51results about How to "Guaranteed Assembly Requirements" patented technology

The invention provides a machining method of a cabin section work-piece. The work-piece comprises end faces. The method comprises the steps of: determining the planeness of the end faces by taking the end faces of the work-piece as benchmarks; determining a rough machining center of the work-piece by taking pin holes and bottom holes in the end faces as benchmarks; carrying out rough machining on a profile of the work-piece and detecting a machining allowance of each end face; carrying out finish machining on the profile of the work-piece by using a diamond milling cutter according to a preset size; determining a finish machining center of the work-piece by taking the finish-machined profile as a benchmark; carrying out side-edge cutting and bottom-edge cutting on the end faces and end face sealing lug bosses by using a diamond coating milling cutter; carrying out boring-machining on the pin holes in the end faces; pressing out notch edges of a notch by using a pressing plate; and carrying out segmental machining and layered machining on the notch with a preset cutting step length by using a spiral cutting method. Thus, by using a benchmark conversion machining method, the problem of non-uniform wall thicknesses caused by machining deformation in a single benchmark is solved, and the phenomena of scaling-off, breaking-up and delaminating appearing during machining are avoided.

The invention discloses a feeding type cylinder side edge strip wing drilling fixture, and belongs to the field of fixtures. The drilling fixture comprises parts such as a fixture body, a drilling jig plate, a rotation shaft, an adjustable positioning plate, a blanking cap, a pressing disc, a limiting block, a compression screw, a knurled thumb screw, a positioning plug pin a, a positioning plug pin b, quick-changing drilling bushings and a bolt washer assembly. By adopting the drilling fixture, the hole machining precision can be greatly improved, the assembling requirement of a corresponding product is guaranteed, occupation of a machining center can be reduced, the machining cost is reduced, and the working efficiency is improved. Through actual detection, when drilling and reaming machining is conducted on sixteen holes formed in four side edge strip wings of a cylindrical product with the diameter of 400 mm and the length of 500 mm by adopting the drilling fixture, the position degree can meet the requirement of 0.1 mm.

The invention relates to a device for measuring a rotor bracket of a hydrogenerator oblique stud support arm structure. The invention belongs to the technical field of hydrogenerators. The device for measuring the rotor bracket of the hydrogenerator oblique stud support arm structure has the characteristics that: the device for measuring the rotor bracket comprises a basic annular plate, a wide yoke rim sheet, and a laminated inspection pin; the height-adjustable basic annular plate is arranged on the external circle bottom of a stud of the rotor bracket; the basic annular plate is provided with the laminated inspection pin to laminate the wide yoke rim sheet into a full circle yoke ring; and an equally-dividing positioning frame is embedded in an internal circle yoke key groove of the laminated full circle yoke ring. The invention has the advantages of simple structure, convenient operation, safe use, reliable performance, precise detection and the like; the requirement of rotor assembling is guaranteed, the progress for detecting the rotor bracket of the hydrogenerator oblique stud support arm structure is greatly improved, the measurement fixture cost is saved, the smoothness of the rotor assembling is guaranteed, and the designing and manufacturing level and the production efficiency are improved.

The invention discloses a flexible support device suitable for multiple model powertrain assemblies. The support device comprises a left mounting base and a right mounting base, a first positioning support mechanism for supporting an engine is arranged on the left mounting base, and a second positioning support mechanism for supporting a rear axle is arranged on the right mounting base. The flexible support device suitable for the multiple model powertrain assemblies has the advantages that supporting bases and positioning bases of multiple model engines are integrated on the first positioningsupport mechanism, the supporting bases and the positioning bases of multiple model rear axles are integrated on the second positioning support mechanism, the production cost is effectively reduced,and the storage space is saved; the assembly needs of different sized powertrains can be met by switching between the supporting bases during an assembling and switching between the positioning bases,the assembly efficiency is effectively improved, the intensity of work is reduced, under the premise of ensuring the production demand, an operator can easily complete all the assembly tasks; meanwhile the positioning bases have positioning and supporting functions, the assembly accuracy of powertrains is ensured, and the skill requirements of the operator are reduced.

The invention discloses a special angular contact ball bearing for a liquid vortex flow retarder, comprising an outer ring (1), an inner ring (2), a steel ball (3) and a holder (4). The special angular contact ball bearing is characterized in that a bearing contact angle alpha is 40 DEG; the small end surface of the outer ring (1) is provided with an upper step (6) and a lower step (8), and a roller path of the outer ring (1) is provided with a lock dot (7); the end surface of the inner ring (2) is provided with an annular groove (9), the outside diameter surface (10) of the inner ring (2) can be used as a piston for sealing a cylinder, a step (11) is arranged above a roller path of the inner ring (2), and a lock dot (12) is arranged below the roller path of the inner ring (2); the holder (4) is led by the steel ball (3), and an angle (beta) of the holder (4) is 30 DEG. The invention has the advantages of compact structure, high rotation speed, long service life, good lubricating property, flexible rotation and steady operation, can simultaneously bear the jointed load of a radial direction and an axial direction and can especially bear heavier axial load. The special angular contact ball bearing can not be heated when urgently stopping at the speed of 2800 rotations/minute and has low manufacture cost and convenient installation.

The invention relates to the technical field of cell parallel battery modules, in particular to a 21700 cell series-parallel battery module. The 21700 cell series-parallel battery module comprises a plurality of 21700 battery module units arranged in sequence, and the 21700 battery module units penetrate through a fixed part in sequence and are fixed into a whole; each 21700 battery module unit comprises a module housing and a plurality of 21700 single cells, parallel confluence plates are mounted on two outer walls of the module housing, and a plurality of insertion slots and electrode insertion through holes are provided in two inner walls of the module housing. According to the 21700 cell series-parallel battery module, the 21700 single cells are fixed in the module housing by insertingand clamping, and the 21700 battery module units are correspondingly clamped and limited and penetrate through bolt nut connectors, which can meet the high-strength structure required for the series-parallel battery module composed of 21700 single cells with large capacity, the structure is simple, and the manufacturing cost is low.

The invention provides a tailor-welding method of an excavator main platform. The tailor-welding method comprises the following steps: hanging a main bottom plate in a fixture, pressing the fixture after positioning with a centre of rotation; hanging a left side plate assembly on the main bottom plate to be fixed by spot welding; hanging a front closing plate on the main bottom plate to be fixed by spot welding; hanging a beam on the fixture to be fixed by spot welding; hanging a right side plate assembly on the main bottom plate to be fixed by spot welding; sectionally welding the joints among the left side plate assembly, the right side plate assembly, the front closing plate and the beam; then arranging a left plug plate and right lug plate in the fixture to be fixed by spot welding. The tailor-welding method of the excavator main platform provided by the invention comprises the following steps: firstly positioning with the centre of rotation of the main bottom plate, orderly combining other parts at a positioned left side plate assembly, and sectionally welding the joints among the left side plate assembly, the right side plate assembly, the front closing plate and the beam, thereby improving the welding quality and efficiency; and the welding can achieve the assembling requirement.

The invention relates to the field of welding, in particular to a 300MW heavy-duty gas turbine nozzle hula seal assembly welding restraining tool and a use method. The 300MW heavy-duty gas turbine nozzle hula seal assembly welding restraining tool and the use method aim at solving the problems that a hula seal molded line and radian are changed due to the fact that the unrestrained end of a 300MWheavy-duty gas turbine nozzle hula seal is deformed to release welding tensile stress, and the follow-up assembly is influenced. The 300MW heavy-duty gas turbine nozzle hula seal assembly welding restraining tool is designed and manufactured and comprises a restraining force application part and a restraining belt, wherein the restraining belt is annular when working, one end of the restraining belt is connected with the restraining force application part, the other end of the restraining belt is tightened through the restraining force application part, the hula seal is forcibly restrained byusing the restraining tool all the time in the high-temperature alloy hula seal and nozzle assembling and welding process, the temperature difference of different positions disappears after welding iscompleted, after a certain welding stress is released, the restraining tool is removed, it is guaranteed that the free end of the hula seal does not have larger free deformation, it is further guaranteed that the molded line and radian of a product meet drawing and design requirements, and the subsequent combustion chamber assembling requirement is met.

The invention discloses a hydraulic cylinder, including a cylinder barrel (1), wherein one end of the cylinder barrel (1) is connected with a cylinder bottom (2) while the other end forms a cylinder rod extending end, a first sealing member (5) is arranged on the inner peripheral surface of the cylinder rod extending end, the cylinder barrel (1) and the cylinder bottom (2) are fixed with each other by a positioning member positioned in the cylinder barrel (1) and simultaneously stopping the cylinder barrel (1) and the cylinder bottom (2). The hydraulic cylinder can simultaneously meet the requirements on strength, assembly and dimensional limit.

The invention relates to a lead bending die of a rotor winding and a processing method, belonging to the technical field of hydraulic generators. The lead bending die of a rotor winding is provided with a soleplate, a line-pressing plate, a positioning plate and a supporting plate, wherein the soleplate and the supporting plate are vertically fixed together, the positioning plate is fixed on the soleplate and provided with a notch in a position where a lead is pressed to be bent at the bottom, and the line-pressing plate is fixed on the positioning plate which is used for positioning and bending the end of the rotor winding. The lead bending processing method of the rotor winding comprises the following steps of: annealing the rotor winding through a copper bar, edgewise winding, secondarily annealing, cold pressing, scribing the lead, dipping tin and drilling holes and carrying out the lead bending treatment of the rotor winding; and putting the rotor winding on a bending die, firmly clamping the copper bar lead by a compressing bolt through the line-pressing plate and bending the lead by adopting shape-beating mode of an iron hammer. The invention has the advantages of simple structure, rapid operation, time and labor saving, less working hour consumption, high production efficiency, high winding lead bending quality, and the like.

The invention discloses a double-layer composite plastic floor. The double-layer composite plastic floor comprises a floor surface layer and a floor cushion layer which is arranged under the floor surface layer, wherein the floor surface layer and the floor cushion layer are paralleled to each other and are horizontally and longitudinally connected together in a dislocation adhesion way, bulge parts between the floor surface layer and the floor cushion layer are formed into connecting strips and connecting lap strips, and adhesive sticker is coated on connecting surfaces opposite to the connecting strips and/or the connecting lap strips; and the floor cushion layer is formed by connecting a left floor cushion layer and a right floor cushion layer through connecting rabbets in a clamping way, the connecting rabbets are just arranged at long sides of the floor cushion layer and are formed by convex tenons and concave mortises, the convex tenons and the concave mortises are respectively arranged at long edges at two sides of the floor cushion layer and can form inserting connection, the convex tenons and the concave mortises are of parallelograms, and the convex tenons and the concave mortises are matched. According to the double-layer composite plastic floor disclosed by the invention, the inserting connection of the tenons and the mortises can be easily and quickly realized, and thus the assembly and the disassembly of a floor can be easy and efficient; and through an optimization structure, the manufacturing technology difficulty can be reduced, the manufacturing cost can be reduced, and the structural strength of a connecting tenon can be increased.

The invention belongs to the field of fasteners special for connection and looseness-proof of aerospace, and provides a locking double-end stud assembly structure with a stopping station. The lockingdouble-end stud assembly structure with the stopping station includes a locking ring and a double-end stud, straight teeth are arranged on the middle of the double-end stud in the circumferential direction, the stopping station is arranged at one ends of the straight teeth, a tool withdrawal groove is formed in the root of the joint of the stopping station and the straight teeth, the width of therelief escape is 0.4-0.5mm, and the groove bottom size of the tool withdrawal groove is 0.05-0.1mm smaller than the small diameter of the straight teeth. The problems that existing fasteners special for connection and looseness-proof of aerospace are not reasonable in structure design and high-probability scrapping is caused during installation are solved.

The invention discloses a high-medium-pressure dummy-shaft-free final assembly method for a modified unit, and relates to the field of assembling processes of large equipment. The method aims to solvethe problems that when an existing assembly method is used for assembling a high-medium-pressure inner cylinder and inner sleeves of a modified unit, the assembling period is too long, the working efficiency is low, and delay is possibly caused. By the adoption of the novel high-medium-pressure part dummy-shaft-free final assembly method, a dummy shaft does not need to be used for centering all the sleeves, the time for centering the inner cylinder and all the inner sleeves through the dummy shaft is saved, due to the fact that the dummy shaft needs to be hoisted in again and calibrated in the centering process of each inner sleeve, the dummy shaft needs to be in place again when a product pin is replaced, the novel final assembly process scheme also meets all assembly requirements of final assembly, a large amount of assembly time is saved, the maintenance period of owners can be met, and the working efficiency is improved. The method is suitable for high-medium-pressure dummy-shaft-free assembly of the modified unit.

The invention relates to a bonded permanent magnet for a large direct-drive permanent-magnet generator. The permanent magnet is formed by bonding a plurality of small permanent magnets. Since each permanent magnet group is formed by bonding a plurality of permanent magnets, the surface eddy, heat and thermal loss of the permanent magnets can be effectively reduced; in consideration of the requirements for salt-fog resistance and humidity-heat resistance in the overall operating environment of a wind-driven generator set, the coating thereof can ensure that the permanent magnets can meet the operating requirements under severe environmental conditions and can not cause the inter-layer conduction of the permanent magnets; and epoxy glue used for bonding the permanent magnets has fine insulating properties such as high temperature resistance, convenient curing process, high dielectric property, surface creepage resistance and arc resistance. In use, the invention can effectively ensure assembling requirements, can achieve the technical requirement effect and can be widely used for permanent magnets of various large permanent-magnet generators.

The invention relates to a manufacturing method of a locking ring and used fixtures, which belong to the technical field of aircraft engines. By using the manufacturing method and the used fixtures, the technical problems of easiness in deformation and difficulty in tight winding and forming due to the fact that a flat wire is used for winding the locking ring are successfully solved. The manufacturing method has the technical scheme that the manufacturing method of the locking ring comprises the following steps of preparation of raw materials, preparation of winding, winding of the flat wire, forming of the locking ring and heat treatment for forming. An auxiliary winding fixture special for the locking ring comprises a base, wherein a shell is arranged on the base, and an outer roller and an inner roller are arranged in the shell. A rectangular thread slot winding fixture special for the locking ring comprises a core rod, wherein a core rod step is arranged on the core rod, a step rectangular slot is formed in the core rod step, a bolt is arranged on one side of the step rectangular slot, and a washer is arranged between the bolt and the core rod step. A forming fixture special for the locking ring comprises a forming base, wherein an inner step is arranged inside the forming base, and a pressure plate is arranged above the forming base.

The invention discloses a 12 kV solid insulation single-phase and single-cavity sealed type shell. The 12 kV solid insulation single-phase and single-cavity sealed type shell comprises a shell body made of solid epoxy resin, wherein a cavity 5 is formed in the shell body, an opening communicated with the cavity 5 is formed in the top of the shell body, an elliptic hole 1 is formed in the upper portion of the outer wall of the front face of the shell body, and a cylinder cavity 2 is formed in the lower portion of the rear face of the shell body. The 12 kV solid insulation single-phase and single-cavity sealed type shell is characterized in that a silica gel layer 3 is arranged between the cylinder cavity 2 and the shell body, an electric conductor 8 is embedded in the bottom of the cavity 5, the electric conductor 8 and the cylinder cavity 2 are isolated through the silica gel layer 3, a hole 7 is formed in the bottom of the cavity 5, and the electric conductor 8 is arranged between the cylinder cavity 2 and the hole 7.

The invention relates to the technical field of cell parallel battery modules, in particular to a 21700 cell parallel battery module. The battery module comprises a module housing and a plurality of 21700 single cells. A confluence plate is installed on the outer walls of two sides of the module housing, a plurality of insertion slots are arranged on the inner walls of two sides of the module housing, through holes for electrode piercing are mounted on the two side walls of the module housing, the through holes of the electrode piercing correspond to the positions of the insertion slots one byone, and a plurality of confluence pieces on each confluence plate are connected with the electrodes at both ends of the 21700 single cells one by one, respectively. According to the 21700 cell parallel battery module disclosed by the invention, the 21700 single cells is fixed in the module housing in an inserting and clamping manner by installing the plurality of insertion slots for installing the 21700 single cells in the module housing, and the 21700 cell parallel battery module can meet the high-strength structure required for the parallel battery module composed of the 21700 single cellswith large capacity, and has a simple structure and is low in manufacturing cost.

The invention discloses a device and method for detecting the uniform distribution positions of blade-shaped holes in a thin-wall fan-shaped section. The inner conical surface of an arc-shaped positioning block can be attached to the outer conical surface of a to-be-detected part, and the positions, close to the two ends, of the arc-shaped positioning block are provided with through grooves which are consistent with the theoretical uniform distribution positions of blade-shaped holes in the two ends of a to-be-measured part, a measuring block is arranged in each through groove in a sliding manner, the measuring end of each measuring block is the same as the theoretical shape of the blade-shaped holes of the to-be-measured part, and the size of the measuring end is equal to the result of the difference of the minimum entity of the blade-shaped holes and the uniform distribution position degree; guide holes consistent with the theoretical uniform distribution positions of the remaining blade-shaped holes of the to-be-measured part are formed in the arc-shaped positioning block and located between the two through grooves, a measuring pin is arranged in each guide hole in a sliding mode, and the diameter of the measuring end of each measuring pin is obtained by subtracting the uniform distribution position degree from the diameter of thesmallest blade-shaped hole inscribed circle in the corresponding position; and a movable pressing block is slidably arranged on the upper end face of a base. According to the device and method of the invention, the measurement of the uniform distribution positions of the blade-shaped holes of the thin-wall fan-shaped section can be rapidly and accurately realized.