Aircraft restraint systems with fixed default mode

1. A modal restraint system including a plurality of seatbelt subsystems, each seatbelt subsystem configured to secure an occupant of a seat of an aircraft, comprising:

a master release selector in communication with each of the seatbelt subsystems;

wherein, each seatbelt subsystem comprises:

a strap feeder unit; and

a strap selectively retractable into and extendable from the strap feeder unit, the strap positionable adjacent to the occupant so as to at least partially dispose the occupant between the strap and the seat;

wherein, the strap feeder unit is adapted to switch between a plurality of modes including a fixed mode and an unfixed mode, the strap substantially unextendable from the strap feeder unit in the fixed mode, the strap extendable from and retractable into the strap feeder unit in the unfixed mode;

wherein, the strap feeder unit is in the fixed mode by default;

wherein, the strap feeder unit is operable to switch to the unfixed mode in response to a user input, thereby increasing freedom of movement of the occupant relative to the seat of the aircraft; and

wherein, the master release selector is selectable to switch the strap feeder unit of each seatbelt subsystem to the unfixed mode.

2. The modal restraint system as recited in claim 1 wherein the strap feeder unit further comprises a spool operable to rotate in first and second directions to wind and unwind the strap thereabout, respectively.

3. The modal restraint system as recited in claim 2 wherein the strap feeder unit further comprises a locking module, the locking module engaging with the spool when the strap feeder unit is in the fixed mode to impede the spool from rotating in the second direction such that the strap is substantially unextendable.

4. The modal restraint system as recited in claim 2 wherein the plurality of modes further comprise a retracted fixed mode and the strap feeder unit further comprises a retraction module adapted to rotate the spool in the first direction to retract the strap into the strap feeder unit in the retracted fixed mode, thereby tightening the strap against the occupant.

5. The modal restraint system as recited in claim 2 wherein the unfixed mode is an inertia reel mode; and

wherein the strap feeder unit further comprises an inertia reel subassembly selectively engagable with the spool in the inertia reel mode.

6. The modal restraint system as recited in claim 1 wherein the strap further comprises a torso strap positionable adjacent to the torso of the occupant and a lap strap positionable adjacent to the lap region of the occupant.

7. The modal restraint system as recited in claim 1 wherein the plurality of modes further comprise a retracted fixed mode and wherein the strap feeder unit is adapted to retract the strap into the strap feeder unit in the retracted fixed mode, thereby tightening the strap against the occupant.

8. The modal restraint system as recited in claim 1 wherein the strap feeder unit is further operable to return to the fixed mode in response to a cessation of the user input.

9. The modal restraint system as recited in claim 1 wherein the strap feeder unit is further operable to return to the fixed mode in response to a cessation of a predetermined time period.

10. The modal restraint system as recited in claim 1 wherein the strap feeder unit automatically returns to the fixed mode in response to a precautionary event.

11. The modal restraint system as recited in claim 1 further comprising a release selector in communication with the strap feeder unit and wherein the user input further comprises selection of the release selector by the occupant.

12. The modal restraint system as recited in claim 11 wherein the release selector is switchable between a release position and an unrelease position; and

wherein the user input further comprises switching the release selector from the unrelease position to the release position.

13. The modal restraint system as recited in claim 11 wherein the release selector further comprises an input device selected from the group consisting of a button, a lever, a knob or a pull cord.

14. The modal restraint system as recited in claim 11 wherein the release selector is proximate to the seat.

15. The modal restraint system as recited in claim 11 wherein the release selector is disabled in response to a precautionary event, thereby preventing the strap feeder unit from switching to the unfixed mode.

16. An aircraft comprising:

a fuselage;

a plurality of seats in the fuselage; and

a modal restraint system including a plurality of seatbelt subsystems and a master release selector in communication with each of the seatbelt subsystems, each seatbelt subsystem adapted to secure an occupant to one of the seats, each seatbelt subsystem comprising:

a strap feeder unit; and

a strap selectively retractable into and extendable from the strap feeder unit, the strap positionable adjacent to the occupant so as to at least partially dispose the occupant between the strap and the seat;

wherein, the strap feeder unit is adapted to switch between a plurality of modes including a fixed mode and an unfixed mode, the strap substantially unextendable from the strap feeder unit in the fixed mode, the strap extendable from and retractable into the strap feeder unit in the unfixed mode;

wherein, the strap feeder unit is in the fixed mode by default;

wherein, the strap feeder unit is operable to switch to the unfixed mode in response to a user input, thereby increasing freedom of movement of the occupant relative to the seat; and

wherein, the master release selector is selectable to switch the strap feeder unit of each seatbelt subsystem to the unfixed mode.

17. The aircraft as recited in claim 16 wherein the fuselage further comprises a cockpit; and

wherein the master release selector is located in the cockpit.

18. The aircraft as recited in claim 16 wherein the plurality of modes further comprise an inertia reel unfixed mode and a retracted fixed mode; and

wherein the strap feeder units of each of the seatbelt subsystems are operable to switch to the retracted fixed mode in response to a precautionary event.

19. The aircraft as recited in claim 16 further comprising:

a release selector in communication with the strap feeder unit; and

a plurality of flight operation modes including a visual flight rules operation mode and an instrument flight rules operation mode;

wherein the release selector is disabled in response to switching to the instrument flight rules operation mode.