JPWO2019089597A5

JPWO2019089597A5 -

Info

Publication number: JPWO2019089597A5
Application number: JP2020524071A
Authority: JP
Publication date: 2024-04-10

Description

各メモリユニット４２０は、更にビーコン４２８を有していてもよい。このビーコンを装着して、位置又は他の情報、若しくは信号を送信することで、対応するメモリユニット４２０の回収を可能にすることができる。 Each memory unit 420 may further include a beacon 428 that may be equipped to transmit location or other information or signals to allow retrieval of the corresponding memory unit 420.

Claims

An aircraft recorder installed in the aircraft;
a plurality of memory units provided on the aircraft and installed remotely from the aircraft recorder;
a plurality of transceivers corresponding to each of the plurality of memory units;
an Ethernet network connecting the aircraft recorder, the memory units, and the transceivers;
Each of the plurality of memory units has a locator beacon configured to facilitate retrieval of a corresponding memory unit, and the system is configured to receive both audio data and flight data streaming from the aircraft recorder via the Ethernet network and a corresponding transceiver of the plurality of transceivers.

The system of claim 1, wherein the Ethernet network includes at least one of a copper wire network, a fiber optic network, or a wireless network.

The system of claim 1, wherein the plurality of memory units are powered by a power source from the aircraft recorder.

10. The system of claim 1, wherein the plurality of memory units can be destroyed by at least one of an impact of less than 3400 G (1 G=9.8 m/ ^s2 ) or a temperature of less than 1000 degrees Celsius.

The system of claim 1, wherein the memory units are spatially separated from one another and from the aircraft recorder using multiple antennas that are spatially separated from one another.

Further, another aircraft recorder installed on the aircraft;
a second plurality of memory units provided on the aircraft and located remotely from the second aircraft recorder;
10. The system of claim 1, wherein the other memory unit is configured to stream audio data and flight data from the other aircraft recorder over the Ethernet network.

acquiring voice data and flight data corresponding to the aircraft with an aircraft recorder installed in the aircraft;
streaming the voice data and flight data from the aircraft recorder via an Ethernet network and corresponding ones of a plurality of transceivers connected to the Ethernet network to a plurality of memory units located on the aircraft and remotely located from the aircraft recorder;
The method, wherein each of the plurality of memory units has a locator beacon configured to aid in retrieval of a corresponding memory unit.

8. The method of claim 7, wherein the Ethernet network includes at least one of a copper wire network, a fiber optic network, or a wireless network.

The method of claim 7, further comprising powering the plurality of memory units by the aircraft recorder.

8. The method of claim 7, wherein the plurality of memory units can be destroyed by at least one of an impact of less than 3400 G (1 G=9.8 m/ ^s2 ) or a temperature of less than 1000 degrees Celsius.

The method of claim 7, wherein the memory units are spatially separated from one another and from the aircraft recorder using multiple antennas that are spatially separated from one another.

At least one processor;
at least one memory containing computer program code,
The at least one memory and the computer program code are configured to cause the at least one processor to program the device to at least:
acquiring voice data and flight data corresponding to the aircraft using an aircraft recorder installed in the aircraft;
configured to stream the voice data and flight data from the aircraft recorder via an Ethernet network and corresponding ones of a plurality of transceivers connected to the Ethernet network to a plurality of memory units provided on the aircraft and remotely located from the aircraft recorder;
An apparatus, wherein each of the plurality of memory units has a locator beacon configured to facilitate retrieval of a corresponding memory unit.

The apparatus of claim 12, wherein the Ethernet network includes at least one of a copper wire network, a fiber optic network, or a wireless network.

The device of claim 12, wherein the at least one memory and the computer program code are configured by the at least one processor to cause the device to power at least the plurality of memory units by the aircraft recorder.

13. The apparatus of claim 12, wherein the plurality of memory units can be destroyed by at least one of an impact of less than 3400 G (1 G = 9.8 m/ ^s2 ) or a temperature of less than 1000 degrees Celsius.

The apparatus of claim 12, wherein the memory units are spatially separated from one another and from the aircraft recorder using multiple antennas that are spatially separated from one another.