Intelligent ballistic parachute system with fuel discharge
View Patent ↗A method performed by an aircraft, the aircraft including a wing, aircraft fuel, and a whole-aircraft parachute that is coupled to the aircraft. The method comprises: deploying the whole-aircraft parachute while the aircraft is in flight; and after deploying the parachute, but before the aircraft contacts the earth or any object coupled to the earth, discharging at least a portion of the aircraft fuel from the wing of the aircraft.
1. A method performed by an aircraft, the aircraft including a wing, aircraft fuel, and a whole-aircraft parachute that is coupled to the aircraft, the method comprising:
receiving a single request from an aircraft occupant;
based upon the receipt of the single request, both deploying the whole-aircraft parachute while the aircraft is in flight and also discharging at least a portion of the aircraft fuel from the wing of the aircraft.
2. The method of claim 1 , wherein the aircraft includes retractable landing gear, and the method further includes, based upon the receipt of the single request, also extending the landing gear.
3. The method of claim 1 , wherein the discharging at least a portion of the aircraft fuel includes:
creating a fuel discharge passageway for discharging the at least a portion of the aircraft fuel from the wing of the aircraft.
4. The method of claim 1 , wherein the aircraft includes a lower wing skin and a panel coupled to the lower wing skin, and wherein the discharging the at least a portion of the aircraft fuel from the wing of the aircraft includes creating a fuel discharge passageway between the lower wing skin and the panel.
5. A method performed by an aircraft, the aircraft including a wing, aircraft fuel, and a whole-aircraft parachute that is coupled to the aircraft, the method comprising:
deploying the whole-aircraft parachute while the aircraft is in flight; and after deploying the parachute, but before the aircraft contacts the earth or any object coupled to the earth, discharging at least a portion of the aircraft fuel from the wing of the aircraft;
wherein the aircraft includes a lower wing skin and a panel coupled to the lower wing skin and wherein the method further includes:
during the deployment of the whole-aircraft parachute, tensioning a strap that couples the aircraft to the parachute, and tensioning a cable, which is coupled to the strap and the panel.
6. A method performed by an aircraft, the aircraft including a wing, aircraft fuel, and a whole-aircraft parachute that is coupled to the aircraft, the method comprising:
deploying the whole-aircraft parachute while the aircraft is in flight; and after deploying the parachute, but before the aircraft contacts the earth or any object coupled to the earth, discharging at least a portion of the aircraft fuel from the wing of the aircraft;
wherein the aircraft includes a lower wing skin and a panel coupled to the lower wing skin and wherein the method further includes:
during the deployment of the whole-aircraft parachute, tensioning a strap that couples the aircraft to the parachute and tensioning a cable, which is coupled to the strap and the panel; and
then creating a fuel discharge passageway for discharging the at least a portion of the aircraft fuel from the wing of the aircraft.
7. The method of claim 1 , wherein the aircraft includes a lower wing skin and a panel coupled to the lower wing skin and wherein the method further includes:
during the deployment of the whole-aircraft parachute, rotating the panel with respect to at least a portion of the lower wing skin.
8. The method of claim 1 , wherein the aircraft includes a lower wing skin and a panel coupled to the lower wing skin and wherein the method further includes:
during the deployment of the whole-aircraft parachute, translating the panel with respect to at least a portion of the lower wing skin.
9. A method performed by an aircraft, the aircraft including a wing, aircraft fuel, and a whole-aircraft parachute that is coupled to the aircraft, the method comprising:
deploying the whole-aircraft parachute while the aircraft is in flight; and after deploying the parachute, but before the aircraft contacts the earth or any object coupled to the earth, discharging at least a portion of the aircraft fuel from the wing of the aircraft;
wherein the aircraft includes a lower wing skin and a panel coupled to the lower wing skin by a joint that includes epoxy and wherein the method further includes:
during the deployment of the whole-aircraft parachute, breaking at least a portion of the epoxy joint between the panel and the lower wing skin.
10. The method of claim 1 , wherein the aircraft includes anti-icing fluid and wherein the method further includes;
based upon the receipt of the single request, also discharging at least a portion of the anti-icing fluid from the aircraft.
11. An aircraft including:
a whole-aircraft parachute;
a harness containing a plurality of straps that couple the whole-aircraft parachute to a plurality of locations on the aircraft;
aircraft fuel; and
a fuel discharge system;
wherein the aircraft is operative to receive a single request from an occupant of the aircraft, and both deploy the whole-aircraft parachute and also discharge at least a portion of the aircraft fuel based upon the receipt of the single request.
12. An aircraft including:
a parachute;
a harness containing a plurality of straps that couple the parachute to a plurality of locations on the aircraft
aircraft fuel; and
a fuel discharge system operative to discharge at least a portion of the aircraft fuel, after deployment of the parachute while the aircraft is in flight, but before the aircraft contacts the earth or any object coupled to the earth;
wherein the fuel discharge system includes:
a wing that contains a fuel tank that stores the aircraft fuel, a first portion of the fuel tank being formed by a lower wing skin, a second portion of the fuel tank being formed by a panel that is coupled to the lower wing skin and separately coupled to at least one of the plurality of straps.
13. The aircraft of claim 12 , wherein the panel is separately coupled to the at least one of the plurality of straps by a first cable, a pass-through assembly and a second cable.
14. The aircraft of claim 13 , wherein the pass-through assembly includes a tube, a pass-through, and an o-ring that is located between the tube and the pass-through.
15. The aircraft of claim 14 , wherein the tube is coupled to a wing rib that forms a third portion of the fuel tank.
16. The aircraft of claim 12 , wherein the panel is coupled to the lower wing skin via an epoxy joint that includes micro.
17. The aircraft of claim 11 , wherein the fuel discharge system creates a fuel discharge passageway after deployment of the parachute while the aircraft is in flight, but before the aircraft contacts the earth or any object coupled to the earth.
18. The aircraft of claim 11 , further comprising:
anti-icing fluid; and
an anti-icing fluid discharge system;
wherein the aircraft is also operative to discharge at least a portion of the anti-icing fluid, based upon the receipt of the single request.
19. The aircraft of claim 11 , further comprising a processor coupled to a sensor that provides the processor with data that indicates whether the parachute has been deployed.
20. The aircraft of claim 11 , further comprising a ballistic parachute activation interface and a processor coupled to the ballistic parachute activation interface via a communication interface.
21. An aircraft including:
a whole-aircraft parachute;
a harness containing a plurality of straps that couple the whole-aircraft parachute to a plurality of locations on the aircraft; and
retractable landing gear;
wherein the aircraft is operative to receive a single request from an occupant of the aircraft, and based upon the receipt of the single request, both deploy the whole-aircraft parachute and also extend the landing gear.
22. A method performed by an aircraft, the aircraft including a wing, retractable landing gear, and a whole-aircraft parachute that is coupled to the aircraft, the method comprising:
receiving a single request from an occupant of the aircraft; and
based upon the receipt of the single request, both deploying the whole-aircraft parachute and also extending the landing gear.
23. An aircraft including:
a whole-aircraft parachute;
a harness containing a plurality of straps that couple the whole-aircraft parachute to a plurality of locations on the aircraft; and
anti-icing fluid;
wherein the aircraft is operative to receive a single request from an occupant of the aircraft, and based upon the receipt of the single request, both deploy the whole-aircraft parachute and also discharge at least a portion of the anti-icing fluid from the aircraft.
24. A method performed by an aircraft, the aircraft including a wing, anti-icing fluid, and a whole-aircraft parachute that is coupled to the aircraft, the method comprising:
receiving a single request from an occupant of the aircraft; and
based upon the receipt of the single request, both deploying the whole-aircraft parachute and also discharging at least a portion of the anti-icing fluid from the aircraft.