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462results about How to "Increase the moment of inertia" patented technology

Body in white bend resistance structure and arrangement mode thereof

The invention provides a body in white bend resistance structure and an arrangement mode thereof. The lower end of a lower vertical plate of a column A is in overlap connection with a sill strip. The upper end of the lower vertical plate of the column A is in overlap connection with an outer plate of the column A. The outer plate of the column A is in overlap connection with an upper beam of a column B. The upper end of an outer plate of the column B is in overlap connection with the upper beam of the column B. The lower end of the outer plate of the column B is in overlap connection with the sill strip. Two to three layers of spot welding connection is formed at each overlap joint to form a closed structure. The bend resistance section of the sill strip, the bend resistance section of the vertical plate of the column A, the bend resistance section of the outer plate of the column A and the bend resistance section of the upper beam of the column B are each in a closed annular shape. Due to the fact that the bend resistance sections form the closed annular shapes and are composed of three or four sheet metal parts, the bend resistance is improved; due to extending sections at the upper and lower ends of the outer plate of the column B, the overlap connection efficiency of the upper beam and the sill strip of the column B and the outer plate of the column B is enhanced, and the bend resistance performance is improved; the transverse and longitudinal staggered closed structure has the effect of enhancing inertia torque, and the bend resistance performance is improved.
Owner:CHINA AUTOMOTIVE ENG RES INST

Single column maritime wind power generation device with circumferential stabilizing column

The invention provides a single column maritime wind power generation device with a circumferential stabilizing column, and belongs to the technical field of ocean energy resource utilization. The single column maritime wind power generation device with the circumferential stabilizing column comprises a wind power generation set, a single column base, the circumferential stabilizing column, a supporting structure, a berthing system and a fixed ballast system; the wind power generation set is fixed on the single column base; the circumferential stabilizing column is fixed at the periphery of the single column base; both ends of the supporting structure are connected with the circumferential stabilizing column and the single column base respectively; the middle part and the bottom of the single column base are connected with the berthing system and the fixed ballast system respectively; and the berthing system is connected with the seabed. By arranging the circumferential stabilizing column, a larger waterline plane inertial moment can be obtained in a smaller waterline plane area; meanwhile, due to the low gravity center of the single column base, the stability requirement is met and the high water power performance is gained; therefore, a stable, economic and flexible floating base is provided for the wind power generation set, so the single column maritime wind power generation device with the circumferential stabilizing column is particularly applicable to deep water regions of the open sea.
Owner:SHANGHAI JIAO TONG UNIV

Method for regulating and controlling posture of spacecraft by flow velocity and actuating mechanism thereof

The invention relates to a method for regulating and controlling a posture of a spacecraft by the flow velocity and an actuating mechanism thereof and belongs to the field of control to the posture of the spacecraft. The method comprises the following steps that: according to a difference value of a current posture and a desired posture, a three-axis control moment vector required by the spacecraft is obtained, and according to a principle of the momentum moment, a relation between the three-axis control moment vector and the variation of a liquid fuel flowing angular velocity is obtained; according to the working principle of ring-shaped pipe liquid angular momentum exchange equipment, a relation between the liquid fuel flowing angular velocity and the change rate of a velocity vector inthe tangential direction of a pipe when liquid fuel flows is obtained; according to corresponding generated required conditions, the power of the pressure pump is controlled to apply work to the liquid, so that the flow velocity of the liquid is changed, and thus, the angular momentum H of a mass center of the spacecraft is changed and the posture of the spacecraft 10 is changed; and the changed posture is measured by a sensor and is compared with the desired posture and the steps are circularly repeated from the beginning of the step 1. The actuating mechanism for regulating and controlling the posture of the spacecraft by the flow velocity, which is used for implementing the method disclosed by the invention, comprises a liquid filled ring-shaped pipe, the pressure pump, an oil storage tank, a valve, a liquid outlet connecting pipe, a liquid return connecting pipe and a control mechanism.
Owner:BEIHANG UNIV

Flywheel motor adopting no-cross one-range winding

The invention discloses a flywheel motor adopting a no-cross one-range winding, relating to the technical field of the motor and solving the problems that the existing flywheel motor has complex structure, large power consumption and poor moment stability. A rotor in the invention is a wheel body of a flywheel; an outer rotor iron core and an inner rotor iron core of the rotor are fixedly connected on a torque output shaft; a no-iron core frame type stator is fixed between the inner rotor iron core and the outer rotor iron core; permanent magnets are fixed on the inner rotor iron core or the outer rotor iron core and the side wall corresponding to the no-iron core frame type stator; a winding of the no-iron core frame type stator consists of a plurality of groups of planar coils which areevenly distributed and fixed on the side wall of the frame; two adjacent groups of planar coils have an electric angle of 240 degrees, and have no cross; three position sensors are respectively fixedon the frames at the central positions of three adjacent groups of planar coils; and the ratio of the number Z of the planar coils and the number 2p of poles of the permanent magnets is 3/4. The flywheel motor is applicable to the technical fields of posture control of the satellites and control moment gyros and the like.
Owner:HARBIN INST OF TECH

Novel load-bearing and heat-insulation integrated prefabricated fabricated-type shear wall and construction method

InactiveCN108149814AStable mechanical propertiesWith load-bearing functionWallsHeat proofingFiberBlade plate
The invention relates to a novel load-bearing and heat-insulation integrated prefabricated fabricated-type shear wall and a construction method, and belongs to the technical field of fabricated-type building construction. The novel prefabricated fabricated-type shear wall comprises an inner blade plate, an outer blade plate, a heat-insulation structure layer and a plurality of connecting pieces made of fiber reinforced plastic, wherein both the inner blade plate and the outer blade plate are provided with vertically-distributed steel bars and transversely-distributed steel bars. A restrained edge member area is provided with longitudinal stress steel bars, stirrups and first steel sleeves. According to the novel prefabricated fabricated-type shear wall, the thickness of a wall body is reduced, so that the effective usable area of a building is increased, the structures of the inner blade plate and the outer blade plate are optimized, so that the two sides of the heat-insulation structure layer are effectively protected, and the connecting pieces and the stirrups adopt the fiber reinforced plastic, so that heat-insulation performance of the heat-insulation structure layer is improved; and meanwhile, the wall body has excellent mechanical properties. The construction method has the advantages of being simple in operation, high in construction efficiency and the like.
Owner:SHANGHAI CONSTRUCTION GROUP

Flying wheel energy storage type rivetless connection device of servo motor and connection method of connection device

The invention discloses a flying wheel energy storage type rivetless connection device of a servo motor and a connection method of the connection device. The connection device comprises a motor, wherein an output shaft of the motor is connected with a shaft; a flying wheel is fixed on the shaft; a clutch is connected together with the flying wheel; the clutch is fixed at an optical shaft end of a screw rod; a screw rod nut is fixed with a nut sleeve; the nut sleeve is fixed on a sliding block; the sliding block is configured on a guide rail; the guide rail is fixed on a rack; a punch head is connected with the nut sleeve; a plate material is placed on the rack below the punch head; the rack is provided with a die cavity; the motor drives the flying wheel, the clutch and the screw rod to do rotary movement; the flying wheel stores energy for increasing the rotary inertia, and the rotary movement of the flying wheel is converted into the linear movement by the screw rod nut; the flying wheel is separated from the clutch the moment the punch head is in contact with the plate material, and the screw rod transmits a torque for driving the punch head to do linear impact movement for punching the plate material; and when the deformation amount reaches the expected requirement, and the plate material is filled in the die cavity of the rack, and the connection is finished. According to the flying wheel energy storage type rivetless connection device, the connector bonding quality and the production efficiency are guaranteed, and the connection device has the advantages of time-saving, labor-saving and energy-saving.
Owner:XI AN JIAOTONG UNIV

Method for improving stability of virtual synchronous machine grid-connected inverter system with consideration of sampling delay

The invention discloses a method for improving the stability of a virtual synchronous machine grid-connected inverter system with the consideration of sampling delay. The method comprises the steps: establishing a small signal state space model of a VSG grid-connected inverter system; analyzing the structure of the VSG grid-connected inverter system, and determining the position of a delay link; determining a small signal state space equation of each link in the VSG grid-connected inverter system; establishing a small signal state space delay correction model of the VSG grid-connected invertersystem according to the small signal state space model of the VSG grid-connected inverter system and the small signal state space equation of each link of the VSG grid-connected inverter system; on the basis of the delay correction model, analyzing the stability of the VSG grid-connected inverter system, and determining a control parameter value range capable of enabling the VSG grid-connected inverter system to stably operate, thereby improving the stability of the VSG grid-connected inverter system. The problem that an existing VSG model is not accurate enough is solved, and the problem that the stability of the VSG grid-connected inverter system is not high due to the fact that the stability of the VSG grid-connected inverter system is analyzed on the basis of an ideal VSG model is solved.
Owner:HUNAN UNIV

Multi-locomotive fixing and rolling test platform

The invention relates to a multi-locomotive fixing and rolling test platform which comprises two or three test platforms. Each test platform comprises a pair of counter-force frames (1), an upper axle (2) and test unit groups, wherein the test unit groups comprise test units having same number with single locomotive wheel pairs (41). All the test units adopt the structure that shafts of a track wheel pair (43) for supporting the locomotive wheel pairs (41) are connected with shafts of winding asynchronous motors (36), and the diameter/length ratio of the winding asynchronous motors is larger than 1; stator windings of all the winding asynchronous motors (36) of each test unit group are connected with a power grid by a three-phase switch I (63) of a stator three-phase bus bar (53) of each asynchronous motor, and rotor windings are connected in parallel to a rotor three-phase bus bar (49) of each asynchronous motor; and the rotor three-phase bus bars of the asynchronous motors of all the test unit groups are connected by a breaker (62). The test platform carries out a mutual accompanying test by multiple locomotives and has reliable synchronization and convenient test and can form the mutual feedback of energy, reduce the capacity of a power supply and save energy sources and cost.
Owner:SOUTHWEST JIAOTONG UNIV

Large-size high-speed invisible flying saucer

The invention discloses a flying saucer and two smoke- and fire-free engines. The flying saucer is composed of a cabin and a disk which rotates round the cabin. The disk includes a disk-shaped wing and a rotary engine. The cabin includes a driving cabin, a passenger cabin and a device cabin. The rotary engine sucks air which is mixed with water, and then the mixture is jetted out horizontally through jet tubes installed on the edge of the disk according to the sprayer principle, so that a generated reactive force enables the disk to rotate at a high speed, thereby generating an upward raising force on the disk. Four fixing wings are installed outside the device cabin to eliminate reverse rotation of the cabin. A vector engine and a diesel power generating set are installed in the device cabin under the disk. The vector engine sucks large amount of air through an air inlet duct in the passenger cabin to form vacuum above the passenger cabin, which enables air pressure difference between an upper surface and a lower surface of the disk to be increased, thereby generating a huge raising force. The sucked air is compressed to form high-pressure gas which is discharged into vector jet tubes and is jetted out, wherein the directions and the angles of the vector jet tubes are adjustable to generate pushing forces in different directions, thereby achieving maneuvering flight of the flying saucer.
Owner:周彦辉

Momentum wheel based on disc type structure

The invention relates to a momentum wheel based on a disc type structure. The momentum wheel comprises a lower layer stator and an upper layer stator, wherein the upper layer stator and the lower layer stator are fixed in parallel; an air gap is formed between the upper layer stator and the lower layer stator; a rotor is arranged in the air gap; a mass block is arranged at the outer side of the rotor; the upper and lower planes of the inside are provided with annular sector grooves in the radial direction; a permanent magnet is fixed in each groove; the magnetizing directions of the permanent magnets at the upper and lower layers are identical; the N poles and the S poles are alternately arranged; stator tooth grooves are formed in the upper layer stator and the lower layer stator; a coil is wound in each stator groove; the stators are fixed with the outer sides of bearings; the center of the rotor is a motor middle shaft; the bearings sheath the middle shaft; and the top of the middle shaft is provided with a photoelectric encoder. The momentum wheel has the advantages that in the moving process, the input is a three-phase power supply; a permanent magnet motor of an axial magnetic field structure is used, the momentum wheel can output great torque; by using the disc type structure of the momentum wheel, the structure of the momentum wheel is compact, and the axial size of the momentum wheel is effectively reduced; fractional-slot structure windings are used, so that the tooth groove torque of the momentum wheel can be effectively reduced, and the movement of the momentum wheel is smooth and stable; and meanwhile, the photoelectric encoder is used, so that the rotation condition of the momentum wheel can be precisely measured.
Owner:XI AN JIAOTONG UNIV

Anti-buckling supporting member with lattice type double-rectangular-pipe cross section

An anti-buckling supporting member with a lattice type double-rectangular-pipe cross section comprises two anti-buckling branches which are connected through a plurality of steel batten plates, wherein each branch adopts an anti-buckling supporting member provided with a linear core and a restraint concrete-filled rectangular steel pipe; long edges of the two branches are parallelly arranged at appropriate intervals, a lattice type member formed by connecting the plurality of steel batten plates which are distributed longitudinally is taken as a whole for common work, the steel batten plates and branch short edges, namely short edges of the restraint rectangular steel pipes, are in welded connection through trihedral angle welding seams; and end parts of the linear cross section cores of the two branches extend out of circumferential restraint members, and are connected through a ribbed plate to form an H-shaped cross section which can be connected with a frame member through a high-strength bolt and a connecting plate. The lattice type cross section can increase inertia moment of the whole cross section of the anti-buckling supporting member and the whole flexural rigidity, thereby particularly suitable for a design of a large-tonnage anti-buckling support member, the support end part is conveniently connected with the frame member, and the lower branch still can sufficiently play energy-dissipating capacity when eccentric bending moment is added.
Owner:TSINGHUA UNIV
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