Method and apparatus for a crash survivable flight data recorder

• US 20090112381A1
• Filed: 10/30/2007
• Published: 04/30/2009
• Est. Priority Date: 10/30/2007
• Status: Abandoned Application

• Current Assignee: Avidyne Corporation
• Original Assignee: Avidyne Corporation
• Inventors: Weihs, Joseph, Schwinn, Daniel J., Jacobson, Steven W.
• Application Number:
  US11/978,837
• Publication Number:
  US 20090112381A1
• Time in Patent Office: Days
• US Class Current: 701/14
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

Common practice in the aviation industry is to place a single Flight Data Recorder (FDR) in an aircraft for the purpose of aiding an investigation of an aircraft accident or incident. In contrast, a system employing ‘an example’ embodiment of the invention uses multiple flight data recorders by having a primary node or first FDR, and one or more secondary nodes or one or more additional FDRs configured to store flight data. Each FDR is placed in a different location so as to ensure backup of the recorded and stored data. In this way, the invention system provides redundancy of information for an aircraft accident or incident and more reliable data storage.

Claims

1. A system for storing flight data, comprising:

a primary node configured to store flight data of an aircraft; and

one or more secondary nodes configured to store flight data, where the one or more secondary nodes are located in a different location than the primary node; and

the primary node and one or more secondary nodes are located in existing network nodes in the aircraft.

2. A system as claimed in claim 1 wherein the primary node and the one or more secondary nodes are flight data recorders.

3. A system as claimed in claim 1 wherein the existing network nodes are on an internal aircraft data bus or network.

6. A system as claimed in claim 1 wherein a user obtains the flight data from the primary node or the one or more secondary nodes.

7. A system as claimed in claim 1 wherein the one or more secondary nodes stores substantially the same flight data by using one of the following:

make multiple copies, use parity storage, forward error correction encoding, or other suitable backup.

8. A system as claimed in claim 1 wherein the primary node and the one or more secondary nodes stores flight data without an increase in weight to the aircraft.

9. A system as claimed in claim 1 wherein the primary and the one or more secondary nodes are configured to collect and record the flight data using existing nodes in the aircraft.

4. A system as claimed in claim I wherein the flight data includes parameters for a flight data recorder.

5. A system as claimed in claim 4 wherein the parameters include any one or combination of the following:

time, pressure altitude, airspeed, vertical acceleration, magnetic heading, control-column position, rudder-pedal position, control-wheel position, horizontal stabilizer, fuel flow, or other data relating to the aircraft.

10. A method for storing flight data, comprising:

storing flight data for an aircraft in a primary node; and

storing substantially the same flight data in one or more secondary nodes, where the one or more secondary nodes are in the aircraft and in a different location than the primary node so as to allow a backup of the flight data.

11. A method as claimed in claim 10 wherein the primary node and the one or more secondary nodes are flight data recorders.

12. A method as claimed in claim 10 wherein the flight data includes parameters for a flight data recorder.

13. A method as claimed in claim 12 wherein the parameters include one of the following:

time, pressure altitude, airspeed, vertical acceleration, magnetic heading, control-column position, rudder-pedal position, control-wheel position, horizontal stabilizer, fuel flow, or other data relating to the aircraft.

14. A method as claimed in claim 10 wherein the primary node and the one or more secondary nodes uses existing nodes located on an internal aircraft data bus or network.

15. A method as claimed in claim 10 wherein a user obtains the flight data from the primary node or the one or more secondary nodes.

16. A method as claimed in claim 10 wherein the one or more secondary nodes stores substantially the same flight data by using one of the following:

making multiple copies, using parity storage, forwarding error correction encoding, or other suitable backup.

17. A method as claimed in claim 10 wherein the primary node and the one or more secondary nodes stores flight data without an increase in weight to the aircraft.

18. A method as claimed in claim 10 further comprising the steps of:

collecting the flight data using existing nodes in the aircraft; and

recording the collected flight data using existing nodes in the aircraft.

19. A system for storing working data of a subject vehicle, comprising:

a primary node means configured to store working data of a subject vehicle; and

one or more secondary node means for storing the working data, the one or more secondary node means each being located in a different location than the primary node means, and the primary node means and the one or more secondary node means being located in existing network nodes in the subject vehicle.

20. A system as claimed in claim 19 wherein:

the primary node means and the one or more secondary node means are data recorders; and

the working data includes parameters recordable by data recorders including any one or combination of the following;

time, pressure altitude, airspeed, vertical acceleration, magnetic heading, control-column position, rudder-pedal position, control-wheel position, horizontal stabilizer, fuel flow, or other data relating to the aircraft.