1712 results about "Front edge" patented technology

The invention provides a turbine blade design method which comprises the following steps: S1, dividing a turbine blade profile into four sections at equal intervals along the radial direction according to the size of a turbine, and calculating section parameters of a middle-section turbine blade profile; s2, connecting the four sections by adopting a third-order Bezier curve, defining a blade front edge angle theta as an included angle between the Bezier curve and a blade front edge radial inlet angle alpha, and generating a three-dimensional blade model by changing the inclination angle theta of each section; s3, performing optimization to obtain an optimized theta parameter; and S4, according to the optimized theta parameter, fitting each section blade profile by using a third-order Bezier curve to generate a turbine stator and rotor three-dimensional model. According to the method, the machine learning method is applied to design of the turbine blade, the three-order Bezier curve, the CFD numerical simulation method and the particle swarm optimization are utilized, the blade parameters are given, the geometric parameters can be quickly and accurately predicted, the calculated amount is reduced, the cost is reduced, the design efficiency is improved, and the quality of the designed blade is guaranteed.

A bipedal robot includes an upper region includes a head and neck assembly having a neck portion and a head portion coupled to the neck portion. Said head portion includes: a frontal shell having a rear edge, a rear shell having a frontal edge, and an illumination assembly. The illumination assembly is configured to illuminate a region that: (i) extends between a rear edge of the frontal shell and an extent of the frontal edge of the rear shell, (ii) is positioned adjacent to the extent of the rear edge of the frontal shell, and (iii) is positioned adjacent to the extent of the frontal edge of the rear shell.

A bipedal robot includes an upper region includes a head and neck assembly having a neck portion and a head portion coupled to the neck portion. Said head portion includes: a frontal shell having a rear edge, a rear shell having a frontal edge, and an illumination assembly. The illumination assembly is configured to illuminate a region that: (i) extends between a rear edge of the frontal shell and an extent of the frontal edge of the rear shell, (ii) is positioned adjacent to the extent of the rear edge of the frontal shell, and (iii) is positioned adjacent to the extent of the frontal edge of the rear shell.

The invention relates to a cooperative control method for smooth pit-passing braking of a vehicle. The cooperative control method comprises the following steps that geometric data of a road surface pit and initial time data of predicted contact between a target wheel and the front edge of the pit are obtained through a preview sensing system; when the geometric data and the initial time data meet a preset triggering condition, triggering a suspension position control mode of the target wheel: acquiring target height data of a suspension, and generating a movement track of an active suspension of the target wheel from the current height data to the target height data; controlling an active suspension actuator to track the motion trail; and responding to the condition that the active suspension actuator reaches the preset supporting state. According to the method, traditional passive impact bearing is converted into active impact avoiding and buffering, so that collision energy between the wheels and the pothole edge is greatly absorbed, vertical bumping and pitching shaking of a vehicle body under the condition that a single wheel passes through a pit are effectively restrained, and unprecedented stable and comfortable braking experience is provided for passengers.

The utility model discloses a blade for wind power generation, and belongs to the technical field of wind power. The blade comprises a first blade section and a second blade section which are independent of each other, a first section is arranged at the tail end of the first blade section, a second section is arranged at the head end of the second blade section, and the first section and the second section are connected in an assembled mode through a mechanical connecting assembly and an inclined glue joint layer. The mechanical connecting assembly comprises a plurality of single connecting structures which are distributed on the upper side, the lower side and the front edge area of the blade section. An included angle of 30 degrees is formed between the fracture surface and the axis of the blade; the distance between the setting position of the section and the root of the blade is 30-35% of the length of the whole blade; local reinforcing skins are laid on the transition area of the blade root and the easily-damaged area at the position 1 / 3 away from the blade tip. According to the utility model, a mixed connection mode can be adopted, the advantages of the two connection modes can be integrated, and the connection strength is ensured while the weight of the segmented blades is reduced.

The invention relates to the technical field of axial flow fans, in particular to an impeller with S-shaped blades and an axial flow fan applying the impeller. On the axial projection of the impeller, the peripheral contour of each blade is defined by a blade root edge, a blade front edge, a blade outer edge and a blade rear edge, and the blade root edge is connected with the hub; the blade front edge and the blade rear edge are both wavy curves, and the blade root edge and the blade outer edge are both arc-shaped lines with the axis O of the hub as the circle center. Each blade is provided with a pressure face and a suction face, the pressure faces and the suction faces are oppositely arranged, and on the radial projection of the impeller, the pressure faces are arranged in a wave shape in a protruding mode from one end of the blade root edge to one end of the blade rear edge towards the suction faces and then concavely arranged, so that the blades are of an S-shaped structure. The problem that a traditional blade structure cannot meet the use requirements of high efficiency and low noise can be solved.

The invention relates to an active optimization design method of an axial flow fan blade, which comprises the following steps of: defining a blade profile construction line by adopting seven parameters such as a leading edge radius, and parameterizing and representing two-dimensional blade profile geometric characteristics based on NURBS curve control points; a two-dimensional blade profile and three-dimensional fan coordinate system is constructed, and control point coordinate mapping is achieved through matrix transformation; the method comprises the following steps: acquiring an initial sample based on Latin hypercube sampling, and establishing a Gaussian process proxy model by combining two-dimensional CFD calculation data; a K-RVEA algorithm is applied, maximization of a worst attack angle lift-drag ratio and minimization of a resistance coefficient are taken as double targets, Pareto optimization is carried out in combination with geometry and performance constraints, and iteration is terminated through a hyper-volume convergence criterion; and the optimized two-dimensional blade profile parameters are converted into NURBS description, and stacking is carried out in the spanwise direction to generate a three-dimensional blade entity. The grid sensitive effect in three-dimensional optimization is overcome, the flow field analysis precision is improved, invalid calculation is reduced, the blade profile curvature continuity and the process feasibility are guaranteed, and the design period of the axial flow fan is shortened.

The invention relates to the technical field of optics, in particular to blade front and tail edge polishing and correcting equipment which comprises a clamp for loading a to-be-detected guide vane, a polishing system is arranged beside the clamp, and the to-be-detected guide vane is vertically placed on the clamp; the system also comprises a laser interferometer system. The laser interferometer system comprises a laser and a beam splitter, and the beam splitter splits a measuring light beam and a reference light beam; linear collimating lenses are respectively arranged on light paths of the measuring light beam and the reference light beam, and the measuring light beam and the reference light beam respectively penetrate through the collimating lenses to form horizontal linear light beams. On-line real-time detection is achieved through the laser interferometer system, the defect portions of the front edge and the tail edge of the guide vane are accurately positioned, the polishing head can conveniently move to the defect portions to conduct fine polishing, the production period is shortened, and the production cost is reduced.

The invention belongs to the technical field of uncertainty probability characterization analysis, and discloses a thermoplastic composite material leading edge structure design allowable value probability characterization method and system under a small sample condition, and the method comprises the steps: defining a plurality of candidate probability distribution models; fitting each model based on the original sample data and calculating an AIC value and a BIC value; a dynamic weight factor alpha is calculated according to the sample size n, and then a hybrid information criterion HIC value is calculated; generating a plurality of sample sets through Bootstrap self-service sampling, recalculating the HIC value on each sample set, and counting the selected optimal frequency of each model; and determining an optimal probability distribution model according to the frequency, wherein the optimal probability distribution model is used for representing a design allowable value. According to the method, the dynamic weight factor alpha is introduced, AIC and BIC criteria are effectively unified, optimal balance between prediction precision and model complexity is achieved under the condition of small samples, and engineering practicability and robustness are remarkably improved.

A recreational vehicle comprising a generally horizontal floor, a plurality of generally upstanding walls defining a living space in conjunction with the floor, and a seating element in contact with the floor and comprising a plurality of tubular supports and a plurality of generally planar side panels, and wherein: upper edges of the plurality of side panels comprise a first ledge adjacent a front edge and a second ledge proximal a rear edge, the ledges being closer to a lower edge than a remainder of the upper edge is to the lower edge, each of tubular supports extends from a ledge of one side panel to a corresponding ledge of another side panel, and an upper surface of the tubular supports positioned in the ledges is coplanar with the remainder of the upper edge.

The invention relates to the crossing field of mechanical engineering and intelligent manufacturing, and discloses a real-time monitoring, regulating and controlling method for the manufacturing process of an automobile lightweight component. According to the method, a distributed fiber bragg grating sensing array is embedded in a mold, and a three-dimensional strain field at the flowing front edge of resin is obtained in real time; a multi-scale pore generation kinetic model is combined to perform online inversion on an unwetted area and pore distribution; and the pressure gradient and the mold temperature field of the hot press are adaptively regulated and controlled, and the flow path is dynamically corrected. The system comprises a sensing embedding module, a strain demodulation module, a pore inversion module, a regulation and control instruction generation module and a multi-zone execution module. According to the method, closed-loop precise control over the porosity being lower than 0.5% is achieved, and the consistency and reliability of the mechanical property of the component are remarkably improved.

A modular omnidirectional robotic system for navigating nonplanar structures including pipes, poles, chimneys, and trees. The system comprises multiple modules connected by hinges in an open C-shape configuration. Each module contains an omnidirectional drive mechanism with compliant treads, motors, batteries, and controllers. Adjustable tensioning mechanisms adapt to different structure diameters and enable both external and internal operation. The open configuration allows navigation around complex geometries including T-junctions, branches, and sharp bends by aligning the open section with obstructions. Sharp turns are negotiated using the leading edge of the drive mechanism as a pivot point. A control system coordinates module movement using sensors. The system operates on ferrous and non-ferrous materials, features an adaptable payload area for tools and sensors, and can be scaled by adding modules for larger structures.

A lockbar in a tongue of a seat belt system in a vehicle, wherein the crash locking tongue includes the lockbar, a base plate, and a cover material overmolded onto the base plate. The base plate is configured to be reversibly coupled to a buckle in the seat belt system and to have a slot through which a belt webbing extends in order to restrain the movement of a passenger in the vehicle. The lockbar includes one or more fins located on a bottom surface near a front edge, a pair of guide wings located on a back edge adjacent to opposite sides, a clamping surface that is in contact with the belt webbing, and an elastomeric spring. The lockbar undergoes a vertical translation upon a vehicle accident that causes a clamping surface to apply an inward pressure on the belt webbing, thereby, reducing movement of the belt webbing.

A pickleball paddle, comprising a handle, a striking blade, and an edge guard along the perimeter of the striking blade, is provided. The edge guard comprises a front edge configured to partially extend over a front of the striking blade, a back edge configured to partially extend over a back of the striking blade, and a body connecting the front edge and the back edge and comprising at least one of a structural support component extending in a direction of the striking blade or an exterior protection component extending in a direction opposite to the direction of the striking blade.

1. The name of the design product: cutting blade of grader. 2. The use of the design product: usually installed in the front edge of grader blade, used for cutting and leveling ground. 3. The design points of the design product: in shape. 4. The picture or photo that best shows the design points: design 1 perspective view 1. 5. Design 1 is designated as the basic design.

An iron-type golf club head incudes a body, a recessed channel, and a weight assembly. The body includes a striking face, a sole, and a back portion positioned between the sole and the striking face. The striking face includes an upper topline edge and a lower leading edge opposite to the upper topline edge. The recessed channel is formed in the back portion and includes a plurality of dividers. The weight assembly includes a weight at least partially disposed within the recessed channel and configured to engage one of the plurality of dividers in a locked configuration.

A method for joining together two webs includes: overlapping a head portion of the second web on a tail portion of the first web, jointly cutting the head portion of the second web and the tail portion of the first web along a cutting line, so as to form on the first web and on the second web respective front edges offset from each other, and applying a first adhesive splicing tape between a head end of the second web and a tail end of the first web and at the same time aligning frontally with each other the front edges of the first and the second webs.

The invention provides a blade-fused full-rotation shaftless rim propeller, and relates to the technical field of propellers, the blade-fused full-rotation shaftless rim propeller comprises a propeller body, the propeller body comprises a propeller shell, a first driving mechanism and a blade assembly, and the propeller shell is provided with a cylindrical mounting shell and a containing space located on the inner side of the mounting shell; the first driving mechanism comprises a stator assembly and a rotor assembly which are coaxially arranged on the inner side of the accommodating space; the paddle assembly comprises a plurality of main paddles and a plurality of auxiliary paddles, the main paddles are evenly distributed along the inner circumference of the rotor assembly, the guide edges of the main paddles are of zigzag bionic structures, the auxiliary paddles are located between the adjacent main paddles, the chord length of the auxiliary paddles is 30%-50% of the chord length of the main paddles, and the front edges of the auxiliary paddles are arranged close to the guide edge sides of the main paddles. Through the collaborative design of the main paddle and the auxiliary paddle, the sawtooth-shaped guide edge is used for damaging the vortex continuity, the auxiliary paddle guides secondary flow and inhibits pressure fluctuation, and the technical problems that a traditional propeller is high in noise, low in efficiency and disordered in flow field in a closed flow channel environment are solved.

A molded fiber packaging system for a toilet includes a first molded fiber tray comprising a toilet bowl cavity molded to receive a top portion of a toilet bowl, a first outer edge comprising an overhang that is configured to extend over a nose of the toilet bowl along an outer surface of the bowl toward a base of the bowl, a first tank cavity molded to fit a back portion of a toilet tank, a first tank lid cavity molded to fit a back edge of a toilet tank lid, and one or more protrusions positioned between the first toilet tank cavity from the first lid cavity. The system includes a second molded fiber tray comprising a second tank cavity molded to fit a front portion of the toilet tank and a second lid cavity molded to fit a front edge of the toilet tank lid.

A vehicle rocker assembly includes a sill outer and a sill inner that together define an elongated hollow interior. The vehicle rocker assembly also includes a rocker insert disposed within the elongated hollow interior. The rocker insert includes a stiffening member defining a wave-shaped structure and including at least one sheet defining a fore edge, an aft edge, a first side edge and a second side edge opposite the first side edge. Additionally, the fore edge and the aft edge are disposed at different locations along the length of the rocker insert. Moreover, a crest of the wave-shaped structure extends between the first side edge and the second side edge and is configured to carry a load path laterally between the inboard and outboard wall portions.

The invention relates to the technical field of section line fairing, in particular to a curvature fairing method for the front edge and the rear edge of a blade modeling section line, and the method comprises the following steps: 1, importing a three-dimensional model of an impeller, and obtaining the blade section line of the impeller; step 2, solving discrete points on the section line in an isoparametric manner, and converting Cartesian three-dimensional coordinates of the discrete points into two-dimensional cylindrical coordinates; 3, finding out an initial leading edge endpoint and an initial trailing edge endpoint of the section line by using a central axis algorithm; step 4, according to the curvature of the front edge endpoint and the curvature of the rear edge endpoint, determining a segmentation point of the front edge endpoint and a segmentation point of the rear edge endpoint respectively; 5, the curvature of the front edge and the curvature of the rear edge are smoothed, curve smoothing is carried out in a third-order derivative mode, position constraint and end point constraint are carried out on the basis of an original curve, and the curve can achieve the curve smoothing effect within the minimum range.

A runner for a hydraulic turbine, including a hub and a plurality of pivotable blades extending from the hub. Each pivotable blade of the plurality of pivotable blades includes a root located at the hub, a tip opposite the root, and a leading edge. Each pivotable blade of the plurality of pivotable blades is pivotable relative to the hub about a respective pivot axis. For at least one blade, the leading edge at the root is positioned along a radial axis of the runner and the leading edge at the tip is cantilevered beyond the radial axis in a circumferential direction of the runner.

An adjustable workstation includes a tabletop having opposed upper and lower surfaces, a leg for supporting the tabletop, a gas spring having opposed spring front and rear ends, and a tabletop mount affixed to an upper end of the leg and pivotably coupled to the lower surface of the tabletop at a tilt axis. The spring front end is pivotably coupled to the lower surface of the tabletop. The spring rear end is pivotably coupled to the mount at an elevation lower than the tilt axis. The tabletop pivots in a first direction about the tilt axis upon extension of the gas spring to raise a front edge of the tabletop relative to a rear edge of the tabletop. The tabletop pivots in a second direction about the tilt axis upon retraction of the gas spring to lower the front edge of the tabletop relative to the rear edge of the tabletop.

The invention relates to the technical field of plastic molding processes, and discloses a negative pressure injection molding plastic molding method and device. The method comprises the steps that in the negative pressure injection molding process, gas parameter data of a plurality of monitoring points in a mold cavity are obtained in real time; based on the change of the gas parameter data of each monitoring point, identifying the state of the gas pushed by the melt, and determining the propulsion path of the melt flowing front edge in the cavity; according to the propelling path, the melt filling progress and the filling time sequence of all areas in the cavity are calculated; and based on the filling progress and the filling time sequence, generating evaluation information of the filling state of the melt in the cavity. According to the method, the real-time visual prediction of the melt filling process in the mold is realized, and the control accuracy of the negative pressure injection molding process and the stability of the product quality are improved.

A fixed cutter drill bit for drilling an earthen formation has a central axis and a cutting direction of rotation about the central axis. The drill bit includes a bit body configured to rotate about the central axis in the cutting direction of rotation. The bit body includes a bit face and a blade extending radially along the bit face. The blade has a leading side relative to the cutting direction of rotation, a trailing side relative to the cutting direction of rotation, and a cutter-supporting surface extending from the leading side to the trailing side. The blade includes a socket extending from the leading side of the blade and penetrating the cutter-supporting surface of the blade. The socket has a central axis, an open end at the leading side of the blade, and a closed end distal the leading side of the blade. The socket has (i) a first width W1 in a front view of the blade measured parallel to a projection of the cutter-supporting surface across the socket in the front view at a first distance D1 measured perpendicular to the projection of the cutter-supporting surface in the front view, and (ii) a second width W2 in a front view of the blade measured parallel to the projection of the cutter-supporting surface across the socket in the front view at a second distance D2 measured perpendicular to the projection of the cutter-supporting surface in the front view. The second distance D2 is greater than the first distance D1 and the second width W2 at the second depth D2 is greater than the first width W1 at the first width W1. In addition, the drill bit includes a cutter element assembly mounted to the blade and extending from the cutter-supporting surface of the blade. The cutter element assembly includes a cutter element carrier seated in the socket and fixably attached to the blade. The cutter element carrier includes a base that mates with the socket. The cutter element assembly also includes a cutter element fixably attached to the cutter element carrier.

A front opening crib assembly for easing the task of child placement and retrieval includes a sleeping structure, which in turn comprises rear, bottom and a pair of side panels, a pair of doors, and a latching device. Each side panel has a rear edge that is attached to a respective opposed edge of the rear panel. The bottom panel is attached to of the side panels proximate to their lower edges and to the rear panel proximate to its bottom edge. The bottom panel supports a mattress pad. Each door is hingedly attached to a respective side panel proximate its front edge. The panels and doors define a sleep space that is substantially cuboid, open topped, and accessible by swinging the doors outwardly. The latching device selectively secures the doors in a closed configuration.

The invention relates to the technical field of wind power generation, in particular to a blade deicing device and method and a wind generating set, and the blade deicing device comprises heating modules which are arranged on the front edge, the rear edge, the pressure surface and the suction surface of a blade and used for heating an ice layer on the surface of the blade; the monitoring module is mounted on the surface of the blade and is configured to monitor the ice layer thickness, the environment temperature and the humidity of the surface of the blade; the control module is electrically connected with the heating module and the monitoring module, and the control module is configured to start the heating module to deice if the thickness of the ice layer is larger than or equal to a first threshold value and the environment temperature and humidity meet the icing condition. The icing state of the blade can be intelligently monitored, efficient deicing is achieved, and energy conservation and environmental protection are achieved.

The invention discloses a gasoline filter element assembly machine and a using method thereof, and belongs to the technical field of gasoline filter element assembly.The gasoline filter element assembly machine comprises a workbench, a plurality of filter material positioning mechanisms are linearly arranged on the side wall of the workbench at equal intervals, and paper filter materials to be glued are arranged on the filter material positioning mechanisms; a downward pressing mechanism is arranged at each circular opening in the upper surface of the workbench, an end cover is arranged at the output end of each downward pressing mechanism, the filter material positioning mechanism comprises a cylinder, a cover body and a chassis, a limiting plate is arranged on the side wall of the cylinder, the front edge of the limiting plate can make contact with a crease of a paper filter material, and a gluing mechanism is arranged above the cylinder. The folding marks of the paper filter material are limited, deformation, deviation and adhesion of the folding marks during gluing are avoided, the design can be adjusted to adapt to filter materials with different folding mark numbers, universality is improved, glue brushing is guided, glue consumption is reduced, overflowing and hole blocking are prevented, the filter area is guaranteed, the process is simplified through integrated design, the rejection rate is reduced, and the filter performance and efficiency are both considered.

A self-closing door assembly for limiting access to goods displayed on a shelving system. A frame assembly is attached to the shelving system adjacent the front edge of a first shelf, with upper and lower guide rails to slidably engage a pair of overlapping and self-closing doors. The doors are aligned to laterally slide open from a closed position at which they interfere with manual access to the goods displayed on the shelf. Biasing members disposed between the frame assembly and the doors urge the doors toward the closed position. The doors are adapted for manual engagement to be urged toward the open position, and the biasing members automatically return the doors to the closed position upon manual release thereof.

The invention provides an axial flow fan blade and a fan comprising the same. The axial flow fan blade comprises a hub and blades. Each blade sequentially comprises a plurality of base circle sections in the direction from the blade inner edge to the blade outer edge. The contour line SP of each base circle section is generated by a first multinomial function; the starting points of the contour lines SP are connected together to form a blade front edge, the blade front edge is a large-radian curved surface, and the blade front edge is generated by a second multinomial function; the chord length L of each contour line SP is generated by a third multinomial function; the suction surface and the pressure surface of the blade in the direction from the inner edge of the blade to the outer edge of the blade are both of a curved surface structure, and the curved surface is generated by boundary mixing of a fourth multi-term function; the end points of the contour lines SP are connected together to form a blade tail edge, and the blade tail edge is of a wavy curved surface structure and is generated by a fifth multi-term function. The blades and the trailing edge of the axial flow fan blade are both based on multi-frequency harmonic superposition collaborative optimization design, the operation power consumption of the fan blade is remarkably reduced while the requirement for the air volume is met, and noise is greatly restrained.