Thermal isolation of flight recorder memory core
Various systems may benefit from appropriate thermal protection. For example, various flight recorder systems may benefit from thermal isolation of a flight recorder memory core. A system can include a memory core of a flight recorder. The system can also include an inner chamber housing the memory core. The system can further include an outer chamber housing the inner chamber with a vacuum between the inner chamber and the outer chamber. The system can additionally include a signal path from avionics equipment to the memory core through the outer chamber and the inner chamber. The system can also include a power path for the memory core through the outer chamber and the inner chamber.
1. A system, comprising:
a memory core;
an inner chamber housing the memory core;
an outer chamber housing the inner chamber with a vacuum between the inner chamber and the outer chamber; and
a first relay within the outer chamber configured to selectively connect and disconnect power from outside the outer chamber to the memory core,
wherein an outer surface of the inner chamber is coated with a material that is configured to reflect heat.
2. The system of claim 1 , further comprising:
a fiber optic signal path from outside the outer chamber to the memory core.
3. The system of claim 1 , further comprising:
a second relay within the outer chamber configured to selectively connect and disconnect a signal path from outside the outer chamber to the memory core.
4. The system of claim 1 , further comprising:
a heat sink within the inner chamber and configured to remove heat from integrated circuits of the memory core.
5. The system of claim 1 , wherein the inner chamber and the outer chamber are cylinders, concentric boxes, or concentric spheres.
6. The system of claim 1 , wherein the inner chamber is set off from the outer chamber by one or more insulating supports.
7. The system of claim 1 , wherein outer chamber comprises stainless steel or titanium.
8. The system of claim 1 , wherein an inner surface of the outer chamber is coated with a material that is configured to absorb radiant heat.
9. The system of claim 1 , wherein the inner chamber comprises stainless steel or titanium.
10. The system of claim 1 , further comprising an underwater locater beacon.
11. The system of claim 10 , wherein the underwater locater beacon is located at one end of the outer chamber.
12. The system of claim 1 , further comprising:
a ballistic casing provided around the outer core.
13. The system of claim 12 , wherein the ballistic casing comprises an aluminum honeycomb structure.