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37results about How to "Fix flutter" patented technology

Braking flutter inhibition method based on chassis angle assembly transient dynamics

InactiveCN107908871AFix flutterChoose accurate and reasonableGeometric CADSustainable transportationElement modelSimulation
The invention relates to a braking flutter inhibition method based on chassis angle assembly transient dynamics. The method comprises the following steps that: performing a braking flutter finished automobile road experiment; obtaining experiment data, according to the obtained data, obtaining a working condition parameter and a flutter evaluation index when flutter happens; establishing a finiteelement model of the chassis angle assembly transient dynamics, setting an input parameter according to the working condition parameter when the flutter happens, and verifying the model; according tothe finite element model, obtaining stick slip motion characteristics when the flutter happens, and determining a relationship among a system structure parameter input by the model, frictional characteristics and stick slip motion; and inputting the parameters into the model, and according to a model output result, selecting the input parameter which exhibits a highest influence amplitude value onthe flutter evaluation index output by the model, and obtaining a method for inhibiting the flutter of a vibrator. Compared with the prior art, the method has the advantages that a flutter problem ina braking process is effectively solved from a principle, automobile improvement cost is low, feasibility is high and the like.
Owner:TONGJI UNIV

Special positioning fixture for blade numerical control precision machining

The invention discloses a special positioning fixture for blade numerical control precision machining. The special positioning fixture comprises a chuck a and a chuck b, the chuck b is connected with a tailstock of a machine tool, the chuck a is connected with a main shaft head of the machine tool, a fixture body and a baffle ring are connected to the end face of the chuck a, and the fixture body is located between two clamping jaws of the chuck a and comprises a fixing block; and an L-shaped connecting rod a and a connecting rod b are vertically connected to the fixing block, a fastening screw is arranged on the connecting rod a, the connecting rod b is provided with a sliding block sliding along the connecting rod b, and the sliding block is located between the connecting rod a and the connecting rod b. When the special positioning fixture for blade numerical control precision machining is used, it is guaranteed that the blade and the main shaft of the machine tool are coaxial; the two ends of the blade are fastened to solve the problems of chattering caused by dynamic cutting force in the cutting process and deformation caused in the machining process. The special positioning fixture is simple and compact in structure, high in positioning accuracy, rapid and convenient to operate and demount, and capable of effectively guaranteeing the machining accuracy of the front face and the back face of the blade.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Geophysical exploring device and method for transitional zone areas between bog and shallow beach sea

A geophysical exploring device method for the transitional zone areas between bog and shallow beach sea belongs to the technical field of geophysical exploration. An air gun is arranged in a drill bit composed of two drill bit piece bodies, filling blocks are welded into the two drill bit piece bodies, a drill stem connecting flange is arranged at the bottom of a drill stem, the drill stem connecting flange is of an integrated structure, drill bit connecting flanges are arranged at the upper portions of the drill bit piece bodies, the drill bit connecting flanges are of two semi-annular structures, the drill stem connecting flange is sleeved by an anti-loosen screw to be connected with the drill bit connecting flanges, and accordingly the drill stem and the drill bit piece bodies are combined to form a main body structure of a detachable type air gun drill bit. Two symmetrical spiral pieces are welded to the bottoms of the drill bit piece bodies respectively to form a dual-spiral drill bit structure. The diameter of the drill bit composed of the two combined spiral piece is 500mm. The drill bit piece bodies are of hollow structures, composed of two semi-tubular structures respectively and sleeved by screws to be fixed. The air gun is arranged in the hollow structures. By means of the dual-spiral drill bit structure, stimulating operation of the air gun can be finished synchronously.
Owner:BGP OF CHINA NAT GASOLINEEUM CORP

Numerical control card-less rotary cutter

The invention discloses a numerical control card-less rotary cutter, which comprises a base, a front tool post, a rear tool post, a moving motor, compression rollers, a compression roller speed control system and a compression roller rotating motor, wherein two ends of the base are provided with upright brackets which are provided with round timber clamping mechanisms; the base is provided with a tool post slideway, and two ends of the front and the rear tool posts are arranged on the tool post slideway through slide blocks which are sleeved on a sliding leading screw; two compression rollers are arranged on the front tool post in parallel, one compression roller is arranged on the rear tool post, and the three compression rollers are arranged in a triangular shape; the base is provided with a rotary motor which is matched with the round timber clamping mechanisms through a triangular belt, a driven wheel and a big gear wheel, and the driven wheel is matched with a cutting feed speed reducer, a rear transmission gear box, a rear driving shaft and the sliding leading screw; the compression roller rotating motor is matched with the front tool post compression roller; and the motors are connected with a master control system of a computer control cabinet through conducting wires, and an integrated circuit chip is arranged in the computer control cabinet. The numerical control card-less rotary cutter solves the technical problems of rotary cutting bending and fluttering of thin round timbers and operation semi-automation in the prior art.
Owner:朱景振

Supporting module, and electronic device applying same

The invention discloses a supporting module, and an electronic device applying the same. The supporting module is arranged between a first body and a second body and comprises a guide rail, a sliding part, an elastic part and a supporting unit, wherein the guide rail is fixed on the first body and is provided with a first side wall and a second side wall which are opposite to each other; the first side wall is provided with a plurality of first concave parts; the second side wall is provided with a plurality of second concave parts; the first concave parts are in one-to-one correspondence with the second concave parts, and the first concave parts and the second concave parts are depressed in the opposite directions, so that the guide rail has different widths in a first direction; the sliding part can be arranged on the guide rail in a sliding mode along the first direction; the elastic part is arranged on the sliding part and is pressed against a part between the first side wall and the second side wall; and two ends of the supporting unit are respectively arranged on the sliding part and the second body in a rotatable mode along a second direction which is vertical to the first direction. The supporting module is simple in structure, convenient to operate, low in cost and high in universality.
Owner:PROTEK SHANGHAI +1

Double supersatellite inter-cabin data transmission system and its operation method

The invention provides a data transmission system between noncontact double super satellite cabins and an operation method thereof. The integrated responder of a measurement and control subsystem supports measurement and control to the ground and measurement and control to the relay through different frequencies, and a load cabin and a platform cabin adopt the working mode of different pseudo-codes. The data integrated processor of a data transmission subsystem receives the high speed data of camera load, and the data are wirelessly transmitted to the platform cabin in real time to perform data transmission or the data are stored and arranged back to the platform cabin from a storage device and then data transmission is performed according to the situation of whether the satellite is within the border or the visual arc segment of the relay satellite. The inter-satellite communication responder adopts the modulation mode of an inter-satellite non-coherent direct sequence spread spectrum communication system and works in the S-band and the duplex mode, and the inter-satellite communication responder between the two cabins adopts the mode of different bands and different codes. The load cabin and the platform cabin communicate in a noncontact manner so that the problems of interference and fluttering caused by vibration of large flexible structures and moving parts can be solved, and the inter-satellite communication efficiency and the communication efficiency to the ground and the relay can be enhanced.
Owner:SHANGHAI SATELLITE ENG INST

Brake shoe outer circle machining clamp

InactiveCN109648367ASolve the problem of reduced machining accuracyFix flutterPositioning apparatusMetal-working holdersCircular discBrake shoe
The invention relates to the technical field of automobile part machining clamps, in particular to a brake shoe outer circle machining clamp. The brake shoe outer circle machining clamp comprises a rotary machining table, positioning mandrels, a lower fixed circular truncated cone and an upper fixed circular truncated cone, wherein the rotary machining table is in a disc shape, and two sides of the rotary machining table are respectively provided with two first mounting holes which vertically penetrate through the disc surface of the rotary machining table, the positioning mandrels are fixedlyarranged in the first mounting holes, the lower fixed circular truncated cone and the upper fixed circular truncated cone are arranged on the positioning mandrels in a sleeved mode, the fine end of the lower fixed circular truncated cone is arranged upwards, and the thin end of the upper fixed circular truncated cone is arranged downwards, the clamp can fix and machine two brake shoes at the sametime, and the end faces of the brake shoes are not in contact with the clamp, so that the problem that the machining precision of the outer circle surface is reduced due to the fact that the end faceof the brake shoe is uneven is solved, and the positioning hole of the brake shoe is clamped between the upper fixed circular truncated cone and the lower fixed circular truncated cone, so that the problem that the brake shoe is vibrated during machining due to the fact that the positioning hole of the brake shoe is in clearance fit with the positioning mandrel is solved.
Owner:丽水市信裕机械制造有限公司

Novel marine self-floating type wind-wave power generating device

The invention relates to a novel marine self-floating type wind-wave power generating device. The novel marine self-floating type wind-wave power generating device is composed of four self-floating type multi-energy collecting wheels fixed by an anchored rectangular rod frame and used for driving power generators separately. The novel marine self-floating type wind-wave power generating device ischaracterized in that six arc-shaped blades are arranged on a hub of each self-floating type multi-energy collecting wheel, the above-water portions of the blades receive wind energy, and the underwater portions of the blades receive wave energy; and the hollow hubs are used for achieving self-floating, ratchets are arranged on the inner rings of the hollow hubs, ratchet wheels on speed-up machines force the wave energy and the wind energy to selectively rotate in the same direction to push the hollow hubs to rotate the ratchet wheels only in the same direction. The sector blades can be used for receiving the wind energy or the wave energy, the wind energy or the wave energy is absorbed by arc-shaped concave surfaces of the blades, the wind energy or the wind energy is converted into mechanical axial force to push the hollow hubs to rotate, the ratchets cooperating with the ratchet wheels are arranged on the inner rings of the hollow hubs, the ratchet wheels force the wave energy or the wind energy to selectively rotate in the same direction to push the hollow hubs to rotate only in the same direction, thus, the speed-up machines are driven to rotate, and the power generators coaxial with the speed-up machines rotate at a high speed to start to generate power.
Owner:ANHUI UNIV OF SCI & TECH

One-way valve, rocket engine supercharging system and rocket engine

PendingCN114060574AAchieving reverse sealingSolve the problem that the seal is easily brokenCheck valvesRocket engine plantsClassical mechanicsVALVE PORT
The invention discloses a one-way valve, a rocket engine supercharging system and a rocket engine. The one-way valve comprises a guide cylinder, a valve body and a valve element. The guide cylinder is provided with an open end, a closed end and a first boss which transits from the closed end to the open end; the valve body is connected with the outer wall of the guide cylinder to form a main cavity, and is provided with an inlet channel and an outlet channel communicated with the main cavity; the axial cross section of the valve element is in a T shape, the small-diameter end of the valve element is a connecting end, the large-diameter end of the valve element is a force application end, the connecting end is movably arranged on a first boss in the guide cylinder through an elastic piece, and the force application end is used for sealing the inlet channel under the action of the elastic piece. A discharge cavity is formed between the closed end and the elastic piece, and a leakage opening is formed in the portion, forming the discharge cavity, of the guide cylinder and used for discharging media leaked from the main cavity to the discharge cavity. In the state that the force application end seals the inlet channel, the contact areas of the two surfaces in the thickness direction of the force application end and the main cavity are the same, so that the valve is prevented from being opened when the valve is reversely communicated with a high-pressure medium.
Owner:BEIJING LANDSPACETECH CO LTD

Semi-automatic five-shaft dividing and cutting machine

The invention discloses a semi-automatic five-shaft dividing and cutting machine which comprises a machine frame, a shaft supporting component, a rotating shaft component, a supporting wheel component, a cutting and moving platform, a control panel, an electrical box, a driving box, a displayer and a cutting component. Five cutting shafts are symmetrically installed on a shaft bottom plate and a shaft installation rear plate through radial bearings respectively, and two sets of shafts are installed on the shaft bottom plate. One set of shafts are used for cutting, the other set of shafts are used for feeding and discharging, can rotate around a T-shaped shaft and are interchanged in position, shaft supports are arranged during cutting of the cutting shafts, supporting wheels are arranged on one side of a workpiece and used for offsetting cutting radial force, five shafts carry out cutting at the same time, the production efficiency is nearly five times that of a single shaft, the overall machining time is shortened due to coincidence of feeding and discharging auxiliary time and cutting basic time, the production efficiency is improved, due to the application of the shaft supportsand the support wheels, the problems of flutter, cutter back-off and the like in the cutting process are effectively solved, the cutting quality is improved, and the defects are overcome.
Owner:CHANGZHOU COLLEGE OF INFORMATION TECH

Remote sensing satellite platform control and image correction method based on flutter information

PendingCN114545959AFix flutterSolve the problem of clear imagingImage enhancementImage analysisData setImage correction
The invention discloses a remote sensing satellite platform control and image correction method based on flutter information. The method comprises the steps of simulating satellite motion and constructing a flutter image data set, expanding data volume through data enhancement, preprocessing flutter image data, extracting image flutter information by using a ResNet algorithm, feeding back the flutter information to a satellite attitude control system for control, and guiding a Transformer model to perform image correction by using the flutter information. In order to solve the technical problem that space tasks such as high-resolution reconnaissance cannot be clearly imaged due to limitation of high-frequency low-amplitude micro-vibration of a spacecraft, satellite flutter information is solved by using a flutter image, and a satellite platform is controlled and image correction network learning is guided by using the flutter information. Therefore, a satellite flutter estimation, attitude control feedback and image correction closed-loop system is built. The invention provides a satellite flutter information estimation and attitude control information feedback based on a ResNet algorithm and a flutter image correction intelligent method based on a Transform model, and the spatial information intelligent processing capability of China is effectively improved.
Owner:PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV

Pneumatic support device for steady operation of overlong boring cutter bar

The invention provides a pneumatic support device for steady operation of an overlong boring cutter bar. In the device, two support plates of a cylinder support (3) are fixed on a base plate, and thedistance between the two support plates meet the mounting requirements of a cylinder (7); a connecting line between cylinder mounting holes on the two support plates and the central line of the base plate form an included angle alpha; and the degree of the included angle alpha is consistent with the direction of resultant cutting force. Two ends of the cylinder (7) are fixed on the cylinder support (3); and the cylinder support is fixed on an end face of a boring cutter bar (1); the boring cutter bar (1) is provided with an air tube mounting groove, one end of an air tube (8) is communicated with the cylinder, and the other end thereof is communicated with a pressure regulating/stabilizing unit (4) and an air tube switch (5). A piston rod of the cylinder extends to prop on the inner wall of a bottom hole and support the boring cutter bar when compressed air enters the cylinder. The pneumatic support device solves the problems of cutter relieving and vibration due to insufficient cutterbar rigidity in precision boring of hole parts with large length-diameter ratio, is applicable to boring of holes with large length-diameter ratio, and has the advantageous of simple structure, convenient operation, reliable operation, low cost and no pollution.
Owner:AECC AVIATION POWER CO LTD

Rate gyro stabilizing platform type antenna followup system

InactiveCN101382805BUnrestricted angleFast trackingControl using feedbackNegative feedbackRadar
The invention provides a follow-up tracking system of a rate gyroscope stabilized platform type antenna, which comprises a direction-finding device, an adjustment link, a PID controller, a PWM driver, a moment motor, an angle measuring potentiometer, an angular rate gyroscope and a differential link. The PWM driver, the moment motor, the angular rate gyroscope and the differential link are connected in sequence to form an angular acceleration negative feedback loop; the PID controller, the PWM driver, the moment motor and the the angular rate gyroscope are connected in sequence to form an angular rate negative feedback loop; the direction-finding device, a preamplifier, the adjustment link and the angular rate negative feedback circuit form an angular position negative feedback loop; the angle measuring potentiometer, the preamplifier, the adjustment link and the angular rate negative feedback loop form an angle searching loop. The follow-up tracking system is an antenna follow-up system which is used for realizing the follow-up tracking technology of stably tracking, searching and isolating the angular motion of a carrier in the direction-finding devices, such as radars, optical imaging, and the like, in moving carriers so as to realize high precision, weak coupling, anti-turn-off performance, fastness and stabilization and realize proportional guidance.
Owner:HARBIN ENG UNIV
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