Abstract: An insulin delivery rate converter includes a comparator and an insulin delivery supervisor. The comparator is configured to receive insulin data and glucose data and to determine a difference delta between (i) estimations of metabolic data and behavior data derived from the insulin data and blood glucose measurements; and (ii) estimations of metabolic data and behavior data derived from the insulin data without use of the blood glucose measurements. The insulin delivery supervisor is configured to modulate an insulin delivery rate based at least in part on the difference delta determined by the comparator.

Abstract: A propulsion device for a rotating blade aerodyne with vertical take-off and landing, comprising a hollow chassis and contra-rotating coaxial rotors with fixed-pitch blades. The means for driving the rotation of each rotor comprise motor means and, for each rotor, a rotating part capable of turning about a yaw axis, located in the central opening of the respective rotor and connected to the latter via a ball joint with finger, the centre of which is the intersection of the prospective rotor disc and the yaw axis and for which the prohibited rotation is that about the axis of rotation of the rotor. Means for controlling the inclination of the rotors about the roll and pitch axes. Aerodyne equipped with the propulsion device.

Abstract: The invention relates to an expandable tubular element for a fluid-inflatable cylinder, comprising a peripheral wall that is fluid-tight and formed by a plurality of panels connected in pairs by substantially rectilinear links each representing a pivot axis, the panels being more rigid than the links, so that two panels adjacent to a link can rotate about the pivot axis represented by this link, each end of a link being connected to at least two ends of other links so as to define a node, each node having a thickness greater than the minimum thickness of the adjacent links. The invention also relates to a method for producing such an expandable tubular element, as well as a fluid-inflatable cylinder comprising such an expandable tubular element.

Abstract: A propulsion device for a rotating blade aerodyne with vertical take-off and landing, comprising a hollow chassis and contra-rotating coaxial rotors with fixed-pitch blades. The means for driving the rotation of each rotor comprise motor means and, for each rotor, a rotating part capable of turning about a yaw axis, located in the central opening of the respective rotor and connected to the latter via a ball joint with finger, the centre of which is the intersection of the prospective rotor disc and the yaw axis and for which the prohibited rotation is that about the axis of rotation of the rotor. Means for controlling the inclination of the rotors about the roll and pitch axes. Aerodyne equipped with the propulsion device.

Abstract: A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system. According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.

Abstract: A protection device for a power cable that includes a central conductor surrounded by insulation based on paper impregnated with material based on impregnation oil may include a sheath around the insulation, a first portion of the cable stripped of the sheath, an adjacent portion of the cable stripped of both the insulation and sheath, the adjacent portion penetrating the connector; an outer protection extending over at least the first and adjacent portions, and extending over the connector; and/or a plug of high-permittivity mastic material filling an axial space extending along the adjacent portion. The outer protection may include a barrier layer in contact with the insulation along at least part of the first portion. The barrier layer may include elastomer material that is virtually impermeable to the oil. The plug may axially separate the barrier layer and connector to prevent migration of the oil into the connector.

Abstract: A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system, According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.

Abstract: Protection device for power cables with impregnated-paper-based insulation Protection device for a power cable (3) having an insulation (4) based on oil-impregnated paper and an external protection (15). It comprises a barrier layer (11) placed in contact with the insulator (4) and made of an oil-impermeable elastomer material having a permittivity of between (2) and (100). The elastomer material is practically impermeable to water vapour and has a Mooney viscosity of between (12) and (90) at 100° C.

Abstract: The DVD standard, with which a very good quality is required all along the recording step, allows for variable bit rate transmission of data, according to which more bits are spent when the pictures are more complex. As the encoded sequence must fit into a fixed bit budget, the invention relates to an encoding method in which, thanks a first analysis step, corrective modifications of the quantization step of the encoding process are carried out at regular intervals during a second control step. These changes are made regarding the state of a reserve of bits, periodically computed and updated, but preferably only when said reserve reaches critical values, and in order to maintain said reserve at a value as close to 0 as possible.

Abstract: A hydraulic antivibration device comprises an inner strength member and an outer strength member together with an elastomer body disposed between the inner and outer strength members. The elastomer body includes at least two sets of two hydraulic chambers the chambers in any one set intercommunicating via a duct in which a fluid flows. The device includes a window strength member disposed inside the elastomer body and including at least one plate element close to the outer strength member. The ducts interconnect two chambers of a given set via at least a portion situated between a plate element of the window strength member and the outer strength member, and include walls formed by the elastomer body.

Abstract: The invention relates to the processing of video signals prior to encoding or other compression operations, and, more particularly, to a method for encoding video signals corresponding to a sequence of frames each of which consists of two fields F1 and F2. The proposed method comprises the steps of receiving successive frames of an input video signal and delaying them with at least a “two fields” duration delay, and detecting any dominance change and adjusting said delay. When a change from an F1 dominance to an F2 dominance is detected, the first field of the first F2 dominant frame is suppressed, and said delay is decreased by a quantity equal to “one field” duration; when a change from an F2 dominance to an F1 dominance is detected, the last field of the last F2 dominant frame is repeated, and the delay is further increased by a quantity equal to “one field” duration.

Abstract: A brake booster having a movable partition (6) through which an output force is carried through a first reaction device (24,25) to a brake system in response to an input force applied to a brake rod (9). A second reaction device (29-34) is located between the brake rod (9) and the first reaction device (24,25) and includes a first spring (34) that is compressed by a predetermined reaction force and the input force such that any further input force is carried through a second spring (32) into the movable partition (6) to provide and additional force in the development of an output farce corresponding to a desired a brake application.

Abstract: For a lateral face of the lattice girder, defined by an upper chord and a lower chord, the triangulation comprises compression bars substantially perpendicular to the chords, oblique tension bars of smaller length connecting the top of a compression bar to the lower chord, and other oblique tension bars of greater length, also connecting the top of a compression bar to the lower chord, at a point located further ahead toward the base of the next compression bar. This triangulation is used, in particular, for the jib and counterjib elements of tower cranes.

Abstract: Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system. According to the invention, provision is made for the pivotings of said control (2) to be damped by controllable damping means (15, 16) controlled by means (7) detecting oscillations corresponding to pilot induced oscillations.

Abstract: Hydraulic antivibration pivot comprising coaxial internal and external reinforcements connected by an elastomer body that defines two hydraulic chambers communicating with each other through a throttled passage. An intermediate reinforcement embedded in the elastomer body comprises two rigid annuluses about which the external reinforcement is tightened, the said annuluses having collars that project from this reinforcement. The external reinforcement is immobilized between the two collars, which means that axial loads are absorbed without the risk of the pivot becoming detached.

Abstract: In order to provide additional pneumatic boosting which comes into play only for heavy braking, provision is made, in a pneumatic brake-booster, for some boosting force (28, 33) which is in addition to a boost force (25) normally applied by a reaction disk (24) to be absorbed. In a preferred example, force is absorbed by means of a slide (29) containing an envelope (31) and a plunger (30). The plunger is rigidly fixed to the first reaction device. The envelope rests against a piston (23) of the pneumatic booster. The plunger is expelled from the envelope by a spring (34), the excursion of which is countered by a peg (35) as long as the force applied by a driver is below an intermediate force. Beyond that, the reaction of a hydraulic braking circuit downstream compresses the spring and causes the additional pneumatic boosting to come into effect.

Abstract: The present invention relates to a stable aqueous solution (A) comprising an azo dye, a borate buffer and one or more masking agents, wherein the azo dye changes its coloration or coloration intensity in the presence of chlorine dioxide. The present invention further relates to a process for manufacturing the aqueous azo-dye solution (A), and to its use for the determination of residual chlorine dioxide in water.

Abstract: The bit rate of a data stream having the following characteristics is modified. The data stream includes control words, each of which defines when a data portion of the data stream has to be read from an input buffer at a receiving end. An MPEG video stream has such characteristics. It is calculated, for at least one future instant in time (Tfut), within which bounds (Rmax, Rmin) the bit rate (R) of the data stream can be modified at that future instant of time, so as to cause neither underflow nor overflow of the input buffer. The bit rate is modified at a future instant in time within the bounds (Rmax, Rmin) which have been calculated for the future instant in time. This allows a fast modification of the bit rate which generally contributes to the quality of the data comprised in the data stream.

Abstract: For a lateral face of the lattice girder, defined by an upper chord and a lower chord, the triangulation comprises compression bars substantially perpendicular to the chords, oblique tension bars of smaller length connecting the top of a compression bar to the lower chord, and other oblique tension bars of greater length, also connecting the top of a compression bar to the lower chord, at a point located further ahead toward the base of the next compression bar. This triangulation is used, in particular, for the jib and counterjib elements of tower cranes.

Abstract: Control system for a control surface (100) of an aircraft comprising at least one actuator (102, 104) of the control surface, connected to a hydraulic circuit and equipped with at least two power jacks (110) capable of operating in at least one activated mode and one deactivated mode. According to the invention, the system also comprises a control unit (114) capable of making a number of jacks operate in activated mode depending on the aircraft flight conditions. Application to aircraft.