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1. WO2020112205 - UNITÉS DE LOGEMENT DURCIES POUVANT ÊTRE DÉPLOYÉES

Note: Texte fondé sur des processus automatiques de reconnaissance optique de caractères. Seule la version PDF a une valeur juridique

[ EN ]

CLAIMS

1. A chassis for housing electronic componentry, the chassis comprising:

a chassis frame having a top plate and a bottom plate, wherein the chassis frame has a plurality of protrusions that extend beyond the top plate and the bottom plate;

a first handle and a second handle, wherein the first handle is attached to two of the plurality of protrusions and the second handle is attached to two of the plurality of protrusions;

an interface panel and a back panel, wherein the back panel is located on the chassis frame opposite the interface panel; and

a first cooling vent.

2. The chassis according to claim 1, wherein the plurality of protrusions are configured to protect the interface panel during transportation, installation, and operation of the chassis.

3. The chassis according to any one of claims 1-2, wherein the interface panel includes an interface connection configured to communicate with a processor control unit or an antenna interface unit.

4. The chassis according to any one of claims 1-3, further comprising shock mounts having bolt holes, wherein the shock mounts are a monolithic component of the chassis frame.

5. The chassis according to any one of claims 1-4, further comprising a plurality of heat pipes disposed inside the chassis frame, wherein one of the plurality of heat pipes is in thermal contact with the top plate, and one of the plurality of heat pipes is in thermal contact with the back panel.

6. The chassis according to any one of claims 1-5, wherein the top plate includes a heat sink with fins.

7. The chassis according to any one of claims 1-6, further comprising a second cooling vent located in the back panel, and wherein the first cooling vent is located in the interface panel.

8. The chassis according to claim 7, further comprising a fan operable to draw air into the chassis and expel air from the chassis.

9. The chassis according to any one of claims 1-8, further comprising an internal mount for mounting computer componentry and radio componentry within the chassis frame.

10. A multi-chassis system for housing electronic componentry, the multi-chassis system comprising:

a first chassis frame having a first top plate and a first bottom plate, wherein the first chassis frame has a plurality of first protrusions that extend beyond the first top plate and the first bottom plate;

a first handle and a second handle, wherein the first handle is attached to two of the plurality of first protrusions and the second handle is attached to two of the plurality of first protrusions;

a first interface panel having a first port;

a first back panel, wherein the first back panel is located on the first chassis frame opposite the first interface panel;

a second chassis frame having a second top plate and a second bottom plate, wherein the second chassis frame has a plurality of second protrusions that extend beyond the second top plate and the second bottom plate;

a third handle and a fourth handle, wherein the third handle is attached to two of the plurality of second protrusions and the fourth handle is attached to two of the plurality of second protrusions;

a second interface panel having a second port; and

a second back panel, wherein the second back panel is located on the second chassis frame opposite the second interface panel,

wherein the first port and the second port are configured to be coupled via a wired communication link.

11. The multi-chassis system of claim 10, wherein the wired communication link is configured to carry communication signals between the first interface panel and the second interface panel, and wherein the wired communication link is configured to carry electric

power from the first interface panel to the second interface panel.

12. The multi-chassis system of any one of claims 10-11, wherein the plurality of first protrusions are configured to protect the first interface panel during transportation, installation, and operation of the multi-chassis system, and wherein the plurality of second protrusions are configured to protect the second interface panel during transportation, installation, and operation of the multi-chassis system.

13. The multi-chassis system of any one of claims 10-12, wherein the second interface panel further comprises a first Wi-Fi antenna port, a second Wi-Fi antenna port, a high band antenna port, a low band antenna port, and a GPS antenna port.

14. The multi-chassis system of any one of claims 10-13, wherein the first and second chassis frames further comprise internal mounts for mounting computer componentry and radio componentry within the respective chassis frames.

15. The multi-chassis system of any one of claims 10-14, further comprising a plurality of heat pipes disposed inside the first and second chassis frames.

16. A method comprising:

providing a system comprising a processor control unit chassis operably coupled to an antenna interface unit chassis, the processor control unit chassis including a first interface panel and first electronic componentry, and the antenna interface unit chassis including a second interface panel and second electronic componentry;

detecting, via the system, an unmanned aircraft system entering restricted airspace; and

locating, via the system, the unmanned aircraft system based on the detecting step.

17. The method according to claim 16, further comprising identifying, via the system, the unmanned aircraft system based on the detecting step.

18. The method according to any one of claims 16-17, further comprising mitigating, via the system, a threat of the unmanned aircraft system based on the detecting step, wherein the mitigating step includes delivering a non-kinetic, non-attributable signal.

19. The method according to any one of claims 16-18, further comprising:

connecting the processor control unit chassis and the antenna interface unit chassis by a communication link;

carrying signals between the first interface panel and the second interface panel via the communication link; and

carrying electric power from the first interface panel to the second interface panel via the communication link, wherein the system is a counter unmanned aircraft.

20. The method according to any one of claims 16-19, further comprising:

protecting the first electronic componentry by providing the processor control unit chassis with a first protective protrusion extending beyond the first interface panel, a first heat sink including second fins, a first heat pipe disposed inside the processor control unit chassis, and a first cooling vent;

protecting the second electronic componentry by providing the antenna interface unit chassis with a second protective protrusion extending beyond the second interface panel, a second heat sink including second fins, a second heat pipe disposed inside the processor control unit chassis, and a second cooling vent; and

securing the processor control unit chassis and the antenna interface unit chassis to an object via shock mounts.