Automatically ejecting flight data recorder

• US 8,493,715 B1
• Filed: 04/21/2010
• Issued: 07/23/2013
• Est. Priority Date: 09/11/2009
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Angelucci, Marc T.
• Primary Examiner(s): Lee, Benjamin P
• Application Number:
  US12/764,374
• Time in Patent Office: 1,189 Days
• Field of Search: 244/1.R, 701/14, 701/35, 312/223.2, 312/223.3, 361/679.01
• US Class Current: 361/679.01
• CPC Class Codes: B64D 2045/0065 Black boxes, devices automatically broadcasting distress signals
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: H05K 5/021 specially adapted for data recorders, e.g. for flight recorders
• CPC Class Codes: H05K 5/0213 Venting apertures; Constructional details thereof

Abstract

An apparatus for holding a flight data recorder in an aircraft includes a housing that defines a compartment enclosing the flight data recorder and a flotation device attached to the flight data recorder. If the aircraft crashes into a body of water and become submerged, one or more releasable fasteners holding the compartment'"'"'s cover in place are triggered thereby removing the cover over an opening in the compartment and ejecting the flotation device and the flight data recorder out of the compartment. The floatation device then floats the flight data recorder to the surface of the water where it can be located by the rescuers.

Claims

1. An apparatus for holding a flight data recorder in an aircraft comprising:

a housing for enclosing the flight data recorder, the housing provided with an opening for the flight data recorder to egress from the housing;

a cover for closing the opening when the cover is in a closed position;

one or more releasable fasteners holding the cover in the closed position and configured to open the cover when the one or more releasable fasteners are triggered; and

a pressurized flotation device provided within the housing and attached to the flight data recorder, wherein when the aircraft is under water, one or more releasable fasteners are triggered thereby opening the cover and the flotation device floats pulls the flight data recorder out of the housing and floats the flight data recorder to the surface of the water,

wherein the flight data recorder is attached to the flotation device such that the flight data recorder is contained inside the flotation device.

2. The apparatus of claim 1, wherein the one or more first releasable fasteners are explosive bolts that are triggered by an electrical trigger signal.

3. The apparatus of claim 1, wherein the lid is hingeably attached to the housing on one side thereof by a biased hinge and the one or more first releasable fasteners are provided on the opposite side thereof for holding the lid in closed position until the one or more releasable fasteners are triggered.

4. The apparatus of claim 1, further comprising one or more data links for connecting the flight data recorder to the aircraft.

5. The apparatus of claim 4, further comprising a means for disconnecting the flight data recorder from the one or more data links.

6. The apparatus of claim 5, wherein the means for disconnecting the flight data recorder is a compressed gas.

7. The apparatus of claim 5, wherein the means for disconnecting the flight data recorder from the one or more data links is a second releasable fastener.

8. The apparatus of claim 7, wherein the second releasable fastener is an explosive bolt that is triggered by an electrical trigger signal.

9. The apparatus of claim 1, wherein the housing is integrated into the aircraft'"'"'s fuselage.

10. The apparatus of claim 9, wherein a portion of the housing is formed by the aircraft'"'"'s fuselage.

11. An apparatus for holding a flight data recorder in an aircraft comprising:

a housing for enclosing the flight data recorder, the housing provided with an opening for the flight data recorder to egress from the housing;

a pressurized flotation device provided within the housing and attached to the flight data recorder,

wherein the floatation device is configured to exceed the size of the opening when pressurized to a predetermined pressure during normal operating conditions, and

wherein, when the aircraft is under water and the housing is at a predetermined depth, the floatation device is configured to decrease to a size less than that of the opening when the ambient water pressure contracts the pressurized flotation device causing the flotation device to egress from the housing through the opening and float the flight data recorder to the surface of the water.

12. The apparatus of claim 11, further comprising one or more data links for connecting the flight data recorder to the aircraft.

13. The apparatus of claim 12, further comprising a means for disconnecting the flight data recorder from the one or more data links.

14. The apparatus of claim 13, wherein the means for disconnecting the flight data recorder is a compressed gas.

15. The apparatus of claim 11, further comprising a flexible membrane for covering the opening, the membrane arranged within the housing and configured to egress from the housing with the floatation device when the housing is at the predetermined depth.

16. The apparatus of claim 11, wherein the housing is configured to be flooded with ambient water upon submersion such that the pressure within the housing is equalized with respect to that of the surrounding water.

17. The apparatus of claim 16, further comprising a valve for equalizing the pressure within the housing with respect to the surrounding water.

18. An apparatus for holding a flight data recorder in an aircraft comprising:

a housing for enclosing the flight data recorder, the housing provided with an opening for the flight data recorder to egress from the housing;

a pressurized flotation device provided within the housing and attached to the flight data recorder, wherein when the aircraft is under water and the housing is at a predetermined depth, the ambient water pressure contracts the pressurized flotation device causing the flotation device to egress from the housing through the opening and float the flight data recorder to the surface of the water,

wherein the flight data recorder is attached to the flotation device such that the flight data recorder is contained inside the flotation device.

19. An apparatus for holding a flight data recorder in an aircraft comprising:

a housing for enclosing the flight data recorder, the housing provided with an opening for the flight data recorder to egress from the housing;

a cover for closing the opening when the cover is in a closed position;

one or more releasable fasteners holding the cover in the closed position and configured to open the cover when the one or more releasable fasteners are triggered;

a valve for equalizing the pressure between the portion of the housing enclosing the flight data recorder and the ambient water; and

a flotation device provided within the housing and attached to the flight data recorder,

wherein when the aircraft is under water, the portion of the housing enclosing the flight data recorder is configured to be flooded with ambient water upon submersion, and one or more releasable fasteners are triggered thereby opening the cover and the flotation device floats pulls the flight data recorder out of the housing and floats the flight data recorder to the surface of the water.