IP Library Granted Patent US 12,247,813
Granted Patent B2
US 12,247,813 · App. 18/307,266 · Granted Mar 11, 2025

Payload delivery device

Inventors: Lee Thornhill (Salisbury, GB); Alistair Wragg (Salisbury, GB); Fergus Duncan (Salisbury, GB)
Assignee: THOR INDUSTRIES LTD
F42B25/00F42B10/04F42B12/00F42C5/00B64D1/04F42C9/00
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Quick Facts
Patent No.
US 12,247,813
App. No.
18/307,266
Granted
Mar 11, 2025
Kind
B2
Abstract

Disclosed herein is a payload delivery device. The payload delivery device is configured for delivering an explosive component. The payload delivery device comprises a first module having an interior cavity for containing an explosive component. The payload delivery device further comprises at least one attachment module connected to the central module via a connection means. The at least one attachment module having an interior cavity for containing an additional component.

Claims (35)

1. A payload delivery device for delivering an explosive component, the payload delivery device comprising:

a first module, the first module defining an interior cavity for containing, at least in part, the explosive component, wherein the interior cavity is accessible to a user to allow for the user to configure the explosive component within the interior cavity;

an attachment device configured to releasably attach the payload delivery device to an unmanned aerial system (UAS);

a first sensor configured to sense an environmental parameter;

a second sensor configured to sense a second parameter, different to the environmental parameter;

a memory configured to store a stored environmental parameter and to store a stored second parameter; and

a controller configured to compare the sensed environmental parameter to the stored environmental parameter and to compare the sensed second parameter to the stored second parameter and, on the basis of the comparisons, to transmit a trigger signal configured to cause a detonator to detonate the explosive component.

2. The payload delivery device of claim 1 , wherein the first sensor is an altimeter and the stored environmental parameter is a pressure value.

3. The payload delivery device of claim 1 , wherein the memory is read-writable (RWM) to allow the user to edit the stored environmental parameter.

4. The payload delivery device of claim 3 , further comprising a receiver configured to receive transmissions from an associated transmitter, wherein the memory is operably connected to the receiver such that the stored environmental parameter may be remotely edited by the user via an electromagnetic wave transmission.

5. The payload delivery device of claim 1 , wherein the second sensor is a timer and wherein the second stored parameter is a value of time after release of the payload delivery device from a UAS.

6. The payload delivery device of claim 1 , wherein the second sensor is an impact switch and wherein the second stored parameter is activation of the impact switch.

7. The payload delivery device of claim 5 , wherein the memory is read-writable (RWM) to allow the user to edit the second stored parameter.

8. The payload delivery device of claim 7 , further comprising a receiver configured to receive transmissions from an associated transmitter, wherein the memory is operably connected to the receiver such that the second stored parameter may be remotely edited by the user via an electromagnetic wave transmission.

9. The payload delivery device of claim 1 , further comprising a battery configured to supply electrical energy to the controller and to the memory.

10. The payload delivery device of claim 1 , wherein the controller and the memory are shielded from electronic transmissions.

11. The payload delivery device of claim 1 , further comprising a second module that is releasably connectable in a direct or indirect manner to the first module, wherein the second module comprises stabilizer fins.

12. The payload delivery device of claim 11 , further comprising guidance means and wherein the stabilizer fins are movable based upon control signals from the guidance means so as to allow steering of the payload delivery device after release of the payload delivery device from the UAS.

13. The payload delivery device of claim 1 , wherein the attachment device comprises a second receiver and is configured to detach the payload delivery device from the UAS to which it is mounted upon receipt, by the second receiver, of an electromagnetic wave transmission.

14. A kit of parts comprising parts operable to be assembled into a payload delivery device comprising:

a first module, the first module defining an interior cavity for containing, at least in part, an explosive component, wherein the interior cavity is accessible to a user to allow for the user to configure the explosive component within the interior cavity;

an attachment device configured to releasably attach the payload delivery device to an unmanned aerial system (UAS);

a first sensor configured to sense an environmental parameter;

a second sensor configured to sense a second parameter, different to the environmental parameter;

a memory configured to store a stored environmental parameter and to store a stored second parameter; and

a controller configured to compare the sensed environmental parameter to the stored environmental parameter and to compare the sensed second parameter to the stored second parameter and, on the basis of the comparisons, to transmit a trigger signal configured to cause a detonator to detonate the explosive component.

15. A method for manufacturing a payload delivery device, the method comprising:

producing parts of the payload delivery device including:

a first module, the first module defining an interior cavity for containing, at least in part, an explosive component, wherein the interior cavity is accessible to a user to allow for the user to configure the explosive component within the interior cavity;

an attachment device configured to releasably attach the payload delivery device to an unmanned aerial system (UAS);

a first sensor configured to sense an environmental parameter;

a second sensor configured to sense a second parameter, different to the environmental parameter;

a memory configured to store a stored environmental parameter and to store a stored second parameter; and

a controller configured to compare the sensed environmental parameter to the stored environmental parameter and to compare the sensed second parameter to the stored second parameter and, on the basis of the comparisons, to transmit a trigger signal configured to cause a detonator to detonate the explosive component,

wherein three-dimensional (3D) printing is used to form at least one of the first module or the attachment device.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 27, 2023
From: THORNHILL, LEE; WRAGG, ALISTAIR; DUNCAN, FERGUS
To: THOR INDUSTRIES LTD
Reel/Frame 063455/0221 →
Priority Claims (1)
GB 2209844 · Jul 5, 2022 · national
Continuity (1)
Related Publication 20240010335A1 · Jan 11, 2024
References Cited (13)
US 4344489A · Bonaparte · 1982 [cited by applicant]
US 8746355B2 · Demmitt · 2014 [cited by examiner]
US 11185724B1 · Beard · 2021 [cited by applicant]
US 11685527B2 · Treadway · 2023 [cited by examiner]
US 11754380B2 · Benson · 2023 [cited by examiner]
US 11840339B2 · Sly · 2023 [cited by examiner]
US 20120138319A1 · Demmitt · 2012 [cited by applicant]
US 20120291613A1 · Rastegar · 2012 [cited by applicant]
US 20160216091A1 · Erickson et al. · 2016 [cited by applicant]
US 20210116221A1 · Benson · 2021 [cited by applicant]
EP 4303529A1 · 2024 [cited by examiner]
GB 2620396A · 2024 [cited by examiner]
WO 2018063076A1 · 2018 [cited by applicant]
Cited By (1)
US 12,623,781