Adapter assemblies for aircraft and launchers for deploying aircraft
Adapter assemblies for aircraft and launchers for deploying aircraft are described herein. An example adapter assembly for an unmanned aerial vehicle (UAV) includes a first adapter to be removeably coupled to a first side of a fuselage of the UAV. The first adapter includes first and second posts to interface with a carriage of a launcher. The adapter assembly also includes second adapter to be removeably coupled to a second side of the fuselage of the UAV. The second adapter includes third and fourth posts to interface with the carriage of the launcher.
1. An adapter assembly for an unmanned aerial vehicle (UAV), the adapter assembly comprising:
a first adapter to be disposed on a first side of a fuselage of the UAV, the first adapter including first and second posts to interface with a carriage of a launcher;
a second adapter to be disposed on a second side of the fuselage of the UAV, the second adapter including third and fourth posts to interface with the carriage of the launcher; and
a clamp to couple the first and second adapters to the fuselage of the UAV such that the first and second adapters remain coupled to the fuselage after the UAV is released from the carriage of the launcher.
2. The adapter assembly of claim 1 , wherein the first adapter includes a first plate, the first and second posts extending from the first plate.
3. The adapter assembly of claim 2 , wherein the second adapter includes a second plate, the third and fourth posts extending from the second plate.
4. The adapter assembly of claim 3 , wherein the clamp is a circular band clamp to be disposed around the fuselage of the UAV and engage the first and second plates of the first and second adapters to clamp the first and second adapters against the fuselage of the UAV.
5. The adapter assembly of claim 4 , wherein the clamp is to be disposed between the first and second posts of the first adapter and between the third and fourth posts of the second adapter.
6. The adapter assembly of claim 1 , wherein the first and second adapters are constructed of aluminum.
7. The adapter assembly of claim 1 , further including a first spacer to be disposed on a top side of the fuselage between the fuselage and the clamp.
8. The adapter assembly of claim 7 , further including a second spacer to be disposed on a bottom side of the fuselage between the fuselage and the clamp.
9. The adapter assembly of claim 8 , wherein the first and second spacers are constructed of acrylonitrile butadiene styrene (ABS) plastic.
10. The adapter assembly of claim 1 , wherein the first and second posts have different cross-sectional shapes and sizes.
11. The adapter assembly of claim 1 , wherein the first, second, third, and fourth posts have circular cross-sectional shapes.
12. A system comprising: a launcher to deploy an unmanned aerial vehicle (UAV), the launcher including a moveable carriage, the carriage having a first arm with a first notch and a second arm with a second notch; a first adapter to be removably coupled to a first side of a fuselage of the UAV, the first adapter including a first post to interface with the carriage, the first post having a shape corresponding to the first notch of the first arm; and a second adapter to be removably coupled to a second side of the fuselage opposite the first side, the second adapter including a second post to interface with the carriage, the second post having a shape corresponding to the second notch of the second arm.
13. The system of claim 12 , further including a clamp to removably couple the first adapter and the second adapter to the fuselage of the UAV.
14. The system of claim 13 , further including spacers to be disposed between the clamp and the fuselage of the UAV.
15. The system of claim 12 , wherein the first adapter includes a first plate, the first post extending from the first plate, and wherein the second adapter includes a second plate, the second post extending from the second plate.
16. The system of claim 12 , wherein the first and second adapters are constructed of aluminum.
17. A method comprising: removably coupling a first adapter to a first side of a fuselage of an aircraft, the first adapter including first and second posts; removably coupling a second adapter to a second side of the fuselage of the aircraft opposite the first side, the second adapter including third and fourth posts; setting the aircraft on a carriage of a launcher, where in the carriage has a first set of arms with notches and a second set of arms with notches, and wherein setting the aircraft on the carriage includes setting the first and second posts in the notches of the first set of arms and setting the third and fourth posts in the notches of the second set of arms; and launching the aircraft with the launcher.
18. The method of claim 17 , further including removing the first and second adapters from the aircraft.
19. The method of claim 17 , wherein the aircraft is an unmanned aerial vehicle (UAV).
20. A method comprising: clamping, via a clamp, first and second adapters to first and second sides, respectively, of a fuselage of an aircraft to removably couple the first and second adapters to the fuselage of the aircraft, the first adapter including first and second posts, the second adapter including third and fourth posts; setting the aircraft on a carriage of a launcher; and launching the aircraft with the launcher.