Modular unmanned aerial vehicle airframe with structurally integrated yoke and payload assembly
Disclosed here are unmanned aerial vehicle embodiments including some embodiments having a fuselage, tail, and wings including example embodiments with an adaptable payload section, alternatively or additionally, modular flight surfaces including tail, wings and motor, alternatively or additionally the vehicle configured for short landings with reversible thrust, alternatively or additionally, the unmanned aerial vehicle configured with direct connection to moveable flight control surfaces.
1 . An unmanned aerial vehicle, comprising:
a fuselage;
first and second wing sections configured for detachable connection to the fuselage via wing connectors positioned between the fuselage and the first and second wing sections, the first and second wing sections each having a structural component that runs in transverse relation to a length of the unmanned aerial vehicle when connected to the fuselage via the wing connectors;
a yoke connected to the wing connectors and extending internally within the fuselage in transverse relation to a length of the unmanned aerial vehicle, wherein the yoke aligns with the structural components of the first and second wing sections when the first and second wing sections are connected to the fuselage via the wing connectors to form a continuous primary structural element across the fuselage and the first and second wing sections;
a payload section directly connected to the yoke such that the payload section extends forwardly therefrom;
a motor connector positioned at a forward end of the payload section such that the motor connector is spaced from the yoke along the length of the unmanned aerial vehicle;
a tail including a tail boom connected at one end to the fuselage and detachably coupled to a tail connector, wherein the tail boom is configured with multiple resilient tabs and the tail connector includes a cavity that is shaped to receive the tail boom with a matching hole for each of the multiple resilient tabs.
2 . The unmanned aerial vehicle of claim 1 , further comprising a motor detachably connected to the motor connector.
3 . The unmanned aerial vehicle of claim 1 , further comprising a frame extending forwardly from the yoke such that the yoke, the frame, and the motor connector collectively define the payload section.
4 . The unmanned aerial vehicle of claim 3 , wherein the frame includes first and second frame members spaced transversely from each other along a width of the unmanned aerial vehicle.
5 . The unmanned aerial vehicle of claim 3 , further including a payload support bracket spanning the frame and located between the yoke and the motor connector.
6 . An unmanned aerial vehicle, comprising:
a fuselage;
first and second wing sections connected to the fuselage via respective first and second wing connectors, the first and second wing sections each having a structural component;
a yoke having a first and second ends end respectively connected to the first and second wing connectors, wherein the yoke extends internally within the fuselage along a width of the unmanned aerial vehicle and aligns with the structural components of the first and second wing sections to form a continuous primary structural element across the fuselage and the first and second wing sections when the first and second wing sections are connected to the fuselage via the wing connectors;
a frame directly attached to and extending forwardly from the yoke such that the yoke and the frame collectively define a payload section;
a propeller assembly located at a forward end of the unmanned aerial vehicle; and
a tail including a tail boom connected at one end to the fuselage and detachably coupled to a tail connector, wherein the tail boom is configured with multiple resilient tabs and the tail connector includes a cavity that is shaped to receive the tail boom with a matching hole for each of the multiple resilient tabs.
7 . The unmanned aerial vehicle of claim 6 , wherein the payload section is directly connected to a forward portion of the yoke.
8 . The unmanned aerial vehicle of claim 6 , wherein the frame includes discrete first and second frame members.
9 . The unmanned aerial vehicle of claim 8 , wherein the first and second frame members are spaced transversely from each other along the width of the unmanned aerial vehicle.
10 . The unmanned aerial vehicle of claim 6 , further comprising a motor connector positioned at a forward end of the payload section such that the motor connector is spaced from the yoke along a length of the unmanned aerial vehicle.
11 . The unmanned aerial vehicle of claim 10 , wherein the motor connector extends transversely in relation to the frame.
12 . The unmanned aerial vehicle of claim 10 , further comprising a motor detachably connected to the motor connector.
13 . The unmanned aerial vehicle of claim 10 , further including a payload support bracket spanning the frame.
14 . The unmanned aerial vehicle of claim 13 , wherein the payload support bracket extends beneath the payload section.
15 . The unmanned aerial vehicle of claim 13 , wherein the payload support bracket is located between the yoke and the motor connector.
16 . An unmanned aerial vehicle, comprising:
a fuselage;
an internal structural component extending transversely within the fuselage;
wing connectors connected to opposite ends of the internal structural component and configured to releasably connect wing sections of the unmanned aerial vehicle to the fuselage, wherein the wing sections each have a structural component that connects with the wing connectors and aligns with the internal structural component of the unmanned aerial vehicle when connected to form a continuous primary structural element across the fuselage and the wing sections when the wing sections are connected;
a payload section directly connected to a forward portion of the internal structural component such that the payload section extends along a length of the unmanned aerial vehicle;
a propeller assembly located at a forward end of the unmanned aerial vehicle;
a tail including a tail boom connected at one end to the fuselage and detachably coupled to a tail connector, wherein the tail boom is configured with multiple resilient tabs and the tail connector includes a cavity that is shaped to receive the tail boom with a matching hole for each of the multiple resilient tabs.
17 . The unmanned aerial vehicle of claim 16 , further comprising a camera located within the payload section.
18 . The unmanned aerial vehicle of claim 16 , further comprising a motor connector secured to a forward end of the payload section such that the motor connector is spaced from the internal structural component along the length of the unmanned aerial vehicle.
19 . The unmanned aerial vehicle of claim 18 , further comprising a frame extending between the internal structural component and the motor connector.
20 . The unmanned aerial vehicle of claim 19 , wherein the frame includes first and second frame members extending forwardly from the internal structural component, the first and second frame members being spaced transversely from each other along a width of the unmanned aerial vehicle.