Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
  • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
  • B60N2/62—Thigh-rests
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
  • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
  • B60N2/90—Details or parts not otherwise provided for
  • B60N2/995—Lower-leg-rests, e.g. calf-rests

Definitions

• the present invention relates to a vehicle seat, of the type comprising:
• a second electric actuator adapted for moving the footrest between its extended position and its retracted position
• Such a vehicle seat is used in particular in passenger transport aircraft.
• a motorized seat comprises a legrest and a footrest both controlled by clean electric actuators which can be controlled independently of one another from control means made available to the 'User, there is a risk that, in certain particular configurations of the seat, the user seeks to move one or the other of the seat elements towards a position made impossible by the configuration of the environment of the seat.
• the object of the invention is to provide a solution to the problem mentioned above, by providing a vehicle seat offering passengers a very wide range of travel of the legrest and the footrest, while preventing the seat from being damaged if the footrest contacts the ground.
• the subject of the invention is a vehicle seat, of the aforementioned type, characterized in that it includes, for at least one of the first and second actuators, monitoring means during its use. at least one variable characteristic of the force produced by the actuator and means for estimating at least one predetermined evaluation criterion relating to the or each characteristic variable, t in that the central control unit is adapted for automatically controlling, according to a predefined command order, the operation of at least one of the first and second actuators, independently of the command commands entered by the user, when at least one of the criteria for predetermined evaluation is checked.
• the vehicle seat comprises one or more of the following characteristics: - said predefined control order is the stopping of the or each actuator during control by the user and for which the criterion d the associated predetermined evaluation is satisfied;
• Said predefined command order is the drive in the opposite direction of the actuator during command by the user and for which the associated predetermined evaluation criterion is satisfied;
• At least one variable characteristic of the force produced by an actuator is a variable characteristic of the electric current consumed by this actuator;
• Said characteristic variable is the intensity consumed by the actuator, and said predetermined evaluation criterion is the comparison of the intensity consumed with a predetermined threshold;
• Said characteristic variable is the derivative with respect to time of the intensity consumed by the actuator, and said predetermined evaluation criterion is the comparison of the derivative with respect to time of the intensity consumed with a predetermined threshold.
• FIG. 1 is a schematic view of a vehicle seat according to the invention.
• FIGS. 2 and 3 are two different variants of the algorithm implemented in the central seat control unit of Figure 1.
• the seat 10 shown in Figure 1 is a passenger seat of an aircraft. This seat is fixed to the ground 12 of the aircraft.
• the seat 10 comprises a base 14 secured to the ground 12 on which rests a substantially horizontal seat 16. At one end of the seat is articulated a backrest 18. At the other end of the seat 16 is articulated a leg rest 20 movable between a folded position substantially vertical below the seat 16 and an extended position substantially horizontal in the extension of the seat 16.
• the seat 10 further includes a footrest 22 mounted movably sliding relative to the leg rest 20 in the extension thereof.
• the footrest 22 can be moved between a retracted position inside the legrest 20 and an extended position in which it extends the latter and is practically completely extended.
• a first electric actuator 24 is mounted between the seat 16 and the leg rest 20 in order to ensure movement of the latter between its folded position and its extended position.
• a second actuator 26 is provided between the legrest 20 and the footrest 22 in order to ensure the movement of the footrest between its retracted position and its extended position.
• Each of the actuators 24 and 26 is supplied with electric current from a central control unit 28.
• This control unit 28 is connected separately to each of the actuators 24 and 26 in order to ensure their independent control.
• the seat comprises on an armrest 30 to which is fixed a control keyboard 32 allowing the independent control of the actuators 24 and 26 in order to cause an independent movement of the legrest and the footrest.
• the control keyboard 32 is connected to the central control unit 28.
• the unit 28 includes a source 34 for supplying the actuators.
• the latter is formed pr example of a transformer connected to the general power supply network of the aircraft by suitable connection means.
• a supply interface 36, 38 ensuring the supply of the actuators, respectively 24 and 26, from the supply source 34.
• the source 34 is formed for example by a transformer.
• the power supply interfaces 36 and 38 are controlled by a central information processing unit 40.
• This unit 40 is connected to the control keyboard 32, in order to collect the control commands from the user.
• the unit 40 implements a control program, the main algorithms of which will be described in the following description.
• the monitoring means 42 and 44 are connected to the central information processing unit 40.
• the central information processing unit 40 implements a program known per se suitable for controlling the supply interfaces 36 and 38 so that they supply the actuators 24 and 26 in one direction or the other by reversing the current direction, as a function of the information received from the keyboard 32.
• the central information processing unit 40 continuously implements, for example, the algorithm illustrated in FIG. 2.
• the monitoring means 42, 44 are adapted to determine the instantaneous intensity ii, i 2 consumed respectively by the actuator 24 and 26 during their operating phase.
• two threshold values noted and l 2 are stored in the control means 28 in order to compare the instantaneous intensity values and l 2 measured by the monitoring means 42 and 44.
• the values li and l 2 correspond to minimum values of current consumed by the actuators 24 and 26, when the free end of the footrest comes into contact with the ground 12 of the aircraft. These threshold values h and l 2 are determined from measurements made on a typical seat. As illustrated in FIG. 1, in step 98, the program implemented in the central information processing unit-40 determines the values measured for and i 2 by the monitoring means 42, 44. At the step 100, it is determined whether the value i 2 is greater than the first predetermined threshold li. If this is the case, that is to say that the legrest is initially driven by the actuator 24 towards its folded position, and that it is now stopped and immobilized by the contact of the free end of the footrest against the ground, step 102 is implemented.
• step 104 the central information processing unit 40 controls the power supply interface 36 in order to control the actuator 24 in the opposite direction, for a brief period of time corresponding to a displacement of a few degrees from the legrest to its extended position, allowing the free end of the footrest to be moved off the floor 12.
• step 104 is implemented.
• the instantaneous intensity measured i 2 is compared to the second predetermined threshold l 2 . If the intensity i 2 is greater than the threshold value l 2 , step 106 is implemented. This step is thus carried out if the footrest was then moved to its extended position, its free end has just struck the ground, leading to the immobilization of the actuator 26 and thus to the increase of the current consumed by the latter. .
• step 106 the information processing unit 40 controls the power supply interface 38 in order to cause the reversal of the direction of current in the actuator 26 and thus the movement of the footrest towards its retracted position.
• This command is carried out for a short period of time, which leads to the rearward movement of the footrest 22 over a short stroke, thus making it possible to separate the free end of the footrest from the surface of the ground 12.
• step 98 is again implemented.
• step 98 is each time implemented.
• FIG. 3 is illustrated a variant of the algorithm of FIG. 2.
• the monitoring means 42 and 44 are each adapted to determine not the intensity of the current consumed but the derivative with respect to time of the intensity of the current consumed by the actuators 24 and 26. These latter values are noted d / dt and di 2 / dt.
• the tests carried out by the central information processing unit 40 ensure the comparison of the time derivatives of the intensities measured at two predetermined thresholds denoted Di and D 2 . These predetermined thresholds correspond to the variations observed in the instantaneous intensity consumed by the actuators 24 and 26 when the free end of the footrest comes into contact with the ground.
• the algorithm illustrated in FIG. 3 includes steps 200 and 204 replacing steps 100 and 104, during which the instantaneous values of the derivative of the intensity consumed by the actuators 24 and 26 are compared with the predetermined thresholds Di and D 2 .
• steps 200 and 204 replacing steps 100 and 104, during which the instantaneous values of the derivative of the intensity consumed by the actuators 24 and 26 are compared with the predetermined thresholds Di and D 2 .
• step 102 or 106 is implemented, making it possible to separate the free end of the footrest from the ground .
• the free end of the footrest can be brought as close as possible to the ground until it comes into contact with it.
• the actuator during operation is controlled in the opposite direction, in order to avoid slightly the free end of the footrest relative to the floor.
• the actuator when the characteristic variable of the current consumed by one of the actuators exceeds a predetermined threshold value, the actuator is not controlled in the opposite direction but the latter is only stopped automatically, thus preventing the user of the wheelchair to continue controlling the actuator in the same direction. Only the control of the actuator in the opposite direction is authorized for the user.
• variable characteristic of the force produced by the actuators during their use can be used.
• the variables characteristic of the current consumed described above, which are representative of the force applied by the actuator considered can be replaced by the torque applied by an actuator or by the power delivered by the latter.
• the monitoring means described can be replaced by torque sensors, the comparisons carried out then being implemented on the measured couples.
• the seat can be used in any other type of vehicle, in particular a rail vehicle, a road vehicle, or a boat.

Landscapes

• Engineering & Computer Science (AREA)
• Aviation & Aerospace Engineering (AREA)
• Transportation (AREA)
• Mechanical Engineering (AREA)
• Passenger Equipment (AREA)
• Seats For Vehicles (AREA)

Applications Claiming Priority (3)

Publications (1)

Family

ID=9550557

Family Applications (1)

Country Status (4)

Cited By (1)

Families Citing this family (6)

Family Cites Families (4)

• 1999
  • 1999-10-04 FR FR9912366A patent/FR2799164B1/fr not_active Expired - Fee Related
• 2000
  • 2000-10-03 AU AU76719/00A patent/AU7671900A/en not_active Abandoned
  • 2000-10-03 WO PCT/FR2000/002745 patent/WO2001025053A1/fr not_active Application Discontinuation
  • 2000-10-03 EP EP00966271A patent/EP1135277A1/de not_active Withdrawn

Non-Patent Citations (1)

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