Ejectable flight data recorder systems, methods, and devices

• US 9,738,398 B1
• Filed: 04/28/2017
• Issued: 08/22/2017
• Est. Priority Date: 01/27/2017
• Status: Active Grant

• Current Assignee: Comac America Corporation
• Original Assignee: Comac America Corporation
• Inventors: Wang, Mingwei, Lane, Richard, Harris, Don, Li, Chen
• Primary Examiner(s): Baghdasaryan, Hovhannes
• Application Number:
  US15/581,567
• Time in Patent Office: 116 Days
• CPC Class Codes: B64D 1/12 Releasing
• CPC Class Codes: B64D 1/14 Absorbing landing shocks
• CPC Class Codes: B64D 2045/0065 Black boxes, devices automatically broadcasting distress signals
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 25/08 Ejecting or escaping means escape apertures B64C
• CPC Class Codes: B64D 25/20 Releasing of crash position indicators
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G01S 1/725 Marker, boundary, call-sign or like beacons transmitting signals not carrying directional information
• CPC Class Codes: G01S 15/66 Sonar tracking systems
• CPC Class Codes: G01S 15/88 Sonar systems specially adapted for specific applications seismic or acoustic prospecting or detecting G01V1/00
• CPC Class Codes: G01S 19/14 specially adapted for specific applications
• CPC Class Codes: G01S 2201/04 Emergencies
• CPC Class Codes: G01S 7/003 Transmission of data between radar, sonar or lidar systems and remote stations
• CPC Class Codes: G10K 11/006 Transducer mounting in underwater equipment, e.g. sonobuoys
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

An ejectable flight data recorder for robust retention of flight data and aiding in locating an aircraft after an emergency situation comprises: a buoyant housing comprising an internal cavity, a door for access to at least a portion of the internal cavity, and an aerodynamic outer shape having a longitudinal axis; an energy-dissipating nose cone for reducing an impact load on the housing when the flight data recorder impacts a water surface; a nonvolatile memory configured to store flight data; a position sensor for detecting a geographic position of the flight data recorder; a radio transmitter; an antenna electrically coupled to the radio transmitter; a sustainable power system; and a hydrophone for acoustically tracking a sinking trajectory of the aircraft in a body of water.

Claims

1. An ejectable flight data recorder for robust retention of flight data and aiding in locating an aircraft after an emergency situation in a remote location over a body of water, the ejectable flight data recorder comprising:

a buoyant housing configured to provide shock and heat protection to components positioned within the housing;

a nonvolatile memory positioned within the housing, the nonvolatile memory configured to store flight data comprising at least duplicated data from a conventional flight data recorder and a cockpit voice recorder;

an energy-dissipating nose cone positioned at a distal end of the housing for reducing an impact load on the housing and components positioned within the housing when the ejectable flight data recorder impacts a water surface;

a distress signal generating circuit positioned within the housing;

an antenna electrically coupled to the distress signal generating circuit, wherein the distress signal generating circuit is configured to transmit via the antenna a distress signal to a satellite;

at least three hydrophones configured to be deployable from the housing and suspended beneath the housing after a water landing of the ejectable flight data recorder; and

one or more computer processors programmed to analyze acoustic information received by the at least three hydrophones to estimate a sinking trajectory of the aircraft in a body of water.

2. The ejectable flight data recorder of claim 1, further comprising a water sensor configured to detect the water landing of the ejectable flight data recorder and to cause deployment of the at least three hydrophones and activation of the distress signal generating circuit.

3. The ejectable flight data recorder of claim 1, further comprising:

a hydrophone separation structure comprising a spring positioned to separate the at least three hydrophones from each other after deployment from the housing,

wherein the at least three hydrophones are configured to detect a signal transmitted by an underwater locator beacon of the aircraft.

4. The ejectable flight data recorder of claim 1, further comprising at least one sonar sensor for tracking the sinking trajectory of the aircraft.

5. The ejectable flight data recorder of claim 1, further comprising:

a first orientation sensor for detecting an orientation of the housing with respect to an environment; and

a second orientation sensor for detecting an orientation of one or more of the at least three hydrophones with respect to the environment or the housing.

6. The ejectable flight data recorder of claim 1, wherein the nonvolatile memory is further configured to store data relating to an orientation and position of the ejectable flight data recorder.

7. The ejectable flight data recorder of claim 1, further comprising:

a sustainable power system for providing backup electrical power, the sustainable power system comprising a solar panel array.

8. The ejectable flight data recorder of claim 1, further comprising:

a sustainable power system for providing backup electrical power, the sustainable power system comprising an electrochemical salt water generator.

9. The ejectable flight data recorder of claim 1, further comprising:

a sustainable power system for providing backup electrical power, the sustainable power system comprising a kinematic movement based generator.

10. The ejectable flight data recorder of claim 1, wherein the antenna comprises a combination of horizontally and vertically oriented elements.

11. The ejectable flight data recorder of claim 1, wherein the housing comprises an aerodynamically stable shape.

12. The ejectable flight data recorder of claim 1, wherein the energy-dissipating nose cone comprises a plurality of interconnected voids to enable crumpling of the nose cone to absorb energy when the ejectable flight data recorder impacts the water surface, the plurality of interconnected voids comprising a honeycomb configuration.

13. The ejectable flight data recorder of claim 1, wherein the buoyant housing comprises an aerodynamically stable shape having a longitudinal axis, the housing further comprising a flat outer surface oriented parallel to the longitudinal axis, a center of gravity of the ejectable flight data recorder being positioned such that the flat outer surface will tend to be oriented in an upward direction when the buoyant housing is floating in the body of water.

14. The ejectable flight data recorder of claim 7, wherein the housing comprises a polycarbonate material.

15. The ejectable flight data recorder of claim 1, wherein the housing comprises a plurality of composite materials.

16. The ejectable flight data recorder of claim 1, wherein the nonvolatile memory is further configured to store at least thirty minutes of data relating to a position of the ejectable flight data recorder.

17. The ejectable flight data recorder of claim 1, further comprising one or more position sensors for detecting a geographic position of the ejectable flight data recorder, wherein the one or more position sensors comprises at least one of the following:

a global positioning system (GPS) sensor, a GLONASS sensor, an inertia based sensor, an altimeter, a barometer, or a compass.

18. The ejectable flight data recorder of claim 1, further comprising a visual warning system comprising one or more of a laser or LED light source configured to project light from the ejectable flight data recorder after the ejectable flight data recorder is deployed from the aircraft.

19. The ejectable flight data recorder of claim 1, further comprising an audible warning system configured to generate a sound as the ejectable flight data recorder descends after being deployed from the aircraft, the audible warning system comprising at least one of the following:

one or more holes in an exterior surface of the housing sized and positioned to cause air passing therethrough to generate a sound, a whistle, a siren, or a speaker.