Unmanned air vehicle weapon adapter
View Patent ↗In some embodiments, an adapter for attaching a handheld firearm to an unmanned air vehicle comprises a mounting assembly configured for attachment to said firearm and to the unmanned air vehicle, and an actuation assembly comprising an actuation device configured to actuate a trigger of the handheld firearm.
1. An adapter for attaching a handheld firearm to an unmanned air vehicle comprising:
a mounting assembly configured for attachment to said firearm and to said unmanned air vehicle; and
an actuation assembly comprising a first actuation device configured to actuate a trigger of said handheld firearm, a second actuation device configured to actuate a safety mechanism of said handheld firearm and a releasable link coupling between the second actuation device and the safety mechanism, said releasable link coupling arranged to release an attachment between said second actuation device and said safety mechanism upon application of a predetermined amount of torque.
2. The adapter of claim 1 , wherein said mounting assembly comprises a recoil isolation mechanism.
3. The adapter of claim 1 , wherein said mounting assembly comprises a first portion slidably engaged with a second portion.
4. The adapter of claim 3 , wherein said mounting assembly further comprises a biasing member.
5. The adapter of claim 4 , wherein said biasing member is positioned between the first portion and the second portion.
6. The adapter of claim 5 , further comprising a damper, wherein said biasing member and said damper are located on opposite sides of the first portion.
7. The adapter of claim 4 , wherein said biasing member forces said first portion to a nominal position.
8. The adapter of claim 1 , wherein said mounting assembly comprises a truss member fixedly attached to said handheld firearm.
9. The adapter of claim 8 , wherein said mounting assembly further comprises a support bracket, said truss member slidably engaged with said support bracket.
10. The adapter of claim 9 , further comprising a shaft, said shaft being slidably engaged with said support bracket or said truss member.
11. The adapter of claim 10 , wherein a longitudinal axis of said shaft is parallel to a longitudinal axis of a barrel of said handheld firearm.
12. The adapter of claim 1 , wherein said actuation assembly comprises a body configured to be supported by a body of said handheld firearm.
13. The adapter of claim 1 , said actuation assembly further comprising a locking mechanism configured to prevent actuation of said safety mechanism.
14. The adapter of claim 1 , wherein said actuation device comprises a servo motor.
15. The adapter of claim 1 , wherein a barrel axis of the handheld firearm passes through a center of gravity of the UAV.
16. The adapter of claim 1 , wherein said actuation assembly comprises a roller configured to contact said trigger.
17. An unmanned air vehicle comprising:
a structural framework;
a commercially available firearm designed to be fired by hand, the firearm comprising a trigger and a safety;
a mounting assembly, a first portion of said mounting assembly attached to said firearm, a second portion of said mounting assembly attached to said structural framework;
a first actuator configured to actuate said trigger;
a second actuator configured to actuate said safety; and
a releasable link coupling between the second actuation device and the safety mechanism, said releasable link coupling arranged to release an attachment between said second actuation device and said safety mechanism upon application of a predetermined amount of torque.
18. The unmanned air vehicle of claim 17 , wherein said mounting assembly comprises a recoil absorbing mechanism that isolates the structural framework from recoil forces generated by the firearm.
19. The unmanned air vehicle of claim 18 , wherein said mounting assembly only contacts a barrel of the firearm.
20. An unmanned air vehicle comprising:
a structural framework;
a firearm designed to be fired by hand, the firearm comprising a body, a trigger, a safety and a barrel;
a mounting assembly attaching said firearm to said structural framework, a first portion of said mounting assembly attached to said barrel of said firearm, a second portion of said mounting assembly attached to said structural framework, said mounting assembly comprising a recoil absorbing mechanism; and
a first actuator configured to actuate said trigger; a second actuator configured to actuate said safety; and a releasable link coupling between the second actuation device and the safety mechanism, said releasable link coupling arranged to release an attachment between said second actuation device and said safety mechanism upon application of a predetermined amount of torque; wherein
said mounting assembly only contacts the barrel of the firearm.
21. The unmanned air vehicle of claim 20 , wherein said firearm is a grenade launcher.