Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

35results about How to "Low-speed" patented technology

Transmission mechanism for permanent magnetic gear

InactiveCN104901510AElectromagnetic structure is simpleReduce manufacturing costsDynamo-electric gearsElectrical conductorPower flow
The invention discloses a transmission mechanism for a permanent magnetic gear. The transmission mechanism comprises a stator assembly, an adjustable magnetic ring assembly, a rotor assembly and an enclosure assembly. The transmission mechanism is only provided with a layer of permanent magnet, so that the processing and assembling difficulty is smaller while a permanent magnet is saved. The permanent magnet is fixed by a built-in hole in a rotor core, and the condition that the permanent magnet is thrown away due to a centrifugal force generated by the rotor core during high-speed rotation is avoided, so that the permanent magnet is safe and reliable. The transmission ratio of the transmission mechanism can be changed according to the requirement; the output rotating speed of the transmission mechanism can be set to be constant according to the requirement. A damping bar made of a conductor material is arranged on the rotor core and can be used for cutting a magnetic field generated by a stator winding and forming induced current; a lorentz force generated by the induced current can form damping, so that the rotating speed and the torque of the rotor after starting are rapidly converged and the rotor stably operates; heat generated by the stator assembly, the adjustable magnetic ring assembly and the rotor assembly can be taken away by air current of the transmission mechanism.
Owner:DALIAN JIAOTONG UNIVERSITY

Asymmetric FHE (Fully Homomorphic Encryption) method and secret key substitution and cipher text delivery methods thereof

The invention relates to an asymmetric FHE method and secret key substitution and cipher text delivery methods thereof. A private key and a public key are generated randomly, and the secret key is used to generate an operation support function, a unit cipher text of secret key encryption and a public key encryption operation support function; a plaintext is encrypted to generate a cipher text, namely, the secret key is used for encryption directly to obtain a direct cipher text, or the public key corresponding to the secret key is used to carry out encryption operation to obtain a compatible cipher text in the same secret key space; and when the cipher text needs to be delivered to the receiving end safely, the sending, receiving and server ends or the sending and receiving ends complete delivery of the cipher text. Operation of the cipher text is carried out directly without leakage of the plaintext, a safe data storage and operation environment is provided, the computing speed is improved substantially compared with the prior art, the required cipher text volume and expansion speed are lower, the methods can be realized in different manners, and a data owner can use different cloud computing services needless of worrying about leakage of sensitive and secrete data.
Owner:上海麟羿信息科技有限公司

Reinforced structure for gear and rotating shaft connection

The invention provides a reinforced structure for gear and rotating shaft connection. The structure comprises a gear, a flat key, a rotating shaft, a reinforcing column, an adjusting hole and buckles;the rotating shaft is fixedly arranged on the inner side of the gear, second springs are fixedly connected to one side faces of the two buckles, a movable cavity is formed in the periphery of the rotating shaft, the reinforcing column is fixedly connected to the middle of each support block, arc clamping grooves are formed in the two sides of the top of the reinforcing column, first springs are fixedly connected to the left end and the right end of the support block, and a screw is fixedly connected to the upper portion of a convex connecting block. Accordingly, by means of cooperation of thereinforcing column and the fixed cavity, when the gear rotates at a high speed, the reinforcing column can be thrown out of the rotating shaft by means of centrifugal force, then the reinforcing column is fixed through the fixed cavity so that the joint of the gear and the rotating shaft can be reinforced through the reinforcing column, and axial support is provided; meanwhile, the radial load ofthe flat key is shared, the phenomena of cutting, deforming and cracking of the flat key are reduced, and the stability and accuracy of the gear in the high-speed rotating process are enhanced.
Owner:蒋宇

Aircraft prediction and correction composite guidance method based on sliding mode disturbance observer

The invention relates to an aircraft prediction and correction composite guidance method based on a sliding mode disturbance observer, wherein the method comprises the following steps: 1, building an aircraft three-degree-of-freedom nonlinear model containing multi-source disturbance according to the nonlinear kinematics and dynamics characteristics of a hypersonic aircraft, and carrying out representation of the multi-source disturbance; 2, designing the sliding mode disturbance observer to carry out rapid online estimation on lumped disturbance; 3, respectively designing a longitudinal guidance law and a lateral guidance law according to the flight state and control input of the aircraft at the current moment, and converting heat flux density, overload and dynamic pressure constraints into heeling angle amplitude constraints by using quasi-equilibrium gliding conditions and disturbance estimated values to ensure that process constraints are met; and 4, designing a composite guidance law according to the disturbance estimation value and the output value of the prediction correction guidance, and finally completing the design of the guidance method. The method is high in anti-disturbance capability, high in guidance precision and suitable for various types of hypersonic aircrafts without power reentry.
Owner:BEIHANG UNIV

Large-diameter offshore wind power rock-socketed single pile excavating method

The invention discloses a large-diameter offshore wind power rock-socketed single pile excavating method. The large-diameter offshore wind power rock-socketed single pile excavating method comprises the following steps that immersion of a pilot shaft pile casing is carried out; a petroleum drilling machine is adopted for excavating a pilot shaft through the pilot shaft pile casing; a geological drill is adopted for drilling two to three rings of main blast holes and one ring of outline blast holes, and a casing off hole is lowered down; a dedicated CO2 phase change expansion crack pipe is mounted, the interiors of the main blast holes are mounted in a segmented manner, and the interiors of the outline blast holes are continuously mounted; a blast network is connected; a rock-socketed single pile steel pile casing is lowered down; mud and weathering sand between the pilot shaft pile casing and the rock-socketed single pile steel pile casing are sucked away; the pilot shaft pile casing and a drilling casing pile are pulled out; underwater slag cleaning is carried out; and concrete is poured to form a rock-socketed single pile foundation. Pilot shaft mechanical excavating and CO2 expansion rock breaking and expanded excavating are combined, the technical problem that a 2-4mm-diameter petroleum drilling machine and a common geological drill are used for finishing excavating of an offshore rock-socketed single pile foundation with the diameter being 8 to 10 m and above can be solved, the expansion pressure generated by a CO2 phase change is controllable, the explosion impact waves and the vibration speed are small, and the method is economic and environment-friendly.
Owner:WUHAN UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products