Aircraft safety apparatus

Claim 2

In safety apparatus for use on aircraft to facilitate the in-flight maneuvering thereof to help overcome the malfunctioning thereof, the combination comprising: front parachute means mounted operatively at the front portions of the aircraft for adding to the buoyancy of the aircraft during landings thereof; rear parachute means mounted operatively at the rear portion of the aircraft for adding to the buoyancy of the aircraft during the landing thereof; means for moving said front and rear parachute means into their operating position; a plurality of auxiliary jet propulsion units containing fluid under pressure for propelling the aircraft to aid in its manueverability; port means of at least some of said auxiliary jet propulsion units mounted on the aircraft to direct fluid under pressure laterally away therefrom to cause lateral reaction movement of the aircraft for steering purposes; said means for moving said front and rear parachute means into their operating position includes an ejection assembly, said assembly including a storage compartment for one of said parachute means, the floor of the aircraft having an opening therein, a movable floor door means for covering over the opening in the floor with said storage compartment being stored beneath said floor, means defining an opening in the ceiling of the body of the aircraft, and a movable ceiling door means for covering over the opening in the ceiling, means for raising said compartment from beneath the floor through the opening therein to said opening in said ceiling, and means for ejecting the contents of the compartment through the opening in the ceiling of the aircraft, wherein said means for ejecting includes parachute ejecting spring means and an electrical solenoid for maintaining said spring means in a retracted position.

Claim 3

The combination according to claim 1, further including an ejection assembly control circuit, said ejection assembly control circuit being responsive to an initiation signal, said ejection assembly control circuit further including means for causing the opening of said ceiling door means, means for causing the opening of said floor door means, means for causing the raising of said compartment, means for triggering the release of said means for ejecting the contents of said compartment.

Claim 4

The combination according to claim 2, wherein said means for raising said compartment includes a plurality of nuts fixed to the exterior of said compartment, a plurality of motor-driven vertically disposed threaded rods extending through corresponding ones of said nuts so that, when said threaded rods are driven about their vertical axes, the nuts are driven upwardly to carry said compartment therewith.

Claim 5

In safety apparatus for use on aircraft to facilitate the in-flight maneuvering thereof to help overcome the malfunctioning thereof, the combination comprising: front parachute means mounted operatively at the front portions of the aircraft for adding to the buoyancy of the aircraft during landings thereof; rear parachute means mounted operatively at the rear portion of the aircraft for adding to the buoyancy of the aircraft during the landing thereof; means for moving said front and rear parachute means into their operating position; a plurality of auxiliary jet propulsion units containing fluid under pressure for propelling the aircraft to aid in its maneuverability; port means of at least some of said auxiliary jet propulsion units mounted on the aircraft to direct fluid under pressure laterally away therefrom to cause lateral reaction movement of the aircraft for steering purposes, downwardly directed port means of at least some of said auxiliary jet propulsion units mounted on the aircraft to direct fluid under pressure downwardly away therefrom to cause upward reaction movement of the aircraft for steering purposes, and a jet propulsion unit control circuit, said circuit including a plurality of gravity switch means for activating selectively the auxiliary jet propulsion unit when the aircraft assumes a preselected downwardly directed attitude, wherein said control circuit further includes a series of electrically energizable valves individually associated with said auxiliary jet propulsion units, a battery for energizing selectively said valves, relay switch means for switching batteries to said valves, an ON switch for connecting said battery to said relay switch means, an OFF switch for disconnecting the battery, a low speed switch connected in parallel with said ON switch for connecting the battery to said relay switch means when the speed of the aircraft falls below a predetermined value, power failure relay means responsive to a power failure to connect the battery to said relay switch means.

Claim 6

In safety apparatus for use on aircraft to facilitate the in-flight maneuvering thereof to help overcome the malfunctioning thereof, the combination comprising: front parachute means mounted operatively at the front portions of the aircraft for adding to the buoyancy of the aircraft during landings thereof; rear parachute means mounted operatively at the rear portion of the aircraft for adding to the buoyancy of the aircraft during the landing thereof; means for moving said front and rear parachute means into their operating position; a plurality of auxiliary jet propulsion units containing fluid under pressure for propelling the aircraft to aid in its maneuverability; port means of at least some of said auxiliary jet propulsion units mounted on the aircraft to direct fluid under pressure laterally away therefrom to cause lateral reaction movement of the aircraft for steering purposes, downwardly directed port means of at least some of said auxiliary jet propulsion units mounted on the aircraft to direct fluid under pressure downwardly away therefrom to cause upward reaction movement of the aircraft for steering purposes, and a jet propulsion unit control circuit, said circuit including a plurality of gravity switch means for activating selectively the auxiliary jet propulsion unit when the aircraft assumes a preselected downwardly directed attitude, wherein said control circuit further includes a series of electrically energizable valves individually associated with said auxiliary jet propulsion units, a battery for energizing selectively said valves, relay switch means for switching batteries to said valves, an ON switch for connecting said battery to said relay switch means, an OFF switch for disconnecting the battery, a low speed switch connected in parallel with said ON switch for connecting the battery to said relay switch means when the speed of the aircraft falls below a predetermined value, power failure relay means responsive to a power failure to connect the battery to said relay switch means.

Claim 7

The combination according to claim 4, wherein at least some of said jet propulsion units are mounted at the front and rear portions of the aircraft and at the tips of the wings thereof.

Claim 8

The combination according to claim 4, further including inflatable pontoons for supporting the aircraft on a body of water during emergency landing procedures, a plurality of telescoping shock-absorbing legs to facilitate the emergency landing of the aircraft on hard ground.

Claim 9

The combination according to claim 4, wherein said means for moving said front and rear parachute means into their operating position includes an ejection assembly, said assembly including a storage compartment for one of said parachute means, means defining an opening in the ceiling of the body of the aircraft, means for raising said compartment to said opening in said ceiling, means for ejecting the contents of the compartment through the opening in the ceiling of the aircraft.