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56 results about "Buckling instability" patented technology

Buckling instability is a treacherous phenomenon in structural engineering, where a small increase in the load can lead to a sudden catastrophic failure.

Buckling restrained energy-consumption supporting device of building frame structure

The invention relates to a buckling restrained energy-consumption supporting device of a building frame structure, which consists of an energy-consumption steel tube (1), an inner restraining steel tube (2), an outer restraining steel tube (3) and connecting steel plates (4 and 5). Corrugations are formed on the outer side of the wall of the energy-consumption steel tube (1) at certain intervals, two ends of the energy-consumption steel tube (1) are respectively connected onto the connecting steel plates (4 and 5), and the inner restraining steel tube (2) and the outer restraining steel tube (3) are placed on the inner side and the outer side of the energy-consumption steel tube (1). The buckling restrained energy-consumption supporting device of the building frame structure has the advantages of high rigidity and deformation ability, easiness in control of buckling, avoidance of buckling instability and high energy consumption ability, and is accurate in stress, simple in structure, convenient in manufacture, easy in installation and maintenance and fine in durability. The buckling restrained energy-consumption supporting device can be used for buildings with multilayered and high-rise concrete structures and buildings with steel structures, and resolves the problem of insecurity of the structures of the buildings in violent earthquake.
Owner:卢锐

Thin plate weld with trailing deformation control device and method with dynamic hot stretching and chilling combined

The invention relates to a thin plate weld with trailing deformation control device and method with dynamic hot stretching and chilling combined. The thin plate weld with trailing deformation control device comprises a walking module, a connecting device and a weld with trailing deformation control module. The weld with trailing deformation control module is borne on the walking module through the connecting device. The weld with trailing deformation control module comprises a dynamic hot stretching module, welding gun modules and a trailing intensive cooling module. Parallel transverse swing heating of dual TIG arcs can be achieved through the dynamic hot stretching module. The thin plate weld with trailing deformation control method comprises the steps that the TIG arcs are used for carrying out dynamic hot stretching on the two sides of a welding seam before welding, the welding seam is welded, and then a chilling medium is used for carrying out chilling on the welding seam. According to the thin plate weld with trailing deformation control device and method, the overall structure is compact, and the size is small; and on the basis of guaranteeing the quality of the welding seam, the welding residual stress level can be lowered, and compressional buckling instability and bending deformation can be controlled well.
Owner:CSSC HUANGPU WENCHONG SHIPBUILDING COMPANY

Heavy-load six-degree-of-freedom compliant parallel robot system

The invention belongs to the technical field of manipulators, and discloses a heavy-load six-degree-of-freedom compliant parallel robot system. Six small electric cylinders are adopted to drive to realize six-degree-of-freedom movement of a moving platform of three-degree-of-freedom of translational movement and three-degree-of-freedom of rotary movement, and upper and lower platforms and the electric cylinders are connected by bevel fixing blocks and force steering parts. Compliant spherical hinges are core parts of the force steering parts, and the single force steering part is composed of one compliant ball hinge and two U-shaped parts. The gravity of compliant hinges borne from other parts and the pressure exerted by the moving platform load on the compliant hinges are turned into tensile force on the compliant hinges through the force steering parts, and the advantages of a conventional six-degree-of-freedom platform are combined with the advantages of a compliant mechanism. Afterthe improvement of the force steering parts of the compliant hinge design, the positioning accuracy of the mechanism can reach a micron level, and the bearable load is much more than a few grams, sothat the compliant ball hinges do not generate buckling instability due to excessive load and can realize micro size motion.
Owner:XIDIAN UNIV

Buckling micro-force sensor and micro-force measuring method based on twin beams or serial connection twin beams

InactiveCN103471745AMeet force measurement requirementsConducive to systematizationForce measurementStructural/machines measurementCapacitanceBuckling instability
The invention discloses a buckling micro-force sensor and a micro-force measuring method based on twin beams or serial connection twin beams, and belongs to the fields of micro-nanomechanics and precise measurement. A group of symmetrical slim beams or two groups of serial connection slim beams are adopted in the sensor, the slim beams are arranged in a parallel mode, one end of each slim beam is fixed, the deformation of the slim beams is limited through limiting ends, a load is applied through a probe and a capacitor, and the displacement is measured. In the process of using, the twin beams are bent to be instable in the axis in advance, and the buckling mode of the twin beams is kept. By appropriately leading in the transverse displacement of the twin beams, the obvious transverse displacement change of the twin beams can be obtained under the very small axial force within a certain load range, and the value of the measured micro-force is obtained through load calculation based on the buckling instability formula or directly obtained through the changes of the displacement via the early calibration. The buckling micro-force sensor is simple in structure and in sensitivity, sequence sensors in different measuring ranges can be formed, and therefore the micro-force measuring method and the sensor design both of which have a wide range of loads and high sensitivity can be provided for the measurement of the micro-nanomechanics.
Owner:TSINGHUA UNIV

Multi-girder structure large size wind power blade and production method thereof

ActiveCN105508142AImprove the ability to resist buckling instabilityImprove structural rigidityEngine manufactureFinal product manufactureFiberCarbon fibers
The invention discloses a multi-girder structure large size wind power blade and a production method thereof. The multi-girder structure large size wind power blade is in a hollow layout structure, and comprises a blade envelope suction edge, a blade envelope pressure edge, main load-carrying construction girders and shearing-resistant web plates, wherein the blade envelope suction edge and the blade envelope pressure edge are combined to form a cavity structure of which the cross section is streamlined; a supporting structure formed by the main load-carrying construction girders and the shearing-resistant web plates is arranged in the cavity structure formed by the blade envelope suction edge and the blade envelope pressure edge; and the blade envelope suction edge and blade envelope pressure edge are in multisection combination structures, and are connected with the side surfaces of the main load-carrying construction girders through a plurality of edge sections respectively to form a blade envelope suction edge and blade envelope pressure edge integrated body. On the premise of ensuring the rigidity and strength of the blade, the resistance to buckling instability of the blade is improved; and by adopting a high-module carbon fiber spread layer, the weight of the blade can be reduced obviously, and loads, particularly a fatigue load, of the blade are reduced.
Owner:ZHUZHOU TIMES NEW MATERIALS TECH

Economical creep aging forming method of large thin-wall component

ActiveCN111195678AInhibition of local buckling instabilitySave materialBuckling instabilityThin walled
The invention discloses an economical creep aging forming method of a large thin-wall component. The economical creep aging forming method comprises the steps that two component plates are firstly cutout; the two component plates are fixed to form a reinforcing plate, and the reinforcing plate is completely covered by ventilated felt and then placed on a mold surface, specifically, the first component plate is close to the mold surface, and the second component plate is away from the mold surface; a vacuum bag is pasted on the edge of a mold to make the vacuum bag and the mold form a closed space; the closed space is vacuumized to make the reinforcing plate approach or keep fit with the mold surface, then the reinforcing plate and the mold are put into a hot-pressing tank to be subjectedto vacuum creep aging forming, and each component plate is separated from the mold after the vacuum creep aging forming is finished; the allowance plate of the first component plate is milled off; andthe process of the vacuum creep aging forming of the reinforcing plate is repeatedly performed on the second component plate to finish a second component. According to the economical creep aging forming method, the precise shape-property integrated forming of the large thin-wall component can be realized, the local buckling instability condition of a component with weak rigidity in the creep aging forming process is effectively inhibited, and meanwhile, the material and the forming time can be saved.
Owner:CENT SOUTH UNIV

Creep age forming method for large thin-wall component

ActiveCN111195677AInhibition of local buckling instabilityReduce weightBuckling instabilitySealant
The invention discloses a creep age forming method for a large thin-wall component. The method comprises the following steps that firstly, an aluminum alloy blank is cut into a component plate containing a component unfolding body; a metal plate is cut into an auxiliary plate with an outer contour consistent with an outer contour of the component plate; the component plate and the auxiliary plateare tightly attached and fixed to form a reinforcing plate; the reinforcing plate is placed on a mold face, and the reinforcing plate is completely coated with ventilated felt; a sealant is pasted onthe edge portion of a mold, and a vacuum bag is pasted on the sealant so as to make the vacuum bag and the mold jointly form a closed space; the closed space is vacuumized to make the reinforcing plate be close to or keep attached to the mold face; the reinforcing plate and the mold are put into an autoclave for vacuum creep age forming, and after completion, the component plate, the auxiliary plate and the mold are separated; and an allowance plate is milled. According to the method, precise shape and property integrated forming of the large thin-wall component can be achieved, and a local buckling instability condition of the component with the weak rigidity in the creep age forming process is effectively restrained.
Owner:CENT SOUTH UNIV

Anti-buckling design method for thin-wall exhaust nozzle of aero-engine

The invention belongs to the field of aero-engine structural design, and discloses an aero-engine thin-wall exhaust nozzle buckling resistance design method which comprises the following steps: S1, determining structural parameters and load of a thin-wall exhaust nozzle; s2, finite element buckling simulation analysis is conducted on the thin-wall exhaust nozzle, and a first-order critical instability load coefficient and a buckling instability vibration mode cloud picture are obtained; s3, based on a finite element buckling simulation analysis result, finding a maximum deformation position in the buckling instability vibration type cloud picture, and applying an annular mounting edge; and S4, finite element buckling simulation analysis is conducted on the thin-wall exhaust nozzle with the installation edge applied, a first-order critical instability load coefficient and a buckling instability vibration mode cloud picture are obtained and calculated, whether the first-order critical instability load coefficient meets the requirement or not is judged, if not, the steps S3-S4 are repeated, and if yes, the process is ended. The rigidity and stability of the thin-wall spray pipe can be effectively improved, the structural weight cannot be obviously increased, and meanwhile the overall appearance and pneumatic performance of the spray pipe cannot be affected.
Owner:TAIYUAN UNIV OF TECH

Stacked paper folding structure with variable stiffness characteristic

The invention discloses a stacked paper folding structure with variable stiffness characteristics, which comprises a plurality of layers of paper folding tubes stacked up and down, each paper foldingtube comprises two symmetrically arranged paper folding plates, each paper folding plate comprises a plurality of basic units, the basic units are connected in sequence, each basic unit comprises n small planes and two large planes, n is an even number greater than 2, the width ratio of the large plane to the small plane is n/2, and the large plane and the small plane are parallelograms. Due to the fact that all layers of paper folding pipes of the stacked paper folding structure are different in rigidity, when the stacked paper folding structure is subjected to compression force from top to bottom, the stacked paper folding structure generates a layer-by-layer progressive buckling instability process, firstly, the paper folding pipe with the minimum rigidity is subjected to buckling instability, and then the paper folding pipe with the second small rigidity is triggered to be subjected to buckling instability; therefore, the paper folding pipe with the maximum rigidity is obtained through recursion, and then the variable rigidity characteristic of the stacked paper folding structure is achieved. According to specific requirements, multiple layers of paper folding pipes with different rigidities can be stacked, and multiple variable stiffness characteristics are achieved.
Owner:GUANGZHOU UNIVERSITY

Airworthiness compliance verification method for combustion chamber casing

The invention discloses an airworthiness compliance verification method for a combustion chamber casing. The method comprises the steps of (1) determining a load boundary condition of the combustion chamber casing according to clauses and requirements of CCAR 33.64, and determining a displacement boundary condition according to a constraint situation under an actual working condition; (2) conducting an eigenvalue buckling analysis on the combustion chamber casing, and obtaining eigenvalues and eigenvalue buckling modes under different orders; (3) selecting a first-order buckling instability portion of the casing as analysis focus, and performing a geometrical and material double nonlinear buckling analysis under a condition (1); (4) calculating a stability safety factor as the condition for determining the stability of the casing; (5) using a nonlinear buckling critical load obtained in (3) through analysis as an internal and external gas pressure difference, loading the boundary condition in (1) for a static strength analysis, and determining the compliance of the combustion chamber casing with the airworthiness clauses. The method simultaneously considers the stability and staticstrength of the combustion chamber casing, proposes a targeted verification analysis method, and indicates the airworthiness compliance of the combustion chamber casing.
Owner:BEIHANG UNIV

Device for lateral displacement control during integral buckling of submarine pipeline

InactiveCN104500837ARestrained buckling deformationIncrease lateral soil resistancePipe laying and repairOcean bottomEngineering
The invention belongs to the technical field of ocean engineering and relates to a device for lateral displacement control during integral buckling of a submarine pipeline. The device comprises a strain sensor, a power source, a control circuit, an annular rigid structure with peripheral projections, a protecting layer and an actuating mechanism capable of enabling the protecting layer to be stripped off. A support of the strain sensor is a ring matched with the external diameter of the pipeline, strain foils of the strain sensor are distributed circumferentially uniformly along the ring, the internal diameter of the annular rigid structure is larger than the external diameter of the support of the strain sensor, the protecting layer is arranged on the outer portion of the annular rigid structure and used for protecting the annular rigid structure to enable the annular rigid structure not to contact with a seabed, and the control circuit is used for controlling whether or not the actuating mechanism actuates and the protecting layer needs to be stripped off according to strain signal values collected by the strain sensor. The device is capable of solving the problem of overlarge lateral displacement during integral buckling of the submarine pipeline effectively and controlling lateral buckling instability of the pipeline.
Owner:TIANJIN UNIV

Forging forming die and method for cylindrical part plate with small fillet characteristic

The invention discloses a forging forming die for a cylindrical part plate with a small fillet characteristic. The forging forming die comprises an inner side male die, an outer side male die, a female die, a female die base plate and a floating mandrel. The invention further provides a forging forming method for the cylindrical part plate with the small fillet characteristic. A pipe blank with the outer diameter equal to that of a cylindrical target part is put on the female die base plate, and the inner side male die and the outer side male die are driven to synchronously move downwards at aconstant speed to upset and extrude the pipe blank to form an inner flange upsetting piece. After moving to the lower limit, the outer side male die is kept still with constant load, the inner side male die continues to descend to shear the inner flange upsetting part, a metal material is forced to continuously flow to a closed cavity defined by the inner side male die, the outer side male die, the female die, the female die base plate and the floating mandrel, and finally the cylindrical part with the small fillet characteristic is upset and extruded. The cylindrical part with the small fillet characteristic is formed in one procedure, the buckling instability problem is solved, the defects of folding, inward sinking and the like are overcome, and the fillet filling plumpness and the mechanical property of the target part are improved.
Owner:XIANGTAN UNIV

Method for controlling lateral displacement of submarine pipeline

InactiveCN104455728ARestrained buckling deformationIncrease lateral soil resistancePipe laying and repairOcean bottomBuckling instability
The invention belongs to the field of ocean engineering technology and particularly relates to a method for controlling lateral displacement of a submarine pipeline. An adopted control device comprises stress sensors, a power source, a control circuit, an annular rigid structure with a protrusion on the periphery, a protective layer, and an actuating mechanism capable of enabling the protective layer to be stripped off. Supports of the stress sensors are circular rings matched with the outer diameter of the pipeline, strain gauges of the stress sensors are distributed in the annular direction of the circular rings, the inner diameter of the annular rigid structure is larger than the outer diameter of the supports of the stress sensors, and the protective layer is arranged outside of the annular rigid structure. The control device is arranged outside the weak position of the submarine pipeline, and the control circuit controls the actuating mechanism to act according to whether strain signals collected by the stress sensors are too large, so that the protective layer is stripped off. By means of the method for controlling the lateral displacement of the submarine pipeline, the problem of too large lateral displacement in the overall buckling process of the submarine pipeline can be effectively solved, and the lateral buckling instability of the pipeline is controlled.
Owner:TIANJIN UNIV

Power transmission tower reinforcing device capable of preventing bending and buckling instability

The invention provides a power transmission tower reinforcing device capable of preventing bending and buckling instability, and belongs to the technical field of iron tower reinforcement. The power transmission tower reinforcing device comprises reinforcing channel steel, a reinforcing steel column, two pieces of reinforcing T-shaped steel and a reinforcing outer connecting plate, wherein the reinforcing outer connecting plate is fixedly connected with two free ends of the reinforcing channel steel separately; the reinforcing outer connecting plate and the reinforcing channel steel are enclosed to form a rectangular cavity for accommodating the reinforcing steel column and the two pieces of reinforcing T-shaped steel; the two pieces of reinforcing T-shaped steel and the reinforcing channel steel are enclosed to form a triangular cavity for accommodating power transmission tower angle steel; and the reinforcing steel column and the reinforcing T-shaped steel are separately positioned at the inner side and the outer side of two limbs of the power transmission tower angle steel. According to the power transmission tower reinforcing device capable of preventing bending and buckling instability provided by the invention, the two pieces of reinforcing T-shaped steel and the reinforcing outer connecting plate are arranged at the outer side of the power transmission tower angle steel, and the reinforcing steel column and the reinforcing channel steel are arranged at the inner side of the power transmission tower angle steel, so that the power transmission tower reinforcing device has a prominent bending and buckling preventing effect, has enough stability, is simple in structure, is simple and convenient to mount, and is low in cost.
Owner:HEBEI HUIZHI ELECTRIC POWER ENG DESIGN CO LTD +3
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