Ejectable flight data recorder unit
First Claim
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1. An apparatus for recording aircraft flight data, the apparatus comprising:
- a primary flight data recorder unit configured to record data generated by aircraft systems during operation of an aircraft; and
a secondary flight data recorder unit in communication with the primary flight data recorder and configured to receive and store data from the primary flight data recorder;
wherein the secondary flight data recorder unit is ejectable from the aircraft, and comprises a propulsion system to enable powered flight of the secondary flight data recorder unit;
wherein the secondary flight data recorder unit further comprises a guidance system configured to guide the secondary flight data recorder unit to a selected destination,wherein the selected destination comprises a land-based location nearest to a last recorded location of the aircraft, andwherein the land-based location nearest to the last recorded location of the aircraft is determined based on aircraft flight data most recently received, prior to ejection, by the secondary flight data recorder unit from the primary flight data recorder unit.
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Abstract
An apparatus for recording aircraft flight data including a primary flight data recorder unit for recording data generated by aircraft systems during operation of an aircraft and a secondary flight data recorder unit in communication with the primary flight data recorder unit. The secondary flight data recorder unit is configured to receive and store data from the primary flight data recorder. The secondary flight data recorder unit is ejectable from the aircraft, and comprises a propulsion system to enable powered flight of the secondary flight data recorder unit.
9 Citations
16 Claims
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1. An apparatus for recording aircraft flight data, the apparatus comprising:
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a primary flight data recorder unit configured to record data generated by aircraft systems during operation of an aircraft; and a secondary flight data recorder unit in communication with the primary flight data recorder and configured to receive and store data from the primary flight data recorder; wherein the secondary flight data recorder unit is ejectable from the aircraft, and comprises a propulsion system to enable powered flight of the secondary flight data recorder unit; wherein the secondary flight data recorder unit further comprises a guidance system configured to guide the secondary flight data recorder unit to a selected destination, wherein the selected destination comprises a land-based location nearest to a last recorded location of the aircraft, and wherein the land-based location nearest to the last recorded location of the aircraft is determined based on aircraft flight data most recently received, prior to ejection, by the secondary flight data recorder unit from the primary flight data recorder unit. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. An apparatus for recording aircraft flight data, the apparatus comprising:
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a primary flight data recorder unit configured to record data generated by aircraft systems during operation of an aircraft; and a secondary flight data recorder unit in communication with the primary flight data recorder and configured to receive and store data from the primary flight data recorder; wherein the secondary flight data recorder unit is ejectable from the aircraft, and comprises a propulsion system to enable powered flight of the secondary flight data recorder unit; wherein a total weight of the secondary flight data recorder unit is less than half of a total weight of the primary flight data recorder unit, and/or a largest dimension of the secondary flight data recorder unit is less than half of a largest dimension of the primary flight data recorder unit.
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10. An aircraft comprising:
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a primary flight data recorder unit configured to record data generated by aircraft systems during operation of an aircraft; a secondary flight data recorder unit in communication with the primary flight data recorder and configured to receive and store data from the primary flight data recorder, wherein the secondary flight data recorder unit is ejectable from the aircraft, and the secondary flight data recorder comprises a propulsion system to enable powered flight of the secondary flight data recorder unit; a conduit connecting a location of the secondary flight data recorder unit to the outside of the aircraft, the conduit configured to enable ejection of the secondary flight data recorder unit from the aircraft; and an ejection mechanism for ejecting the secondary flight data recorder unit from the aircraft via the conduit, wherein the ejection mechanism is configured to activate in response to a predetermined criterion being met, wherein the ejection mechanism comprises a compressed air source configured for selectably delivering compressed air into the conduit to create a suction force at the location of the secondary flight data recorder, wherein the compressed air source is configured to deliver compressed air into the conduit in response to a predetermined criterion being met. - View Dependent Claims (11, 12)
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13. An aircraft comprising:
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a primary flight data recorder unit configured to record data generated by aircraft systems during operation of an aircraft; and a secondary flight data recorder unit in communication with the primary flight data recorder and configured to receive and store data from the primary flight data recorder, wherein the secondary flight data recorder unit is ejectable from the aircraft, and comprises a propulsion system to enable powered flight of the secondary flight data recorder unit; a conduit connecting a location of the secondary flight data recorder unit to outside of the aircraft, wherein the conduit is configured to enable ejection of the secondary flight data recorder unit from the aircraft; and an ejection mechanism for ejecting the secondary flight data recorder unit from the aircraft via the conduit, wherein the ejection mechanism is configured to activate in response to a predetermined criterion being met, wherein the conduit comprises a first selectably openable door between an interior of the conduit and the outside of the aircraft, and a second selectably openable door between the location of the secondary flight data recorder unit and the interior of the conduit, wherein each of the first and second selectably openable doors is configured to open in response to the predetermined criterion being met.
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14. A method comprising:
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positioning an ejectable secondary flight data recorder unit in an aircraft adjacent a conduit in the aircraft and an ejection mechanism, wherein the conduit comprises a first selectably openable door between the an interior of the conduit and outside of the aircraft, and a second selectably openable door between the secondary flight data recorder unit in the aircraft and the interior of the conduit, wherein each of the first and second selectably openable doors are configured to open in response to a predetermined criterion being met, and the ejection mechanism is configured to eject the secondary flight data recorder through the conduit and out of the aircraft in response to the predetermined criterion being met; receiving aircraft flight data at a primary flight data recorder unit; and sending, by the primary flight data recorder unit, at least some of the received aircraft flight data to a secondary flight data recorder unit, wherein the secondary flight data recorder unit is ejectable from the aircraft and comprises a propulsion system to enable powered flight of the secondary flight data recorder unit.
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15. An assembly configured to be mounted in an aircraft and comprising:
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a primary flight data recorder unit configured to record data generated by aircraft systems during operation of the aircraft, wherein the primary flight data recorder unit is fixed to the aircraft and lacks a propulsion device; and a secondary flight data recorder unit releasably mounted to the aircraft, and configured for data communication with the primary flight data recorder and configured to receive and store data from the primary flight data recorder; and a propulsion system included with the secondary flight data recorder unit, wherein the secondary flight data recorder unit is ejectable from the aircraft and the secondary flight data recorder unit is configured to be propelled by the propulsion system after ejected from the aircraft, a conduit configured to convey the secondary flight data recorder unit to outside of the aircraft, wherein the conduit comprises a first selectably openable door between the an interior of the conduit and the outside of the aircraft and a second selectably openable door between the location of the secondary flight data recorder unit and the interior of the conduit, wherein each of the first and second selectably openable doors is configured to open in response to a predetermined criterion being met, and an ejection mechanism configured to eject the secondary flight data recorder unit from the aircraft via the conduit, wherein the ejection mechanism is configured to activate in response to the predetermined criterion being met. - View Dependent Claims (16)
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Specification