Flight recorder system and method

Patent metadata

Field	Value
Publication number	US-12589883-B2
Application number	US-202318355841-A
Country	US
Kind code	B2
Filing date	Jul 20, 2023
Priority date	Jul 20, 2023
Publication date	Mar 31, 2026
Grant date	Mar 31, 2026

Abstract

A CVFDR system of an aircraft includes a cockpit voice and flight data recorder (CVFDR) communicatively coupled, via a data communication network, to a set of flight recorder modules. The CVFDR receives a first voltage from a remote first power source. In the event of an interruption of the first voltage, the CVFDR receives a second voltage from a local second power source for a predetermined period.

First claim

What is claimed is:

1 . A cockpit voice and flight data recorder (CVFDR) system couplable to a data communications network, the CVFDR system comprising:
a control module comprising a processor and coupleable to a remote first power source to receive a first voltage therefrom; a first memory communicatively coupled to the processor; a second memory communicatively coupled to the processor; a second power source coupled to the control module, the control module configured to operate in a normal mode of operation comprising providing power to the processor, executing program code read from the first memory, receiving data from the communications network, and transmitting the received data to the second memory, the second power source configured to provide a second voltage to the control module for a first predetermined period in response to an interruption of the first voltage; and wherein, at a conclusion of the first predetermined period, the control module is configured to operate in an economy mode of operation comprising suspending receiving data from the communications network for a second predetermined period; and wherein the processor includes a set of integrated peripheral controllers, and wherein the economy mode of operation includes ceasing providing power to at least one of the integrated peripheral controllers for the predetermined second period.

2 . The CVFDR system of claim 1 , wherein in response to a restoration of the first voltage received from the remote first power source during the second predetermined period, the processor is configured to transition to the normal mode of operation including executing the program code read from the first memory and resuming a receipt of data from the communications network.

3 . The CVFDR system of claim 1 , wherein the economy mode of operation includes placing the first memory in a self-refresh mode.

4 . The CVFDR system of claim 1 , wherein the processor includes a set of central processing units (CPU), and wherein the economy mode of operation further includes ceasing providing power to at least one CPU for the second predetermined period.

5 . The CVFDR system of claim 1 , wherein the first predetermined period is based on a rate of decay of the second voltage with respect to time.

6 . The CVFDR system of claim 1 , wherein the control module is further communicatively coupled to a flight recorder module via the data communications network, and wherein the received data is provided by the flight recorder module.

7 . The CVFDR system of claim 1 , wherein the first memory is a synchronous dynamic random-access memory.

8 . The CVFDR system of claim 1 , wherein the second memory is remote from the CVFDR.

9 . The CVFDR system of claim 1 , wherein the second memory is one of NOR Flash or NAND Flash memory.

10 . The CVFDR system of claim 1 , wherein the first voltage and the second voltage are selectively provided to the CVFDR via a power controller device.

11 . A method of operating a CVFDR system of an aircraft, including a CVFDR having a control module comprising a processor communicatively coupled to a first memory and a second memory, the method comprising:
receiving, by the processor, a first voltage from a first power source remote from the CVFDR; executing, by the processor, program code read from the first memory; receiving, by the processor, a data signal indicative of operational data from a communications network; transmitting the operational data to the second memory; receiving a second voltage from a second power source in response to an interruption of the first voltage; operating the processor in a normal mode of operation for a first predetermined period; and at a conclusion of the first predetermined period, and operating the processor in an economy mode of operation for a second predetermined period; wherein the processor includes a set of integrated peripheral controllers, and wherein operating the processor in the economy mode of operation includes suspending providing power to at least one of the integrated peripheral controllers for the second predetermined period.

12 . The method of claim 11 , further comprising, in response to a restoration of the first voltage received from the first power source during the second predetermined period, resuming operation of the processor in accordance with the normal mode of operation.

13 . The method of claim 12 , wherein operating the processor in the economy mode of operation includes placing the first memory in a self-refresh mode, and wherein resuming operation of the processor in accordance with the normal mode of operation includes resuming execution of the program code read from the first memory.

14 . The method of claim 12 , wherein operating the processor in the economy mode of operation includes suspending receiving the data signal by the processor, and wherein resuming operation of the processor in accordance with the normal mode of operation includes resuming receiving the data signal by the processor.

15 . The method of claim 12 , wherein the processor includes a set of CPUs, and operating the processor in the economy mode of operation includes suspending providing power to at least one CPU for the second predetermined period, and wherein resuming operation of the processor in accordance with the normal mode of operation includes providing power to the at least one CPU.

16 . The method of claim 12 , wherein resuming operation of the processor in accordance with the normal mode of operation includes providing power to the at least one of the integrated peripheral controllers.

17 . The method of claim 11 , wherein the second power source is a capacitor.

18 . The method of claim 11 , wherein the first predetermined period is based on a rate of decay of the second voltage with respect to time.

19 . The method of claim 11 , wherein the data signal indicative of operational data is provided by a flight recorder module.

Assignees

• Gen Electric

Inventors

• Douthitt Brian Lynn
• Gerken Theodore William
• Stearley Samuel Nyall

Classifications

• H04L67/12

  specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks · CPC title

• B64D2045/0065

  Black boxes, devices automatically broadcasting distress signals · CPC title

• G07C7/00

  Details or accessories common to the registering or indicating apparatus of groups G07C3/00 and G07C5/00 · CPC title

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• G07C5/0841 Primary

  Registering performance data (recording measured values G01D; information storage G11B) · CPC title