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31results about How to "High power load" patented technology

Power apparatus for aircraft

The present invention provides a power apparatus for an aircraft. The apparatus comprises a base, a drive source and a rotation propeller, wherein the drive source drives the rotation propeller to rotate. The rotation propeller comprises a rotation propeller shaft and a propeller blade assembly. The rotation propeller shaft forms a rotatable connection with the drive source. The propeller blade assembly is provided with a propeller blade shaft, wherein the propeller blade shaft is perpendicular to the rotation propeller shaft, and can rotate around the axial line of the propeller blade shaft. The base is provided with a cam part, and a guidance part with a preset shape is formed on the cam part. The propeller blade assembly is provided with a conduction part and a rotation angle spacing part, wherein the conduction part contacts the guidance part to drive the propeller blade assembly to rotate around the propeller blade shaft, the rotation angle spacing part limits the rotation angle of the propeller blade assembly around the propeller blade shaft. According to the present invention, the problems of requirements of large amount of continuous and stable air working medium with a certain dynamic pressure energy during the vertical aircraft taking off and landing process are solved; the power apparatus provided by the present invention has characteristics of simple structure, large power load, high efficiency and convenient and flexible operation.
Owner:陈志灵

Novel inner rotor permanent magnet hub motor for moped scooter

The invention provides a novel inner rotor permanent magnet hub motor for a moped scooter. The novel inner rotor permanent magnet hub motor is characterized in that a left permanent magnet hub motor electromagnetic structure A and a right permanent magnet hub motor electromagnetic structure B are arranged on the left side and the right side of a motor shaft respectively and isolated by an outer shell support, the outer shell support is fixedly connected with the motor shaft, a motor outer shell is fixedly connected with the outer shell support, a motor stator is fixedly connected with the motor outer shell, a motor rotor and a hub are fixed, the hub is installed between the motor shaft and the motor outer shell through a bearing, the hub is connected with a disc-shaped shaft surface, a plurality of holes are formed in the periphery of the shaft surface to be connected with spokes of a bicycle, the rotor rotates to drive the hub to rotate, the hub rotates to drive the shaft surface to rotate, and the spokes of wheels of the bicycle are accordingly driven to rotate. The novel inner rotor permanent magnet hub motor has the advantages that the radiating effect of the motor is good, and large power loads can be borne; meanwhile, the one motor can be selected for working, or two motors can be selected for simultaneous work, and power selection space is large.
Owner:NANTONG LEISHENG SPECIAL MOTOR

A kind of convective heat sink and its manufacturing method

The invention relates to a counter flow type radiator and a manufacturing method thereof. The structure is particularly suitable for devices with ordinary heating requirements. The counter flow type radiator comprises a cooling pipe, cooling fins and an electric heat pipe. The cooling pipe is provided with an electric heat pipe installing hole. Shrinkage joints are arranged in the cooling pipe installing hole. The electric heat pipe is installed in the electric heat pipe installing hole. The cooling fins are arranged outside the cooling pipe. Compensation shrinkage joints are reserved in the cooling fins. The manufacturing method of the counter flow type radiator comprises the steps that firstly, an aluminum sectional bar is adopted to be machined into the cooling pipe, the electric heat pipe installing hole is reserved in the middle of the cooling pipe, and the shrinkage joints are reserved in the electric heat pipe installing hole; secondly, the cooling fins are manufactured above and below the cooling pipe, and the compensation shrinkage joints are reserved in the length direction of the cooling fins; and thirdly, the electric heat pipe is installed and installed in the electric heat pipe installing hole in the middle of the cooling pipe, the electric heat pipe and the electric heat pipe installing hole are in close contact evenly through compression, a compression die is used through a press, the electric heat pipe installing hole formed in the middle of the cooling pipe is pressurized and wraps an electric heat pipe body, the electric heat pipe body and the electric heat pipe installing hole are in close contact evenly through compression, and the counter flow type radiator is manufactured.
Owner:世保康环境电器(南京)有限公司

Fluid curvature engine, fluid curvature engine equipment and control method of fluid curvature engine equipment

The invention discloses a fluid curvature engine, fluid curvature engine equipment and a control method of the fluid curvature engine equipment. The fluid curvature engine is mainly composed of a flying disc shell, a multi-convex-ring disc wing and a high-speed fluid generator, the flying disc shell is an annular or disc-shaped open half cavity, the multi-convex-ring disc wing is annular or disc-shaped, and a plurality of protrusions with curvature radians are arranged on the upper surface of the multi-convex-ring disc wing in the circumferential fluid flowing direction. The fluid curvature engine gives full play to the principle that the combined action of fluid viscosity and high-speed fluid inertia blocks atmospheric pressure to generate a low-pressure area in a curvature reduction area of an upper convex surface so as to generate lift force, and high-speed fluid is controlled to circularly flow in the frisbee shell and repeatedly flow through an arc-shaped curvature upper convex curved surface of a multi-convex-ring disc wing; accordingly, a plurality of corresponding low-pressure areas are generated in the curvature reduction area of the upper convex face of the multi-convex-ring disc wing to generate lift force, the lift-drag ratio of the multi-convex-ring disc wing can be hundreds of, and the problems that an existing engine is small in thrust-weight ratio and insufficient in lift force can be solved. The equipment for providing driving force by adopting the fluid curvature engine is fluid curvature engine equipment.
Owner:田贵川
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