying pod and a connecting device for connecting the conveying pod with the first flight module, the connecting device comprising a longitudinally extended shaft, one end of which connects to the conveying pod;
a second flight module which is different from the first flight module and comprises a plurality of drive units arranged on a supporting framework structure, each drive unit comprising an electric motor and one propeller operatively connected to the electric motor;
a second transport module which is different from the first transport module and comprises a second conveying pod and a second connecting device for connecting the second conveying pod with the second flight module, the second connecting device comprising a longitudinally extended shaft, one end of which connects to the second conveying pod; and
a coupling device configured for coupling and decoupling the first flight module or the second flight module to another end of the longitudinally extended shaft of the first transport module or the second transport module.