IP Library › Granted Patent US 11,041,950
Granted Patent B2
US 11,041,950 · App. 16/163,385 · Granted Jun 22, 2021

Surveillance systems providing integrated functional redundancy

Inventor: James Roy Troxel (Glendale, AZ)
Assignee: AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS, LLC
G01S13/933G01S7/032G01S13/765G01S13/767G06F11/18G08G5/0008G08G5/0013G08G5/0078G08G5/045G01S13/781
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Quick Facts
Patent No.
US 11,041,950
App. No.
16/163,385
Granted
Jun 22, 2021
Kind
B2
Abstract

Various communication systems may benefit from suitable use of redundancy. For example, surveillance systems in avionics applications may benefit from having functional redundancy. A system can include a collision avoidance or alerting system function in wired connection to a directional antenna. The system can also include a first mode-S transponder function in wired connection to the directional antenna. The system can further include a second mode-S transponder function in wired connection to the directional antenna, wherein the first mode-S transponder function is independent from the second mode-S transponder function.

Claims (14)

1. A communication system for an aircraft, the system comprising:

a collision avoidance or alerting system function in wired connection to a directional antenna;

a first mode-S transponder function in wired connection to the directional antenna; and

a second mode-S transponder function in wired connection to the directional antenna, wherein the first mode-S transponder function is independent from the second mode-S transponder function.

2. The system of claim 1 , wherein the system comprises a single unit.

3. The system of claim 1 , wherein being independent comprises having an independent power supply, an independent processor, an independent input/output, an independent transmitter, an independent receiver, or any combination thereof.

4. The system of claim 1 , wherein the first mode-S transponder is internally partitioned, within the system, in a first partition separate from the second mode-S transponder in a second partition.

5. The system of claim 4 , wherein the first partition and the second partition are on a same circuit card.

6. The system of claim 4 , wherein the first partition and the second partition are on separate circuit cards.

7. The system of claim 4 , wherein the first partition and the second partition are on separate units.

8. The system of claim 1 , wherein the first mode-S transponder function and the second mode-S transponder function are configured to provide redundancy for each other.

9. The system of claim 1 , wherein a field programmable gate array of the first partition is in communication with a field programmable gate array of the second partition over a high speed bus.

10. The system of claim 1 , wherein the collision avoidance or alerting system function comprises a TCAS-I, a TCAS-II, a traffic advisory system (TAS), an automatic dependent surveillance broadcast (ADS-B) advisory system, an ACAS-X, or any combination thereof.

11. The system of claim 1 , wherein circuitry of the first mode-S transponder function and circuit of the second mode-S transponder function are each configured to support operation of the collision avoidance or alerting system function.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 6, 2020
From: TROXEL, JAMES ROY
To: AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS, LLC
Reel/Frame 051745/0631 →
Continuity (2)
Provisional Application 62573577 · Oct 17, 2017
Related Publication 20190113617A1 · Apr 18, 2019
Cited By (2)
US 12,190,744 US 12,730,212