Emergency mechanical and communication systems and methods for aircraft
First Claim
1. An aircraft flight data recorder ejection and landing system comprising:
- a flight data recorder comprising electronic storage for storing therein of at least data representative of a flight state of an aircraft;
an ejection system for rapid ejection of the flight data recorder from the aircraft, the ejection system comprising;
a housing comprising an internal cavity, the flight data recorder being positioned at least partially within the internal cavity;
an ejection system pressurized fluid source;
a fluid path fluidly coupled to the internal cavity of the housing and the ejection system pressurized fluid source; and
a valve operatively coupled to the fluid path to selectively allow pressurized fluid to flow from the ejection system pressurized fluid source to the internal cavity of the housing to cause ejection of the flight data recorder from the housing; and
a landing system for reducing landing impact forces and increasing buoyancy, the landing system coupled to the flight data recorder, the landing system comprising;
one or more landing system pressurized fluid sources;
a plurality of inflatable airbags configured to be disposed at least partially about an exterior surface of the flight data recorder when inflated, each of the plurality of inflatable airbags being selectively fluidly coupled to one or more of the one or more landing system pressurized fluid sources; and
a trigger mechanism configured to trigger one or more landing system valves to cause inflation of the plurality of inflatable airbags by the one or more landing system pressurized fluid sources upon occurrence of a condition,wherein the condition is based on at least one of the following;
a passage of time since ejection of the flight data recorder from the aircraft, detecting that the flight data recorder has passed below a predetermined altitude, and detecting a loss of communication with the aircraft.
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Accused Products
Abstract
A system for rapid separation of a flight data recorder from an aircraft comprises a flight data recorder; an emergency detection system comprising a plurality of sensors for detecting flight parameters and at least one computer processor for analyzing the flight parameters and determining, based on the analysis, that an emergency event is occurring; a rapid ejection system comprising a pneumatic system configured to eject the flight data recorder out of an opening in a housing and through the skin of the aircraft when the emergency detection system determines that the emergency event is occurring; and a soft landing system, said soft landing system being attached to the flight data recorder and configured to reduce force of impact upon landing and increase buoyancy of the flight data recorder.
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Citations
19 Claims
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1. An aircraft flight data recorder ejection and landing system comprising:
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a flight data recorder comprising electronic storage for storing therein of at least data representative of a flight state of an aircraft; an ejection system for rapid ejection of the flight data recorder from the aircraft, the ejection system comprising; a housing comprising an internal cavity, the flight data recorder being positioned at least partially within the internal cavity; an ejection system pressurized fluid source; a fluid path fluidly coupled to the internal cavity of the housing and the ejection system pressurized fluid source; and a valve operatively coupled to the fluid path to selectively allow pressurized fluid to flow from the ejection system pressurized fluid source to the internal cavity of the housing to cause ejection of the flight data recorder from the housing; and a landing system for reducing landing impact forces and increasing buoyancy, the landing system coupled to the flight data recorder, the landing system comprising; one or more landing system pressurized fluid sources; a plurality of inflatable airbags configured to be disposed at least partially about an exterior surface of the flight data recorder when inflated, each of the plurality of inflatable airbags being selectively fluidly coupled to one or more of the one or more landing system pressurized fluid sources; and a trigger mechanism configured to trigger one or more landing system valves to cause inflation of the plurality of inflatable airbags by the one or more landing system pressurized fluid sources upon occurrence of a condition, wherein the condition is based on at least one of the following;
a passage of time since ejection of the flight data recorder from the aircraft, detecting that the flight data recorder has passed below a predetermined altitude, and detecting a loss of communication with the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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10. A method of ejecting and landing an ejectable flight data recorder, the method comprising:
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monitoring a flight condition of an aircraft; initiating, responsive to detection of an abnormal flight condition, ejection of the flight data recorder from the aircraft, wherein the initiating comprises; transmitting at least data representative of a flight state of the aircraft to the flight data recorder; and opening a valve fluidly coupled to an ejection system pressurized fluid source, wherein opening the valve causes fluid from the pressurized fluid source to force the flight data recorder from a housing; deploying a descent control parachute coupled to the flight data recorder, the descent control parachute configured to reduce a descending rate of the flight data recorder; triggering, responsive to occurrence of a condition, inflation of a plurality of airbags, wherein the plurality of airbags are configured to be disposed at least partially about an exterior surface of the flight data recorder when inflated; detecting a water landing of the flight data recorder; and disconnecting the descent control parachute from the flight data recorder, responsive to detecting the water landing. - View Dependent Claims (11, 12, 13, 14)
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15. An aircraft flight data recorder ejection and landing system comprising:
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a flight data recorder comprising electronic storage for storing therein of at least data representative of a flight state of an aircraft; an ejection system for rapid ejection of the flight data recorder from the aircraft, the ejection system comprising; an ejection system pressurized fluid source; and an ejection valve operatively coupled to the ejection system pressurized fluid source to selectively allow pressurized fluid to flow from the ejection system pressurized fluid source to an expandable cavity adjacent the flight data recorder, wherein the expandable cavity is configured such that expansion of the cavity causes the flight data recorder to be ejected from the aircraft; and a landing system for reducing landing impact forces and increasing buoyancy, the landing system coupled to the flight data recorder, the landing system comprising; one or more landing system pressurized fluid sources; a plurality of inflatable airbags configured to be disposed about an exterior surface of the flight data recorder when inflated, each of the plurality of inflatable airbags being selectively fluidly coupled to one or more of the one or more landing system pressurized fluid sources; and a trigger mechanism configured to trigger one or more airbag valves to cause inflation of the plurality of inflatable airbags by the one or more landing system pressurized fluid sources. - View Dependent Claims (16, 17, 18, 19)
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Specification