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511 results about "Pitch bearing" patented technology

The pitch bearing, also named blade bearing, is a component of modern wind turbines which connect the rotor hub and the rotor blade. The bearing allows the required oscillation to control the loads and power of the wind turbine. The pitch system brings the blade to the desired position by adapting the aerodynamic angle of attack. The pitch system is also used for emergency breaks of the turbine system.

Method for checking strength performances of variable-pitch bearing and hub connecting bolt and variable-pitch bearing and vane connecting bolt of fan

The invention relates to a method for checking strength performances of a variable-pitch bearing and hub connecting bolt and a variable-pitch bearing and vane connecting bolt of a fan. By utilizing three-dimensional cartographic software, three-dimensional geometrical models of devices in a load transmission path of the variable-pitch bearing and hub connecting bolt and the variable-pitch bearing and vane connecting bolt of the fan are subjected to grid division and assembly separately, and a finite element model is established through finite element software to realize that the load transmission path is complete and consistent with the reality. The devices in the load transmission path at least include a hub, a vane root part, a vane flange, a variable-pitch bearing inner ring, a variable-pitch bearing outer ring, the variable-pitch bearing and hub connecting bolt and the variable-pitch bearing and vane connecting bolt. The method realizes the complete load transmission path, is capable of accurately calculating the limit strength and fatigue strength of the variable-pitch bearing and hub connecting bolt and the variable-pitch bearing and vane connecting bolt of the fan, and improves the operational reliability of a wind power unit.
Owner:XUJI GRP +2

Lightweight helicopter

The present invention relates to a lightweight helicopter with features of coaxial, contra-rotating rotors and weight shift control. It has a rotary wing unit attached to a tricycle assembly through a hang bolt. The rotary wing unit has an engine mounted below a keel post, which drives a pair of contra-rotating coaxial rotors through a primary gearbox and a secondary gear box. The keel post is attached to a triangular control frame, the base of which forms the control bar. The keel post also supports a fuel tank connected to the engine and a tail plane having one or more articulated vertical flaps actuated by cables. The secondary gearbox is provided with a free-wheeling clutch, a pinion gear and bevel gears for transmitting the rotary movement of the engine to the counter rotating coaxial vertical shafts each carrying two rotor blades of airfoil cross section fixed by pitch bearing on teetering plates and teetering hinges to form horizontal rotors. The tricycle assembly has a pilot seat and landing gear as well as controls for operation of the engine, rotors, tail plane and landing gear. The directional control of the helicopter is achieved through the weight shift principle by manipulating the control bar, thereby causing a tilt of the contra-rotating rotors, which cause a corresponding tilt in the aerodynamic thrust of the rotors, propelling the helicopter in the required direction.
Owner:COUNCIL OF SCI & IND RES
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