RESTRAINT SYSTEM AND METHOD FOR OPERATING SAME

Abstract

The invention relates to a restraint system (11) for an aircraft seat (10), comprising a restraint belt (3) and a belt retractor (2) for winding up the restraint belt (3) and allowing the restraint belt (3) to be extracted, further comprising a blocking device (1) for blocking the belt retractor (2) such that the restraint belt (3) cannot be extracted, wherein the blocking device is connectable to a signal (S) used to issue audible and/or visual output (6) inviting passengers to fasten seat belts (3), wherein the blocking device (1) is configured to interact with the seat belt retractor (2) such that the seat belt retractor (2) prevents further extraction of the seat belt (3) while the signal (S) is active. Furthermore, the invention relates to a method for operating a restraint system.

Claims

1. A restraint system for a seat, the restraint system comprising: a restraint belt; and a belt retractor for winding up the restraint belt and allowing the restraint belt to be extracted; and a blocking device for blocking the belt retractor such that the restraint belt cannot be extracted, wherein the blocking device is connectable to a signal used to issue audible and/or visual output inviting passengers to fasten seat belts, wherein the blocking device is configured to interact with the seat belt retractor such that the seat belt retractor prevents further extraction of the seat belt while the signal is active.

2. The restraint system according to claim 1, wherein the seat belt retractor is an automatic locking retractor configured to automatically stop an additional extraction of the belt after extraction of the belt has been stopped.

3. The restraint system according to claim 2, wherein the blocking device comprises a blocking element which keeps the seat belt retractor in an unlocked state so that the belt can be additionally extracted after extraction of the belt has been stopped as long as the blocking element is powered while the signal is inactive.

4. The restraint system according to claim 1, wherein the seat belt retractor is an emergency locking retractor configured to stop extraction of the belt when an emergency situation is detected by an acceleration sensor sensitive to acceleration of the belt and/or acceleration of an aircraft with the restraint system.

5. The restraint system according to claim 4, wherein the blocking device is configured to block the seat belt retractor when the signal is active so that the belt cannot be further extracted.

6. The restraint system of claim 5, wherein the blocking device comprises a blocking element which keeps the seat belt retractor in an unlocked state so that the belt can be additionally extracted unless an emergency situation is detected by the acceleration sensor as long as the blocking element is powered while the signal is inactive.

7. The restraint system of claim 3, wherein the blocking element is a solenoid.

8. The restraint system of claim 7, wherein the signal is inverted and/or amplified before reaching the blocking element.

9. The restraint system of claim 3, wherein the signal is inverted and/or amplified before reaching the blocking element.

10. The restraint system of claim 1, wherein the restraint belt is a pelvic restraint belt or a three-, four-, five- or more point belt.

11. A method for operating a restraint system for an aircraft seat, the method comprising: providing a restraint system comprising a restraint belt, a belt retractor for winding up the restraint belt and allowing the restraint belt to be extracted, and a blocking device for blocking the belt retractor such that the restraint belt cannot be extracted, wherein the blocking device is connectable to a signal used to issue audible and/or visual output inviting passengers to fasten seat belts, wherein the blocking device is configured to interact with the seat belt retractor such that the seat belt retractor prevents further extraction of the seat belt while the signal is active connecting the blocking device to the signal used to issue audible and/or visual output inviting passengers to fasten seat belts; and controlling the blocking device to interact with the seat belt retractor such that the seat belt retractor prevents further extraction of the seat belt while the signal is active.

12. The method of claim 11, wherein the seat belt retractor is an automatic locking retractor configured to automatically stop an additional extraction of the belt after extraction of the belt has been stopped, wherein the blocking device comprises a blocking element which, while the signal is inactive, is powered so as to keep the seat belt retractor in an unlocked state so that the belt can be additionally extracted after extraction of the belt has been stopped.

13. The method of claim 11, wherein the seat belt retractor is an emergency locking retractor configured to stop extraction of the belt when an emergency situation is detected by an acceleration sensor sensitive to acceleration of the belt and/or acceleration of an aircraft with the restraint system, wherein the blocking device blocks the seat belt retractor when the signal is active so that the belt cannot be further extracted.

14. The restraint system of claim 4, wherein the blocking element comprises a solenoid.

15. The restraint system of claim 5, wherein the blocking element comprises a solenoid.

16. The restraint system of claim 6, wherein the blocking element comprises a solenoid.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0025] The present invention will become more fully understood from the detailed description given herein below and the accompanying drawing which is given by way of illustration only, and thus, are not limitative of the present invention, and wherein:

[0026] FIG. 1 is a schematic view of a restraint system for an aircraft seat.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

[0027] FIG. 1 is a schematic view of a passenger seat 10, in particular for an aircraft. A restraint system 11 is provided, comprising a blocking device 1, a seat belt retractor 2 and a restraint belt 3.

[0028] In a first embodiment, the seat belt retractor 2 is an automatic locking retractor (ALR) configured to automatically stop an additional unwinding of the belt 3 after a passenger has buckled up, i.e. the belt 3 has to be pulled out of the seat belt retractor 2 by the passenger. When the passenger stops pulling out the belt 3 and/or closes the belt buckle, the seat belt retractor 2 is blocked so that the belt 3 cannot be extracted further. Further extraction of the belt 3 can only be achieved by optionally releasing the belt buckle, ceasing to pull on the belt 3 and letting the seat belt retractor 2 pull the belt 3 back in and then pulling the belt 3 out again as far as desired.

[0029] The blocking device 1 comprises a blocking element 4, e.g. a solenoid, which keeps the seat belt retractor 2 in an unlocked state so that the belt 3 can be extracted further as long as the blocking element 4 is powered, i.e. fed a current. The blocking element 4 is electrically connected to a signal S used to issue audible and/or visual output 6 inviting the passengers to fasten seat belts 3, i.e. during take-off and during landing, such that the blocking element 4 is powered, i.e. fed a current, as long as the signal S is inactive. As soon as the signal S is active, the blocking element 4 is no longer powered and the automatic locking mechanism of the ALR seat belt retractor 2 is back in its conventional operational mode, i.e. it automatically stops an additional unwinding of the belt 3 after the passenger has fastened the seat belt 3. For this purpose, the signal S may be inverted and/or amplified before reaching the blocking element 4. Consequently, a power breakdown in the cabin of the aircraft also causes the automatic locking mechanism of the ALR seat belt retractor 2 to arrive back in its conventional operational mode.

[0030] In a second embodiment, the seat belt retractor 2 is an inertia locking retractor or emergency locking retractor (ELR), i.e. the extraction of the belt 3 is stopped when an emergency situation is detected by an acceleration sensor sensitive to acceleration of the belt 3 and/or the aircraft.

[0031] The blocking device 1 electrically connects the seat belt retractor 2 to a signal S used to issue audible and/or visual output 6 inviting the passengers to fasten seat belts 3, i.e. during take-off and during landing so that the seat belt retractor 2 is blocked when the signal S is active and that the seat belt retractor 2 is unblocked and in its conventional operational mode when the signal S is inactive.

[0032] For example, the blocking device 1 comprises a blocking element 4, e.g. a solenoid, which keeps the seat belt retractor 2 in an unlocked state so that the ELR seat belt retractor 2 is in its conventional operational mode, i.e. the extraction of the belt 3 is stopped when an emergency situation is detected by an acceleration sensor sensitive to acceleration of the belt 3 and/or the aircraft, and the belt 3 can be extracted further as long as the blocking element 4 is not powered while the signal S is inactive. As soon as the signal S is active, the blocking element 4 becomes powered and blocks the seat belt retractor 2 so that the belt 3 cannot be further extracted. For this purpose, the signal S may be amplified before reaching the blocking element 4. Consequently, a power breakdown in the cabin of the aircraft causes the automatic locking mechanism of the ELR seat belt retractor 2 to arrive back in its conventional operational mode. In an exemplary embodiment, the signal S may be inverted and/or amplified before reaching the blocking element 4 and the blocking element 4 may be configured to block the seat belt retractor 2 when not powered during a power breakdown or while the signal S is active and to unblock the seat belt retractor 2 when powered while the signal S is inactive.

LIST OF REFERENCES

[0033] 1 blocking device

[0034] 2 seat belt retractor

[0035] 3 belt

[0036] 4 blocking element

[0037] 6 output

[0038] 10 passenger seat

[0039] 11 restraint system

[0040] S signal