387 results about "High lift" patented technology

A wing for an aircraft, comprising a main wing and a high lift assembly which includes a body, and an assembly connecting the body to the main wing, so the body is movable between a retracted position and an extended position. The assembly comprises a track extending along a longitudinal axis between first and second ends, with an intermediate portion therebetween. A roller bearing ensures that the track moves along the longitudinal axis. The roller bearing comprises bearing units, each mounted to the main wing and having a bearing surface for engaging the elongate track. The units include a first and second end units and an intermediate unit wherein, relative to the longitudinal axis, the intermediate unit is positioned between the first end unit and the second end unit. The elongate track comprises a recessed portion which, in the retracted position, aligns the intermediate unit.

The invention provides a multidisciplinary coupling optimization design method for integrated joined wing layout. The method comprises the following steps: firstly, determining a design target, a design working condition and a design variable of multi-disciplinary optimization of the joined wing layout; dividing design variables into global design variables and local design variables; taking a high lift-drag ratio, low structural quality and low electromagnetic shielding rate as a system-level design target, taking a global design variable as a design variable, fixing a local design variable, and carrying out system-level optimization; then, high lift-drag ratio, low structural quality and low electromagnetic shielding rate are taken as subsystem-level design targets, local design variables of corresponding subjects are taken as design variables, global design variables and local design variables of other subjects are fixed, and subsystem-level optimization of the subjects is carried out; and finally, judging whether a convergence condition is met or not, and if not, continuing system-level optimization and subsystem-level optimization until convergence. The pneumatic / structural / electromagnetic multi-disciplinary coupling optimization design of the integrated joined wing layout is realized.

The invention provides a modularized flow guide type multi-stage pump, and belongs to the technical field of water pumps. The modularized flow guide type multi-stage pump comprises a pump body assembly and a driving motor, the pump body assembly is formed by sequentially connecting a pump head pattern plate, a multi-stage pump shell, a multi-stage flow guide module set and a water retaining sealing cover, the pump head pattern plate is adjustably connected with a connecting end cover of the driving motor through a long screw rod, and the stage number of the pump can be adjusted by increasing or decreasing the number of the flow guide shells. Different lift requirements are met; the multi-stage flow guide module group is mainly composed of a water inlet flow guide shell, a transmission flow guide shell and a water outlet flow guide shell, a closed impeller is arranged in each flow guide shell to form an independent flow guide module, fluid is guided by spiral flow guide blades between the flow guide shells to orderly flow and smoothly transmit, and turbulent flow eddy current loss is reduced; and the water retaining sealing cover realizes double leakage prevention through a stepped sealing flange and mechanical sealing. The high-lift and high-flow pump has the advantages of being easy to disassemble, assemble and maintain, modularized and flexible to adjust, low in energy loss, high in lift, high in flow and high in sealing performance.

An aircraft wing includes a main wing and a high lift assembly having a high lift body, and a connection assembly movably connecting the high lift body to the main wing to be movable between a retracted and an extended position, and having an elongate track extending along a longitudinal axis between a first end and a second end. The first end of the track is mounted to the high lift body. The track is mounted to the main wing via a roller bearing to be movable along the longitudinal axis. The roller bearing includes a first and a second roller mounted to at least one of the main wing and the track via first and second eccentric connector assembly, respectively. The first and second eccentric connector assemblies are configured to be engaged simultaneously by a single alignment member for synchronous rigging of the first and second rollers.

An aircraft wing includes a main wing and a high lift assembly which includes a high lift body and a connection assembly movably connecting the high lift body to the main wing, such that the high lift body is movable between retracted and extended positions. The connection assembly includes primary and secondary connectors mountable to and engageable with the main wing via primary and secondary mount profiles, respectively. The primary connector is rotatable relative to the primary mount profile and at least one of the connection assembly and the main wing to configure the primary connector and mount profile between a decoupled configuration in which the primary connector may be moved into so as to be engaged with, and removed from so as to be disengaged from, the primary mount profile, and a locked configuration wherein movement between the primary mount profile and the secondary mount profile is restricted.

The invention relates to a vertical water-cooling self-priming pump, and belongs to the technical field of fluid conveying. Comprising an upper liquid storage cylinder and a lower liquid storage cylinder which are fixedly connected, a water inlet pipe is arranged on the rear side of the lower liquid storage cylinder, a discharge pipe is arranged on the front side of the lower liquid storage cylinder, a water outlet pipe is arranged on the front side of the upper liquid storage cylinder, and an exhaust valve is arranged at the top of the upper liquid storage cylinder; a water-cooled motor is fixedly arranged in the upper liquid storage cylinder, a multi-stage water pump is arranged in the lower liquid storage cylinder and connected with the water-cooled motor through a coupling assembly, and a supporting assembly is arranged between the water-cooled motor and the inner wall of the upper liquid storage cylinder; an overflow protection assembly is arranged at one end, away from the lower liquid storage cylinder, of the water inlet pipe; the problems that an existing self-priming pump is unstable in installation of a special-shaped motor, high in requirement for the environment of a cooling system, low in lift, unstable in long-time operation and liquid overflows when the self-priming pump is closed are solved.

Towed aerodynamic platforms approach the behavior of flat plate airfoils to achieve high lift-to-drag (L:D) performance when operated at low pitch angles. A lead aircraft may tow multiple platforms to form train units. Low form drag and high L:D enable solar aircraft that are more robust and faster than approaches extending wingspan rather than extending the length of the aerial train. Applications extend beyond solar aircraft and include vehicles towed along an overhead monorail system and aerial drones.

An aircraft wing includes a main wing and a high lift assembly having a high lift body and a connection assembly movably connecting the high lift body to the main wing, such that the high lift body is movable between retracted and extended positions. The connection assembly includes an elongate track extending along a longitudinal axis between first and second ends and has an intermediate portion. The first end is mounted to the high lift body, and the second end is mounted to the main wing by a roller bearing such that the track is movable along the longitudinal axis. The roller bearing includes a roller unit mounted to the main wing and having a circumferential roller surface engaging an engagement surface of the track and an internal elastic bearing allowing the roller surface, in a cross section parallel to the roller rotation axis, to adapt its orientation or form.

The invention relates to the technical field of centrifugal pump control, and discloses an intelligent control multi-working-condition ultrahigh-lift single-stage centrifugal pump control method which comprises the steps that attention-guided dimension reduction fusion and multi-scale feature extraction are conducted on multi-source working condition data, and multi-scale operation features are obtained; time evolution and clustering processing are conducted on the multi-scale operation characteristics through a time clustering algorithm based on density, and the current working condition of the ultrahigh-lift single-stage centrifugal pump is obtained; and taking the current working condition, the performance parameters and the performance score of the ultrahigh-lift single-stage centrifugal pump as state vectors, and selecting an optimal control vector from a control space by adopting a reinforcement learning model. By fusing multi-source data and introducing time evolution modeling and reinforcement learning optimization strategies, intelligent sensing and self-adaptive control of the ultra-high-lift single-stage centrifugal pump under multiple working conditions and the whole life cycle are achieved, the problems that response to complex operation states is slow and adjustment lags in traditional rule driving control are solved, and the service life of the ultra-high-lift single-stage centrifugal pump is prolonged. The energy efficiency ratio, the operation stability and the equipment service life are improved.

The invention relates to a water pump scheduling method for estimating lift based on data driving, which comprises the following steps: calling structural information and sensing data, calculating friction loss and structural symmetry, extracting differential pressure data flow gradient, judging load matching degree, activating path nodes, identifying differential pressure data change sections, and mapping a calculation path. According to the method, dynamic correction and compensation of input parameters are achieved by means of conjoint analysis of the structural features of the water inlet and the water outlet and flow pressure difference data, and comprehensive judgment of the working condition matching degree and the periodic change state is combined, so that the flow resistance trend is judged, and the calculation result is corrected. The adaptability to cold load fluctuation and loop temperature difference change is enhanced, the response capability of lift calculation to water body characteristic change is improved by introducing flow resistance trend and viscous state factors, and the calculation stability of the model in different operation sections and the calculation accuracy of the model in complex working conditions are optimized by using a path activation configuration and output switching mechanism.

The application relates to a high-efficiency lift flapping wing, a dragonfly-imitating aircraft and an aircraft flight posture control method. The high-efficiency lift flapping wing comprises a flapping wing body and a plurality of one-way air door blades; a plurality of air vents are arranged on the flapping wing body, each one-way air door blade covers the air vent, and the one-way air door blade is used for allowing airflow to pass through the air vent in one direction. The high-efficiency lift flapping wing, the dragonfly-imitating aircraft and the aircraft flight posture control method have the advantages of high lift efficiency, reduced flapping wing burden, improved aircraft service life and stability.

The invention discloses a waverider profile and low-speed airfoil profile fused wide-speed-range airfoil profile design method, and relates to the field of aircraft airfoil profile design, and the method comprises the following steps: S1, based on a lift force generation mechanism of high-speed stage waverider compression characteristics and low-speed stage streaming characteristics, taking a high-speed airfoil profile waverider profile from an airfoil profile front section, and taking a low-speed airfoil profile rear half part from an airfoil profile rear section; s2, according to the task characteristics of the aircraft, a nonlinear weight method is adopted to calculate the distribution proportion of the waverider profile and the low-speed airfoil profile to obtain a basic airfoil profile; and S3, selecting predetermined areas in front of and behind the maximum thickness position of the basic airfoil to perform grid parameterized deformation so as to complete the wide-speed-range airfoil optimization design. According to the wide-speed-range airfoil profile design method integrating the waverider profile and the low-speed airfoil profile, the high lift-drag ratio of the high-speed waverider airfoil profile and the high lift coefficient of the low-speed airfoil profile are fully combined, and the airfoil profile requirement of wide-speed-range aircraft design is met by reasonably selecting the proportion of the waverider airfoil profile and the proportion of the low-speed airfoil profile.

A skew sensing apparatus for detecting skew in at least one, or a plurality of control surfaces of a vehicle. The apparatus includes a tension cord which is held under tension between a) a first spring associated with a sensor and a sensor target and b) an opposing second spring. During normal operation, the apparatus is configured to maintain said sensor target in a first position relative to said sensor, thereby indicating said normal operation. During an abnormal operation, the apparatus is configured to shunt said tension cord such that said sensor target is translated to a second position, relative to said sensor thereby indicating said abnormal status.

A wing for an aircraft, comprising a main wing and a high lift assembly which includes a body, and an assembly connecting the body to the main wing, so the body is movable between a retracted position and an extended position. The assembly comprises a track extending along a longitudinal axis between first and second ends, with an intermediate portion therebetween. A roller bearing ensures that the track moves along the longitudinal axis. The roller bearing comprises bearing units, each mounted to the main wing and having a bearing surface for engaging the elongate track. The units include a first and second end units and an intermediate unit wherein, relative to the longitudinal axis, the intermediate unit is positioned between the first end unit and the second end unit. The elongate track comprises a recessed portion which, in the retracted position, aligns the intermediate unit.

The invention discloses a high-lift water pump with a self-adaptive flow regulation function, and relates to the technical field of high-lift water pumps, the high-lift water pump comprises a water pump shell, the side wall of the water pump shell is fixedly connected with a water inlet pipeline, the upper end of the water pump shell is fixedly connected with a water outlet pipeline, and the inner wall of the water pump shell is rotatably connected with a rotating shaft; the side wall of the rotating shaft is fixedly connected with a closed impeller; the flow adjusting mechanism comprises a valve rod rotationally connected to the inner wall of the water outlet pipeline, the side wall of the valve rod is fixedly connected with a ball, the side wall of the ball is in sealed sliding connection with the inner wall of the water outlet pipeline, a water outlet is formed in the side wall of the ball, and the side wall of the water outlet pipeline is in sealed sliding connection with a pressure sensing block. The rotating angle of the ball body can be adjusted according to the actual water outlet amount and water pressure, then the size of the water outlet is adjusted, the water outlet amount is automatically adjusted, the water outlet amount is made to be within a proper range, manual intervention adjustment is not needed, and using is more convenient.

Described is a wing (3) for an aircraft (1), comprising a main wing (5) and a high lift assembly. The high lift assembly is also described as comprising a high lift body (7), and a connection assembly (9) movably connecting the high lift body (7) to the main wing (5), such that the high lift body (7) is movable between a retracted position (11) and at least one extended position (13, 15). The connection assembly (9) comprises an elongate track (17) that extends along a track longitudinal axis (19) between a first end (21) and a second end (23) and has an intermediate portion (25) between the first and second ends (21, 23). The first end (21) and / or the intermediate portion (25) of the track (17) is mounted to the high lift body (7) and the elongate track (17) is mounted to the main wing (5) by a roller bearing (27) such that the track is movable along the track longitudinal axis (19). The roller bearing (27) comprises a plurality of bearing units (34a-c), each of the bearing units (34a-c) being mounted to the main wing (5) and having a bearing surface (22) for engaging an engagement surface (35) provided on the elongate track (17). In addition, the plurality of bearing units (34a-c) comprises a first end roller unit (34a), an intermediate roller unit (34b) and a second end bearing unit (34c), and the plurality of bearing units (34a-c) are positioned such that, relative to the track longitudinal axis (19), the intermediate roller unit is positioned between the first end roller unit and the second end bearing unit. The elongate track (17) comprises a recessed portion wherein, in the retracted position, the recessed portion is configured to align along the track longitudinal axis (19) with the intermediate roller unit such that a contact force between the intermediate roller unit and the engagement surface (35) of the elongate track (17) is reduced.

A rotor blade for a wind turbine is provided. The rotor blade includes a high lift root profile with flat-back trailing edge with a suction side and a pressure side, a relative airfoil thickness being between 45% and 75% or between 48% and 70% of a chord length. A trailing edge thickness is between 30% and 75% or between 35% and 60% of the relative airfoil thickness. The chord position of the maximum relative airfoil thickness, which is measured from a leading edge towards the trailing edge, is between 35% and 45% or between 36% and 42% of the chord length. Also provided is a wind turbine equipped with the rotor blade(s).

The invention discloses a water pump capable of improving lift, and relates to the technical field of high-lift water pumps. The high-lift water pump comprises a high-lift water pump body, the high-lift water pump body comprises a base, a bearing is matched with the inner wall of a bearing shell, an infrared temperature measurement sensor is arranged on the outer side wall of the bearing shell, a monitoring head of the infrared temperature measurement sensor is located in the bearing shell and close to the bearing, an energy supply mechanism is arranged in a water inlet pipe, and an oil supply mechanism is arranged on the outer side wall of the bearing shell. By arranging the oil supply mechanism, lubricating oil can be automatically added to the bearing, friction of the bearing is reduced, energy loss of the water pump is reduced, the lift of the water pump is improved, and by arranging the quantitative control mechanism, quantitative control can be achieved when the lubricating oil is automatically added to the bearing; the lubricating effect of the bearing can be further improved, energy loss is further reduced, and the lift of the water pump is further improved.

The utility model belongs to the technical field of water pump application, and particularly discloses a high-flow self-adaptive sewage pump. Comprising a fan blade cover, a motor rear end cover, a machine barrel, a motor front end cover, a pump head, fan blades, a shaft clamp spring, a stator assembly, a first rolling bearing, a rotor assembly, a volute, an impeller, a water retaining ring, a water outlet, a water inlet, a waterproof switch assembly, a switch sealing gasket, a capacitor, a capacitor box lower cover and the like which are assembled in a matched mode. The utility model has the beneficial effects that: before the water pump works, the vortex cavity needs to be filled with water; when the impeller rotates at a high speed, liquid between the blades rotates along with the blades, so that the liquid obtains higher pressure energy, and the lift is improved; the volute and the impeller are respectively made of integrally-formed gray cast iron and have good abrasion resistance, the service life of the volute and the service life of the impeller can be prolonged, and it is guaranteed that the water pump has the long service life under the high load. The working efficiency of the whole machine is improved by using a high-efficiency induction type motor; the hook structure facilitates storage of a power line, and the use convenience of the water pump is improved.

The utility model relates to the technical field of centrifugal pump production, in particular to a pump cover punching tool of a high-lift circulating pump, which mainly comprises an inner clamping component, a water inlet hole punch forming component and a mounting hole punch forming component. The mounting hole punch forming assembly is used for punching a mounting hole in a mounting convex plate of a pump cover blank, the inner clamping assembly is used for providing inner clamping support for the pump cover blank, and bearing pressure is provided in the water inlet hole punch forming and mounting hole punch forming processes, in this way, the cover body deformation condition can be avoided in the punching machining process, and the service life of the pump cover blank is prolonged. And the requirement of punching the lateral water inlet hole and the axial mounting hole at the same time is met.

A natural energy full-hydraulic water lifting device based on the pure water hydraulic transmission technology is characterized in that a retaining dam is arranged at a power water source, a power water reservoir is formed after water storage, a high-pressure water tank is arranged at the position H lower than the horizontal plane of the reservoir, a water taking opening is formed in the retaining dam, and a drainage water pipe is connected with the water taking opening and the high-pressure water tank; the high-pressure water tank is connected to the high-lift water pump hydraulically driven by pure water through a high-pressure water tank water outlet pipe, one end of a water pump water outlet pipe on the high-lift water pump hydraulically driven by pure water is connected with the high-lift water pump, the other end is connected to a destination reservoir, and a water pump water inlet pipe is connected to a water source to be lifted; the device is provided with various detection units and control units, and the automatic control device consists of an execution unit and a PLC (Programmable Logic Controller). The utility model has the characteristics of high energy utilization efficiency, high water lift, simple structure, low manufacturing cost, energy conservation and the like. The water lifting device can be widely applied to water lifting in water-deficient mountainous areas, in particular to water lifting in mountainous areas in which the height difference between the water source location and the water using place is large.

A high-lift long-service-life vertical multi-stage centrifugal pump comprises a water feeding base, a water inlet connector arranged on the left side of the water feeding base and a motor arranged over the water feeding base, a main shell is arranged between the motor and the water feeding base, a rotating shaft is arranged at the lower end of a motor shaft of the motor, and a plurality of impellers evenly distributed in the axial direction are arranged on the rotating shaft. The impeller is covered with an impeller shell matched with the impeller, a water inlet hole communicated with the lowest impeller shell is formed in the upper surface of the water supply base, a water supply gap is formed between the outer wall of the impeller shell and the inner wall of the main shell, a water outlet connector communicated with the water supply gap is arranged on the right side of the water supply base, and a filter base is arranged in a port of the left end of the water inlet connector. According to the high-lift long-service-life vertical multi-stage centrifugal pump, granular impurities in water flow can be effectively filtered out, the granular impurities in the water flow cannot make contact with the impeller, the service life of the impeller is prolonged, and the situation that the filtering holes are blocked can be effectively avoided.

The invention provides a flapping wing design method with low power consumption and thrust increasing characteristics, a flapping wing and a long-endurance flapping wing aircraft. When the ornithopter flies, the driving mechanism drives the flapping wings to perform single-degree-of-freedom flapping motion, the wing surfaces generate optimal passive deformation matched with the flight speed under the action of aerodynamic force, deformation and motion of wings in the flight process of birds in nature are simulated, and the design of bionic wings with high thrust, high lift and low power consumption is realized; the flapping wings have better thrust characteristics, the trimming frequency is reduced, so that power consumption is greatly reduced, the shape of a fuselage shell meets the aerodynamics requirement, the resistance effect caused by the fuselage is reduced, and the fuselage has the advantages of being light in weight, good in impact resistance effect and the like due to the section shape, the material and the structural form of the fuselage. And the requirements of typical flight states such as cruise flight and belly landing are met.

The present application provides a kind of mechanical arm for spray seeding greening, including flexible connecting pipe, one end of the connecting pipe is connected with platform, the other end is connected with spray gun seat, connecting rod A is fixedly connected with the spray gun seat, connecting rod B is rotatably connected with the connecting rod A, the platform is fixedly connected with support, the connecting rod B is rotatably connected with support, further including drive mechanism, the drive mechanism is connected on the support, and the output end of drive mechanism is rotatably connected with connecting rod A, to drive connecting rod A to rotate around the output end of drive mechanism and the rotation point of connecting rod A while doing vertical motion.The present application changes the bending mode of the connecting pipe uniformly when in use by the structure, can reduce the wear and tear of connecting pipe and pressure loss in pipeline, improve lift, avoid blockage, convenient to replace, wide source, strong availability, the present application is light in weight, low in cost, adjustable spray seeding angle is large, and spray seeding efficiency is high.

A heat exchanger for heating, ventilation, air conditioning and refrigeration (HVACamp; a compressor system of an HVACamp (R, R) system, the compressor system comprising one or more compressors configured to circulate a working fluid through the HVACamp; a vapor compression system of an R system, each compressor of the one or more compressors having a pre-rotating vane (PRV) and a variable geometry diffuser (VGD), the PRV and the VGD configured to operate to adjust a capacity of the compressor system. The compressor system further includes a controller having a memory and processing circuitry, where the memory includes instructions stored thereon that, when executed by the processing circuitry, cause the processing circuitry to: determine a head coefficient for each compressor of the one or more compressors, and determine a head coefficient for each compressor of the one or more compressors; determining a compressor lift for each of the one or more compressors based at least in part on the head coefficient, comparing the compressor lift for each of the one or more compressors to a low lift threshold and a high lift threshold, and operating each of the one or more compressors in a first mode or a second mode based on a comparison of the compressor lift to the low lift threshold and the high lift threshold.

The utility model relates to a high-lift stainless steel stamping deep-well pump which comprises a pump cylinder and a plurality of impeller sets, the impeller sets are installed in the pump cylinder in a stacked mode, the water outlet end of the pump cylinder is in threaded connection with a gland, and a water outlet connecting pipe is installed on the gland. When the high-lift stainless steel stamping deep-well pump is used, a plurality of impeller sets are installed on the pump cylinder according to actual needs, and then the impeller sets are locked by the gland, so that the impeller sets are stably arranged in the pump cylinder, displacement is increased or reduced by increasing or reducing the number of the impeller sets, and the high-lift stainless steel stamping deep-well pump can be stably arranged in the pump cylinder under the condition that the diameter is not changed. And the water pumping amount is increased through multiple superposition.

A multidisciplinary approach to the automated optimization design of high-flying paragliders integrates automated and modularized functions, including geometric modeling, mesh modeling, aerodynamic calculation, and airfoil shape optimization. These modules are integrated through the Isight platform to establish a multidisciplinary optimization design framework. This method decouples the issue of improving the aerodynamic performance of three-dimensional paragliders and automatically optimizes the airfoil based on parameters such as the canopy structure and material. Each module automatically reads previous result files and runs in a loop, requiring no human intervention, to automatically output the optimized airfoil with the highest lift-to-drag ratio. This method is highly efficient, utilizes a functional airfoil design, offers high precision, and facilitates automated processing and production. This method holds significant implications for the optimized design of high-flying paragliders.

A natural energy hydraulic pressure water lifting device pressurized based on a pure water hydraulic transmission technology is composed of a gas production unit and a water lifting unit, and the gas production unit comprises a retaining dam, a reservoir, a gas-liquid separation box, a pure water hydraulic driven air compressor and a main high-pressure gas storage tank; the water lifting unit comprises an auxiliary high-pressure air storage tank, a high-lift air pressure water pump and a water source pool. The device is provided with an automatic control device. High-pressure water serves as power, the pure water hydraulic transmission air compressor is used for compressing original primary high-pressure air again, the final pressure of the high-pressure air is not limited by the drainage fall of the power water any more, and the water lifting head is greatly improved. Compared with a hydraulic and pneumatic water lifting device in use, the hydraulic and pneumatic water lifting device has the advantages that the pressure of high-pressure water can be utilized, and the hydraulic and pneumatic water lifting device is high in hydraulic and pneumatic energy conversion efficiency and large in water lifting amount. A power water source is separated from a water supply source, and the water lift can be utilized to the maximum extent. The multi-point water supply and multi-stage water lifting can be realized, and the application range is wider.

The invention belongs to the technical field of water conservancy projects, and discloses an extra-high arch dam bank slope dam section concrete first bin high lift layer construction method which comprises the following steps: step 1, determining dam concrete construction layering, step 2, establishing a template support model, step 3, carrying out stress checking calculation and the like. According to the extra-high arch dam bank slope dam section concrete first bin high lift layer construction method, PKPM structural calculation software is combined with the structural form of a dam, the distance from an upstream excavation face is combined, a model is established for structural stress and stability analysis, high lift layer construction is achieved, the highest lift layer height is large, multi-bin parallel one-time pouring is achieved, the pressure of a standby bin is relieved, and the construction efficiency is improved. The construction efficiency is improved. According to the ultrahigh arch dam bank slope dam section concrete first bin high rising layer construction method, the pouring height and quality of each layer can be effectively controlled, the uniformity and compactness of concrete are ensured, and the construction precision of the whole structure is improved.

A high lift system monitoring arrangement (24) includes: a sensor (32), a monitoring unit (34) connected to the sensor (32), wherein the monitoring unit (34) includes: an acquisition module (46), that acquires an analog sensed information (AI) from the sensor (32), a processing module (48) having a first processing circuitry (48A) and a second processing circuitry (48B), different from the first circuitry, wherein the first processing circuitry (48A) processes the analog sensed information (AI) into a first digital sensor data (DD1), the second processing circuitry (48B) processes the analog sensed information (AI) into a second digital sensor data (DD2).