초록 ▼

The invention relates to a force supporting device (10) for providing a load-dependent supporting force, in particular for a lowerable overhead locker (12) in an aircraft. The device (10) comprises a bracket (20), whose one end is attached to a supporting structure so as to be pivotal about an axis

The invention relates to a force supporting device (10) for providing a load-dependent supporting force, in particular for a lowerable overhead locker (12) in an aircraft. The device (10) comprises a bracket (20), whose one end is attached to a supporting structure so as to be pivotal about an axis (P) and whose other end is configured for connection to an object to which the supporting force should be applied. There is also a gas-filled spring (22), whose one end is pivotally articulated to the bracket (20) and whose other is pivotally articulated to one end of an oscillating lever (24), whose other end is pivotally attached to a bearing plate (18) and which can pivot relative to the bearing plate (18) between a first end position and a second end position. By means of an arresting device the oscillating lever (24) can be arrested at a plurality of positions in the region of its first end position to the second end position. A displacing device (46) serves to pivot the oscillating lever (24) between its first end position and its second end position as a function of a load determining device which interacts with the displacing device (46).

대표청구항 ▼

The invention claimed is: 1. Force supporting device (10; 110) for providing a load-dependent supporting force, for a lowerable overhead locker (12; 112) in an aircraft, comprising a bracket (20; 120), having a first end attached to a supporting structure so as to be pivotal about an axis (P) and a

The invention claimed is: 1. Force supporting device (10; 110) for providing a load-dependent supporting force, for a lowerable overhead locker (12; 112) in an aircraft, comprising a bracket (20; 120), having a first end attached to a supporting structure so as to be pivotal about an axis (P) and a second end configured for connection to an object to which the supporting force should be applied, a gas-filled spring (22; 122), having a first end pivotally articulated to the bracket (20; 120) and a second end pivotally articulated to a first end of an oscillating lever (24; 124), the oscillating lever having a second end pivotally attached to at least one bearing plate (18a, 18b; 118a, 118b) and which can pivot relative to the bearing plate (18a, 18b; 118a, 118b) between a first end position and a second end position, an arresting device for arresting the oscillating lever (24; 124) at a plurality of positions in the region of its first end position to the second end position, and a displacing device (46; 146) for pivoting the oscillating lever (24; 124) between its first end position and its second end position as a function of a load determined by a load determining device (50; 150) which interacts with the displacing device (46; 146). 2. Force supporting device according to claim 1, characterised in that the bracket (20; 120) can be pivoted about the axis (P) between a first position, which corresponds to a closed position of the object, to which the supporting force should be applied, and a second position, which corresponds to an open position of the object, to which the supporting force should be applied, and in that the arresting device releases the oscillating lever (24; 124) only in the second position of the bracket (20; 120) to allow the displacing device (46; 146) to pivot the oscillating lever (24; 124). 3. Force supporting device according to claim 2, characterised in that the second position of the bracket (20; 120) a swivelling axis (F) of the first end of the gas-filled spring (22; 122) attached to the bracket (20; 120) aligns with a swivelling axis (S1) of the second end of the oscillating lever (24; 124) pivotally attached to the bearing plate (18a, 18b; 118a, 118b). 4. Force supporting device according to claim 1, characterised in that the arresting device comprises a latching claw (32; 132), attached to the free first end of the oscillating lever (24; 124), which interacts with a segment of a circle-shaped toothing (30; 130). 5. Force supporting device according to claim 4, characterised in that the latching claw (32; 132) is rotatably attached to the first end of the oscillating lever (24; 124) and is resiliently pre-tensioned in the direction of an engagement with the segment of a circle-shaped toothing (30; 130). 6. Force supporting device according to claim 5, characterised in that the latching claw (32; 132) is connected to a release lever (38; 138) which is actuated in the second position of the bracket (20; 120) in such a way that the latching claw (32; 132) comes clear from its engagement with the toothing (30; 130). 7. Force supporting device according to claim 6, characterised in that the release lever (38;138) is pivotally attached to the fixed second end of the oscillating lever (24; 124), and in that its pivotal movement is transmitted to the latching claw (32; 132) by a cable or a rod assembly (36; 136). 8. Force supporting device according to claim 6, characterised in that the bracket (20) comprises at least one actuating and centering pin (40) which actuates the release lever (38) in the second position of the bracket (20), in that the segment of a circle-shaped toothing (30) is connected to the bearing plate (18a, 18b), and in that the bearing plate (18a, 18b) is pivotally attached to the supporting structure for adjustment of this actuating position. 9. Force supporting device according to claim 6, characterised in that the gas-filled spring (122) has a cap (123) which actuates the release lever (138) in the second position of the bracket (120), in that the segment of a circle-shaped toothing (130) is connected to the bearing plate (118a, 118b), and in that the bearing plate (118a, 118b) is pivotally attached to the supporting structure for adjustment of this actuating position. 10. Force supporting device according to claim 8, characterised in that the bearing plate (18a, 18b; 118a, 118b) is pivotal about the axis (P). 11. Force supporting device according to claim 1, characterised in that a pre-tensioning force acts on the oscillating lever (24; 124) which acts in the opposite direction to a force exerted on the oscillating lever (24; 124) by the displacing device (46; 146) in the event of an increase in load and which presses the oscillating lever (24; 124) into its first end position in the load-free state. 12. Force supporting device according to claim 11, characterised in that the pre-tensioning force acting on the oscillating lever (24) and damping of the oscillating lever movement are generated or brought about by a damper gas spring unit (48). 13. Force supporting device according to claim 11, characterised in that the pre-tensioning force acting on the oscillating lever (124) is generated by at least one tension spring (168) having a first end fixed to the bearing plate (118a,118b) and a second end fixed to the oscillating lever (124). 14. Force supporting device according to claim 1, characterised in that the displacement movement of the oscillating lever (24) is damped. 15. Force supporting device according to claim 1, characterised in that the load determining device (50; 150) comprises a pivotal weighing plate (54; 154) which is intended to absorb a load and which transmits its pivotal movement, executed as a function of the magnitude of the load, to the oscillating lever (24; 124) by means of a transmitting device. 16. Force supporting device according to claim 15, characterised in that the transmitting device is a Bowden wire (60) or a rod assembly (160). 17. Force supporting device according to claim 1, characterised in that the object to which the supporting force should be applied is a lowerable overhead locker (12; 112) in an aircraft. 18. Force supporting device according to claim 17, characterised in that the load determining device (50; 150) comprises a pivotal weighing plate (54; 154) which is intended to absorb a load and which transmits its pivotal movement, executed as a function of the magnitude of the load, to the oscillating lever (24; 124) by means of a transmitting device, and the weighing plate (54; 154) is arranged in the base region of the overhead locker (12; 112).