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203 results about "Rotational stability" patented technology

Rotational stability. Property of a body for which a small angular displacement sets up a restoring torque that tends to return the body to its original position.

Stabilization system for sensors on moving platforms

ActiveUS20110175604A1Improve mass balanceSmall biasAcceleration measurementFrequency analysisRotational stabilityAir bearing
A stabilized field sensor apparatus collects field data, in particular magnetic field data, with reduced motion noise. The apparatus includes a tear drop shaped housing, a tow frame in the housing, a plurality of vibration isolating dampers spaced around the frame, a base assembly mounted to the dampers, a support pedestal having a bottom end fixed to the base assembly and an upper free end, a single spherical air bearing connected to the upper free end of the pedestal, an instrument platform with a lower hollow funnel having an upper inside apex supported on the air bearing for a one point support, principal and secondary gyro stabilizers for maintaining pivotal and rotational stability, and at least one field sensor mounted to the instrument platform for collecting the field data while being stabilized against motion noise including vibration, pivoting and rotation from the base assembly, from the tow frame and from the housing. Stabilization of the instrument platform is enhanced by preserving accurate balance through a dynamic balancing system whereby small masses are moved under computer control to maintain the center of mass of the instrument platform at the center of rotation of the spherical air bearing. The dynamic stabilization process is made more precise by actively vibrating the instrument platform by a set of linear vibrators.
Owner:VALE LIMITED

Self-circulation treatment casing for simultaneously improving stator corner region flowing

The invention relates to multistage axial flow air compressor treatment casings, and discloses a self-circulation treatment casing for simultaneously improving stator corner region flowing. The self-circulation treatment casing comprises a target rotor blade, a downstream stator blade, a casing body and an air guide pipe structure located in the casing body. A flow guide cavity structure penetrating the whole circumferential direction is arranged at the position, on the front edge of a target rotor blade tip, in the casing body. Flow guide cavity outlet front guide vanes used for adjusting the jet flow direction are circumferentially and evenly arranged on the front edge of a flow guide cavity outlet, and the outlet directions of the guide vanes are consistent with the pre-rotating direction of the target rotor blade tip. According to the characteristic of stage-by-stage pressurization of a multistage air compressor, self-adaptive suction and jet flow are formed under the action of differential pressure of a downstream stator blade combined suction groove and the flow guide cavity outlet of the target rotor blade tip; separated flowing of a stator three-dimensional corner region of the air compressor is effectively restrained, and meanwhile moving blade rotating stall is prevented from happening too early through circumferentially-even jet flow with the pre-rotating direction consistent with that of the rotor blade tip; the rotor blade rotating stability and margin are increased; and the stable work condition range of the air compressor is widened.
Owner:BEIHANG UNIV

Coupler for electric bus motor and manufacturing process thereof

The invention discloses a coupler for an electric bus motor. The coupler comprises a body (1), a flange (2) and a step-shaped through hole. A shaft fastener containing cavity (3) is formed in one end of the through hole, a conical hole (4) with the inner diameter gradually decreasing in the direction from outside to inside is formed in the other end of the through hole, and two key grooves (5) formed in the axial direction are symmetrically formed in the surface of the conical hole (4). The invention further discloses manufacturing process. The coupler for the electric bus motor and the manufacturing process thereof have the advantages that the conical hole structure further improves the coaxiality of a connecting shaft and the coupler, balance performance is good, and the rotating stability of the connecting part is enhanced. A key groove structure further reinforces the coaxiality of the connecting shaft in the conical hole and a connecting shaft fixedly connected with the flange. In the manufacturing process, location operation is simple, and locating is stable and accurate, so that processing precision of a workpiece is ensured, quality is stable and reliable, the requirement for design precision and the requirement for interchangeability of motor general assembly are ensured, and manufacturing is safe and protects the environment without pollution.
Owner:SICHUAN DONGFENG ELECTRIC MACHINARY WORKS CO LTD

Rotating blade and stationary blade combined self-adaption adjustment multistage axial flow gas compressor

ActiveCN107165864AIncrease marginBroaden the range of stable working conditionsPump componentsPump controlRotational stabilityGas compressor
The invention relates to a multistage axial flow gas compressor and discloses a rotating blade and stationary blade combined adjustment multistage axial flow gas compressor which comprises a target rotor blade, a downstream stator blade, a downstream stator blade wheel disk, a target rotor blade wheel disk and a rotor wheel disk drainage cavity structure rotating synchronously with an engine shaft. Through a guiding blade in a jet flow gas flow guiding cavity, drainage gas has the same convected velocity as a rotor, and a jet flow groove further acts on an end area and a blade tip of the target rotor blade. According to the characteristics of pressurizing by stages of the multistage gas compressor, a self-adaptive suction and wall-attached jet flow is formed in a downstream stator combination suction groove and the target rotor end area and the blade tip, rotor and stator three-dimensional angular area separation flowing of the multistage gas compressor is effectively inhibited, leakage flowing of the rotor blade tip is improved, rotating stall caused by three-dimensional angular area separation, blade tip front edge overflow and tail edge countercurrent flow is effectively prevented, the rotating stability of the target rotor is strengthened, the margin is increased, and the stable working condition range of the gas compressor is widened.
Owner:BEIHANG UNIV
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